Quick Action
Reference
Index
Handbook
737 Flight Crew Operations Manual
737
Quick Reference Handbook
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Quick Action Index
Aborted Engine Start.................................... 7.1
Airspeed Unreliable.................................... 10.1
Airspeed Unreliable (Stick Shaker Deactivation
by Pulling Circuit Breaker) ..................... 10.10
APU FIRE ..................................................... 8.1
CABIN ALTITUDE WARNING.......... 2.1
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Emergency Descent........................0.1
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Engine Fire on the Ground............ Back Cover.2
ENGINE FIRE................................................ 8.2
Engine Limit or Surge or Stall ...................... 7.2
ENGINE OVERHEAT ...................................... 8.7
Engine Severe Damage or Separation .......... 8.2
Engine Tailpipe Fire ..................................... 8.8
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LANDING CONFIGURATION........................ 15.1
Loss Of Thrust On Both Engines ................... 7.6
Rapid Depressurization ................. 2.1
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Runaway Stabilizer ...................................... 9.1
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Evacuation ..................... Back Cover.4
TAKEOFF CONFIGURATION ........................ 15.1
WARNING HORN (INTERMITTENT) ............ 15.2
WARNING LIGHT - CABIN ALTITUDE OR
TAKEOFF CONFIGURATION....................... 15.2
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
2
D6-27370-8AS-NOK
QA.Index.1
March 31, 2023
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Smoke, Fire or Fumes ..................8.10
Quick Reference Handbook Quick Action Index
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737 Flight Crew Operations Manual
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EXPORT CONTROLLED - This document is subject to the U.S. Export Administration
Regulations (EAR), (15 C.F.R. Parts 730-774). No authorization from the U.S. Department of
Commerce is required for export, re-export, in-country transfer, or access EXCEPT to country
group E:1 or E:2 countries/persons per Supp.1 to Part 740 of the EAR. ECCN: 9E991.
BOEING PROPRIETARY
Copyright © 1999-2023 The Boeing Company. All rights reserved.
Boeing claims copyright in each page of this document only to the extent that the page contains
copyrightable subject matter. Boeing also claims copyright in this document as a compilation
and/or collective work.
This document includes proprietary information owned by The Boeing Company and/or one or
more third parties. Treatment of the document and the information it contains is governed by
contract with Boeing. For more information, contact The Boeing Company, P.O. Box 3707,
Seattle Washington 98124.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
QA.Index.2
D6-27370-8AS-NOK
March 31, 2023
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Quick Reference Handbook
(QRH)
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B737-800
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Publication of
Nok Airlines Public Company Limited
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222 Central Building, Room No.4235, 4th Floor,
Vibhavadi Rangsit Road, Sanambin Sub-district,
Don Mueang District, Bangkok, 10210, Thailand
ALL RIGHTS RESERVED.
This Manual belongs to Nok Airlines Public Company Limited. Any
unauthorized reprint or use of this material is prohibited.
No part of this manual may be reproduced or transmitted in any form or by any means,
electronic or mechanical, including photocopying, recording, or by any information
storage and retrieval system without express written permission from Nok Airlines Public
Company Limited.
REVISION: 17
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°Š°µ„µ«¥µœHS-DBO
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1) Emergency Locator Transmitter (ELT)
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2) Emergency Locator Transmitter (ELT)
°Š°µ„µ«¥µœ¨Îµ°ºÉœÇ
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
C406-1 (453-5002), C406-1HM (453-5003)
DESCRIPTION AND OPERATION
TASK 25-62-10-870-801
1. Description
A. Functional Overview
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SUBTASK 25-62-10-870-001
1) The ELT automatically activates during a crash and transmits the standard sweep tone on 121.5 and 243.0
MHz. Approximately every 50 seconds, for up to 520 milliseconds (long message protocol), the 406 MHz
transmitter turns on. During that time, an encoded digital message is sent to the COSPAS-SARSAT Search
and Rescue (SAR) satellite system.
2) The information contained in the message includes:
a) Serial number assigned to the ELT by the beacon manufacturer or the national beacon registration
authority, or
c) Country of registration and country code; plus
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b) Aircraft identification or registration number, and
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d) Position coordinates, when coupled with an ELT/NAV Interface (453-6500). Refer to the ELT/NAV
Interface Abbreviated Component Maintenance Manual (570-4602) for a detailed discussion of the
interaction between the ELT, ELT/NAV Interface, and aircraft navigation system.
3) The 406 MHz transmitter will operate for 24 hours and then shuts down automatically. The 121.5/243.0
transmitter will continue to operate until the batteries are exhausted, which is typically at least 50 hours.
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4) The 406 MHz transmitter produces a much more accurate position, typically 3 kilometers as compared with
15 to 20 kilometers for 121.5/243.0 MHz transmitters. When coupled to the aircraft navigation system via
the ELT/NAV Interface, the accuracy improves to approximately 100 meters.
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5) The ELT transmits a digital message that allows search and rescue authorities to contact the
owner/operator of the aircraft through information contained in a database. Information contained in the
database includes:
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a) Type of aircraft and aircraft registration number,
b) Owner address and telephone number, and
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c) Alternate emergency contact.
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6) After the ELT is activated and the 406 MHz signal is detected by the SAR satellite system and a position is
calculated, the 121.5/243.0 MHz transmissions are used to home in on the crash site.
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NOTE:
Effective February 1, 2009, COSPAS-SARSAT has terminated the satellite processing of
distress signals from 121.5 and 243.0 MHz beacons.
7) Aircraft communications transceivers are not capable of receiving 406 MHz transmissions; therefore, the
only methods of monitoring the ELT are:
a) The blinking cockpit remote switch LED,
b) The buzzer, or
c) 121.5/243.0 MHz transmissions, which can be monitored using the aircraft communications
transceiver or an AM radio tuned to 121.5 MHz.
25-62-10
Page 17 of 67
Feb 28/2019
ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
C406-1 (453-5002), C406-1HM (453-5003)
SUBTASK 25-62-10-870-002
B. Components
1) The C406-1 Series ELT main assembly is housed in a high impact, fire resistant, polycarbonate plastic case,
which is enclosed in a protective mounting frame assembly made of similar material. See Figure 2.
The ELT main assembly and its mounting frame assembly are capable of withstanding
extremely harsh environments and have been subjected to the rigorous environmental
testing required by COSPAS-SARSAT for certification.
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NOTE:
Figure 2 C406-1 Series ELT and Mounting Frame Assembly
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2) The cockpit-mounted remote switch assembly is comprised of an ELT status LED and control switch, which
allows an operator to monitor ELT status and manually turn on the ELT (i.e., activate) for testing and reset
(i.e., deactivate) the ELT. See Figure 3.
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NOTE: The ELT CANNOT be disarmed or disabled from the cockpit. Cockpit operation is limited to
deactivating or manually activating the ELT.
25-62-10
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
C406-1 (453-5002), C406-1HM (453-5003)
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Figure 3 Cockpit Remote Switch
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3) The buzzer (i.e., horn) provides an audible alert when the ELT is active. See Figure 4.
Figure 4 Buzzer
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4) The battery pack for the C406-1 Series ELT consists of four “D” size lithium manganese dioxide cells
connected in series. To prevent the cells from being charged, diodes are connected across each cell and
fuses are connected to the output. See Figure 5 Battery Pack Assembly.
Figure 5 Battery Pack Assembly
5) Four single-input antennas are approved for use with the C406-1 Series ELT:
a) One rod antenna, Artex Part #110-338.
b) Two blade antennas, Artex Part #110-340 and 110-341.
c) One whip antenna, Artex Part #110-343
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Page 19 of 67
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Figure 6 Antennas
TASK 25-62-10-870-802
2. Operation
SUBTASK 25-62-10-870-001
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A. Operational Overview
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
C406-1 (453-5002), C406-1HM (453-5003)
6) Selection of the proper antenna is dependent upon end use, aircraft configuration and speed, and other
factors. See Figure 6.
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1) See Figure 7.
Figure 7 ELT Operational Flow Diagram
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
C406-1 (453-5002), C406-1HM (453-5003)
2) A primary feature of the C406-1 Series ELT is its simplicity of operation. As long as the ELT is connected to
the remote switch harness ELT connector, such that pins 5 and 8 are jumpered (G-switch loop), it will
activate in the event of a crash.
NOTE: Neither the cockpit remote switch or the ELT local switch can be positioned in such a
manner as to prevent automatic activation when the ELT is connected properly.
3) ELT operation is designed to prevent human error and misuse in regards to automatic activation. The ELT
cannot be activated by dropping, rough handling or during shipping.
4) When the ELT is activated, the presence of the emergency sweep tone and the flashing cockpit remote
switch panel LED indicates an active, normal functioning ELT. The remote switch LED must immediately
begin to flash continuously upon ELT activation.
5) The ELT is considered to be either “ACTIVE” or “INACTIVE”. When “INACTIVE”, the ELT is in a state of rest
and performs no functions. Taking the ELT from the “INACTIVE” state to the “ACTIVE” state requires a
positive switch transition from either the cockpit remote switch, ELT local switch, or G-switch.
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a) It is possible the primary G-switch or one of the auxiliary G-switches could activate the ELT in either a
fixed or rotor wing aircraft as the result of severe maneuvers or a very hard landing.
b) To take the ELT from an “ACTIVE” state back to an “INACTIVE” state, a “RESET” must occur. See
SUBTASK 25-62-10-870-004.
6) A warning buzzer is required under C126 TSO approval. The buzzer is powered by the ELT and therefore
not dependent upon the aircraft battery for operation. It is not designed to operate continuously, but
sounds at predetermined intervals and runs for shorter periods toward the end of ELT battery life.
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SUBTASK 25-62-10-870-002
B. Normal Operation
1) The cockpit remote switch is in the “ARM” position (i.e., down).
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2) The local switch on the ELT is in the “OFF” position (i.e., down).
SUBTASK 25-62-10-870-003
C. Manual Activation
1) The ELT may be manually activated by placing either the remote switch or the ELT local switch in the “ON”
position.
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SUBTASK 25-62-10-870-004
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NOTE: As long as the cockpit remote switch and the ELT local switch are in the ARM/OFF
positions respectively, the ELT will automatically activate on impact.
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D. ELT Reset
1) If the ELT is activated accidently, it will need to be reset.
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2) Reset the ELT from the cockpit by moving the remote switch to the “ON” position, waiting approximately
one second, and then moving it back to the “ARM” position. If the switch is already in the “ON” position,
move it to the “ARM” position.
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3) Reset the ELT locally by moving the switch on the ELT to the “ON” position, waiting approximately one
second, and then moving it back to the “OFF” position. If the switch is already in the “ON” position, move
it to the “OFF” position.
NOTE: The ELT cannot be reset if either the cockpit remote switch or the ELT local switch is in the
“ON” position.
25-62-10
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
C406-1 (453-5002), C406-1HM (453-5003)
SUBTASK 25-62-10-750-001
E. Functional Check
1) A monthly functional check is recommended to verify operational status of the ELT.
2) Perform this functional check in accordance with SUBTASK 25-62-10-750-01 on page 33.
TASK 25-62-10-870-803
3. Specifications
SUBTASK 25-62-10-870-001
A. Environmental and Physical
1) Table 2 lists the environmental and physical specifications of the C406-1 Series ELT.
CRITERIA
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NOTE: For automatic activation, the higher threshold of 4.5 ft/sec (2.3 g) is specified in
accordance with Eurocae ED-62. Use of the higher threshold crash sensor has been
approved by the FAA as a deviation to TSO C126 (FAA Reference #98-130S-108, February
6, 1998).
PARAMETER
CHARACTERISTIC
Storage
-55° C to +85° C
Temperature
Operating
Shock
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Crashworthiness
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Vibration
-20° C to +55° C
500 g for 4 ms
100 g for 23 ms
Humidity
95% for 50 hours
Penetration
55 lbs from 6 in. (25 kg from 15 cm)
Crush
1,000 lbs (454 kg)
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Mechanical
10 g, 5 Hz to 2,000 Hz
55,000 ft (16,764 m)
C406-1 Series (Primary G-Switch)
4.5 ±0.5 ft/sec (2.3 g)
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Altitude
Automatic Activation
12 g
ELT Complete w/Battery Pack, Mounting
Tray, and Covers
4.25 lbs (1.9 kg)
ELT Complete w/Battery Pack, Mounting
Tray, and Covers
11.63 x 3.90 x 3.76 in.
(295 x 99 x 96 mm)
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C-406-1HM (Auxiliary Five G-Switches)
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Weight
Dimensions (LxHxW)
Software
In accordance with RTCA/DO-178B, Level D
Table 2 Environmental and Physical Specifications
25-62-10
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Feb 28/2019
ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
C406-1 (453-5002), C406-1HM (453-5003)
B. Electrical
1) Table 3 lists the electrical specifications of the C406-1 Series ELT.
CRITERIA
PARAMETER
CHARACTERISTIC
406.025 MHz
± 2 KHz (Initial)
± 5 KHz (5 years)
2 parts/10E9 in 100 ms
406.028 MHz, or higher
± 1 KHz
121.5 and 243.0 MHz
± 0.005%
Operating Frequencies
406 MHz
Bi-Phase L (G1D)
121.5 and 243.0 MHz
Amplitude Modulation (A3X)
440 ms (± 1%), or
520 ms (± 1%), every
50 seconds (± 5%)
Continuous
5 W (37 ± 2 dB) PERP, or
EIRP for 24 hrs @ -20° to +55° C
Min. 50 mW (17 dBm) PERP for 50 hrs
@ -20° to +55° C or 100 mW EIRP (20
dBm) for 48 hrs @ -20° to +55° C
20 KHz max.
406 MHz
Transmitter Duty Cycle
121.5 and 243.0 MHz
406 MHz
Peak Effective Radiated
Power (PERP)
406 MHz
Occupied Bandwidth
121.5 and 243.0 MHz
25 KHz max.
406 MHz
Per RTCA/DO-204
121.5 and 243.0 MHz
Per CFR Title 47 (FCC), Part 87
Type of Cell
Lithium Manganese Dioxide
Voltage
12.0
Amp-Hour Rating
10.0
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Spurious Emissions
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121.5 and 243.0 MHz
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Modulation
Battery
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Table 3 Electrical Specifications
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ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
C406-1 (453-5002), C406-1HM (453-5003)
SUBTASK 25-62-10-870-003
C. Antennas
1) Table 4 lists the specifications of the antennas approved for use with the C406-1 Series ELT.
CHARACTERISTIC
PARAMETERS
Style
110-338
110-340
110-341
110-343
Rod
Blade
Blade
Whip
Frequencies
121.5, 243.0, 406 MHz
121.5/243.0 MHz 1.75:1 or better
406 MHz - 1.5:1 or
better
VSWR
121.5/243.0 MHz 2.5:1 or less
406 MHz - 1.5:1 or
less
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121.5 and 243.0 MHz - 2.0:1 Max.
406 MHz - 1.5:1 Max.
Polarization
Vertical Monopole
Radiation Pattern
121.5 and 243.0 MHz - Omnidirectional 406 MHz - Hemispherical
Impedance (ohms)
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50 Nominal
0.45 lbs (0.20 kg)
1.40 lbs (0.64 kg)
Drag
2.9 lbs (1.3 kg) @ 350
KTS, 25,000 ft
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Weight
Coax Cable
1.3 lbs (0.6 kg)
@ 241 KTS EAS
0.80 lbs (0.36 kg)
0.31 lbs (0.14 kg)
8 lbs (3.6 kg) @
350 KTS EAS
Minimal
RG-142
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Dimensions
(Base-to-Tip)
7.75 in. (19.7 cm)
10.1 in. (25.7 cm)
17.1 in. 43.4 cm)
Table 4 Antenna Specifications
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15.5 in. (39.4 cm)
BNC Female
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Lights Index
Lights (tab)
737 Flight Crew Operations Manual
Lights
Chapter Lights
Index
Section Index
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A
A/P ................................................................4.1
A/T ................................................................4.1
AFT - Cargo Fire and FIRE WARN......................8.16
AFT CARGO .....................................................1.4
AFT ENTRY ......................................................1.8
AFT SERVICE ................................................. 1.14
AIR STAIR.......................................................1.1
ALIGN and FAULT - IRS................................. 11.12
ALT DISAGREE............................................. 10.20
ALTN - EEC ................................................... 7.14
ANTISKID INOP ............................................. 14.1
AOA DISAGREE............................................ 10.23
APU BOTTLE DISCHARGED ............................. 8.14
APU - Fire and FIRE WARN ................................8.1
APU DET INOP ...............................................8.14
AUTO BRAKE DISARM ..................................... 14.3
AUTO FAIL ......................................................2.4
AUTO SLAT FAIL ..............................................9.6
AUTO UNLK .....................................................1.3
AUX PITOT ......................................................3.6
B
BATTERY DISCHARGE .......................................6.1
BLEED TRIP OFF...............................................2.8
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
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D6-27370-8AS-NOK
Lights.Index.1
Lights.Index.2
737 Flight Crew Operations Manual
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C
CABIN ALTITUDE............................................. 2.1
CAPT PITOT .................................................... 3.6
Cargo Fire Bottle Discharged............................8.19
CDS FAULT.................................................. 10.23
CONFIG (Airplanes with Center Tank
Auto Shutoff) .............................................12.1
COWL ANTI-ICE .............................................. 3.1
COWL VALVE OPEN - Engine Anti-ice.................. 3.2
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D
DC FAIL ...................................................... 11.11
DETECTOR FAULT...........................................8.19
DISCH ..........................................................8.19
DISPLAYS CONTROL PANEL ........................... 10.25
DRIVE............................................................ 6.1
DSPLY SOURCE ............................................ 10.26
DUAL BLEED ..................................................2.13
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ELEC ............................................................. 6.2
ELT ............................................................... 1.6
ENG 1 OVERHEAT............................................ 8.7
ENG 2 OVERHEAT............................................ 8.7
ENG FAIL (both).............................................. 7.6
ENG FAIL (single) ...........................................7.16
Engine 1 - Fire and FIRE WARN ......................... 8.2
Engine 2 - Fire and FIRE WARN ......................... 8.2
ENGINE CONTROL ..........................................7.15
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
Lights.Index.2
D6-27370-8AS-NOK
March 31, 2023
Lights.Index.3
737 Flight Crew Operations Manual
Engine Fire Bottle Discharged L/R..................... 8.20
EQUIP ............................................................1.9
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F
F/O PITOT .......................................................3.6
FAULT - APU.................................................. 7.11
FAULT - Engine Fire/Overheat Detector ............. 8.19
FAULT - IRS ................................................ 11.12
FAULT and ALIGN - IRS................................. 11.12
FEEL DIFF PRESS .............................................9.7
FILTER BYPASS.............................................. 12.5
FIRE WARN and AFT - Cargo Fire......................8.16
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FIRE WARN and APU - Fire ................................8.1
FIRE WARN and Engine 1 - Fire ..........................8.2
FIRE WARN and Engine 2 - Fire ..........................8.2
FIRE WARN and FWD - Cargo Fire .................... 8.16
FIRE WARN and WHEEL WELL - Fire.................. 8.26
FLAP LOAD RELIEF ...........................................9.7
FMC - CDU Alerting ........................................ 11.9
FMC - FMC DISAGREE - VERTICAL .................... 11.3
FMC - FMC DISAGREE ..................................... 11.2
FMC - FMC FAIL (With Dual FMC Option) ........... 11.6
FMC - FMC FAIL (With Single FMC Option) .........11.4
FMC and MSG - CDU Alerting ........................... 11.9
FMC and MSG - FMC DISAGREE - VERTICAL....... 11.3
FMC and MSG - FMC DISAGREE........................ 11.2
FMC DISAGREE - VERTICAL ............................. 11.3
FMC DISAGREE .............................................. 11.2
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
Lights.Index.3
Lights.Index.4
737 Flight Crew Operations Manual
FWD
FWD
FWD
FWD
- Cargo Fire and FIRE WARN.....................8.16
CARGO ................................................... 1.4
ENTRY .................................................... 1.8
SERVICE................................................1.14
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G
GEN OFF BUS, SOURCE OFF and TRANSFER BUS OFF
(both sides) ................................................ 6.3
GLS ..............................................................11.9
GPS............................................................ 11.10
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I
IAS DISAGREE ............................................. 10.28
ILS............................................................. 11.10
IMBAL......................................................... 12.15
INOP - Ground Proximity .................................15.3
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L
L ALPHA VANE ................................................ 3.6
L BOTTLE DISCHARGED ..................................8.20
L ELEV PITOT.................................................. 3.6
L VALVE OPEN - Wing Anti-ice..........................3.10
L VALVE OPEN - Wing Anti-ice........................... 3.8
LE FLAPS TRANSIT .........................................9.12
LEFT AFT OVERWING ......................................1.12
LEFT FWD OVERWING.....................................1.12
LEFT GEAR ....................................................14.6
LOCK FAIL.....................................................1.12
LOW OIL PRESSURE - APU...............................7.12
LOW OIL PRESSURE - Engine ...........................7.30
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
Lights.Index.4
D6-27370-8AS-NOK
March 31, 2023
Lights.Index.5
737 Flight Crew Operations Manual
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LOW PRESSURE - Flight Control .........................9.8
LOW PRESSURE - Fuel Pump ......................... 12.12
LOW PRESSURE - Hydraulic Pump - Standby.... 13.18
LOW PRESSURE - Hydraulic Pump System A (both) ......................................... 13.3
LOW PRESSURE - Hydraulic Pump System A and B ........................................ 13.12
LOW PRESSURE - Hydraulic Pump System B (both) ......................................... 13.6
LOW PRESSURE - Hydraulic Pump (single) .........13.1
LOW QUANTITY ........................................... 13.18
LOW ........................................................... 12.18
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MACH TRIM FAIL ............................................ 9.16
MSG and FMC - CDU Alerting ........................... 11.9
MSG and FMC - FMC DISAGREE - VERTICAL....... 11.3
MSG and FMC - FMC DISAGREE........................ 11.2
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NO AUTOLAND.................................................4.1
NO LAND 3......................................................4.2
NOSE GEAR................................................... 14.6
NOT ARMED ....................................................1.7
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OFF - Equipment Cooling................................. 2.14
OFF - Flight Recorder.................................... 10.27
OFF SCHED DESCENT ..................................... 2.14
OIL FILTER BYPASS ........................................ 7.32
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ON DC ........................................................ 11.14
OVER SPEED - APU .........................................7.12
OVERHEAT - Hydraulic Pump ...........................13.2
OVERHEAT - Window ....................................... 3.6
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PACK ............................................................2.16
PASS OXY ON - Chemical oxygen .....................1.13
PSEU ............................................................15.4
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R ALPHA VANE ................................................ 3.6
R BOTTLE DISCHARGED ..................................8.20
R ELEV PITOT ................................................. 3.6
R VALVE OPEN - Wing Anti-ice .........................3.10
R VALVE OPEN - Wing Anti-ice .......................... 3.8
REV ..............................................................7.43
REVERSER.....................................................7.42
RIGHT AFT OVERWING....................................1.12
RIGHT FWD OVERWING ..................................1.12
RIGHT GEAR..................................................14.6
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SOURCE OFF (both)......................................... 6.3
SOURCE OFF (single) ......................................6.10
SOURCE OFF, TRANSFER BUS OFF and GEN OFF BUS
(both sides) ................................................ 6.3
SPEED BRAKE DO NOT ARM - Without Load Alleviation
System......................................................9.16
SPEED TRIM FAIL ...........................................9.17
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SPEEDBRAKES EXTENDED ............................... 9.18
STAB OUT OF TRIM ........................................ 9.20
STANDBY PWR OFF ........................................ 6.12
START VALVE OPEN........................................ 7.44
STBY RUD ON ................................................ 9.26
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TAI ................................................................3.2
TAKEOFF CONFIG...........................................15.1
TEMP PROBE ...................................................3.6
TR UNIT........................................................ 6.12
TRANSFER BUS OFF........................................ 6.14
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sides)..........................................................6.3
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UNABLE REQD NAV PERF - RNP (FMC Update U10.7
and Later)................................................ 11.16
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VALVE OPEN - Crossfeed ................................. 12.2
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WHEEL WELL - Fire and FIRE WARN.................. 8.26
WING-BODY OVERHEAT .................................. 2.20
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YAW DAMPER ................................................ 9.44
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ZONE TEMP ................................................... 2.26
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Unannunciated
Chapter Unann
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Section Index
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Aborted Engine Start.....................................7.1
ACARS Electrical Power Loss ..............................5.1
ACARS MU Fail or DU Fail ..................................5.1
ADS-B Out Failure .......................................... 11.1
Airspeed Unreliable..................................... 10.1
Airspeed Unreliable (Stick Shaker Deactivation
by Pulling Circuit Breaker)..................... 10.10
All Flaps Up Landing .........................................9.4
Brake Pressure Indicator Zero PSI .................... 14.5
Cabin Temperature Hot .....................................2.9
Display Failure ............................................. 10.24
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Ditching ..........................................................0.4
Elevator Tab Vibration ......................................9.6
Emergency Descent........................0.1
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Engine Failure or Shutdown ............................. 7.16
Engine Fire on the Ground ............ Back Cover.2
Engine High Oil Temperature ........................... 7.20
Engine High Vibration ..................................... 7.24
Engine In-Flight Start ..................................... 7.26
Engine Limit or Surge or Stall .......................7.2
ENGINE LOW OIL PRESSURE ........................... 7.30
Engine Severe Damage or Separation ...........8.2
Engine Tailpipe Fire ......................................8.8
Evacuation ..................... Back Cover.4
Fuel Leak Engine ............................................ 12.6
Fuel Quantity Indication Inoperative ............... 12.13
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Fuel Temperature Low .................................. 12.14
Ice Crystal Icing.............................................. 3.3
Jammed or Restricted Flight Controls ................. 9.8
Landing Gear Lever Jammed in the Up Position. 14.10
Landing Gear Lever Will Not Move Up After Takeoff ...
14.14
Loss Of Thrust On Both Engines ....................7.6
Manual Gear Extension.................................. 14.18
One Engine Inoperative Landing .......................7.34
One Engine Inoperative Landing .......................7.38
Overspeed.....................................................15.3
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Partial or All Gear Up Landing ........................ 14.20
Radio Transmit Continuous (Stuck Microphone Switch)
5.2
Rapid Depressurization ................ 2.1
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Smoke or Fumes Removal ...............................8.22
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Smoke, Fire or Fumes.................. 8.10
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Stabilizer Trim Inoperative ..............................9.22
Tail Strike .....................................................15.5
Trailing Edge Flap Asymmetry ..........................9.27
Trailing Edge Flap Disagree..............................9.32
Trailing Edge Flaps Up Landing.........................9.40
Unscheduled Pressurization Change ................... 2.4
Volcanic Ash ..................................................7.46
Window Damage - Forward (L1, L2, R1, R2) ......1.15
Window Damage - Heated Side (L3, R3) ............1.18
Window Damage - Unheated Side (L3, R3) ........1.22
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Window Open ................................................ 1.25
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Alphabetical Index
Alphabetical Index
737 Flight Crew Operations Manual
Alphabetical
Chapter Alpha
Index
Section Index
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A/P ................................................................4.1
A/T ................................................................4.1
Aborted Engine Start.....................................7.1
ACARS Electrical Power Loss ..............................5.1
ACARS MU Fail or DU Fail ..................................5.1
ADS-B Out Failure .......................................... 11.1
AFT - Cargo Fire and FIRE WARN......................8.16
AFT CARGO .....................................................1.4
AFT ENTRY ......................................................1.8
AFT SERVICE ................................................. 1.14
Airspeed Unreliable..................................... 10.1
Airspeed Unreliable (Stick Shaker Deactivation
by Pulling Circuit Breaker)..................... 10.10
AIRSTAIR .......................................................1.1
ALIGN and FAULT - IRS................................. 11.12
All Flaps Up Landing .........................................9.4
ALT DISAGREE ............................................ 10.20
ALTN - EEC ................................................... 7.14
ANTISKID INOP ............................................. 14.1
ANTISKID INOPERATIVE ................................ 14.1
AOA DISAGREE ........................................... 10.23
APU - Fire and FIRE WARN ................................8.1
APU BOTTLE DISCHARGED ............................. 8.14
APU DET INOP ...............................................8.14
APU DETECTION INOPERATIVE ....................... 8.14
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APU FAULT ...................................................7.11
APU FIRE .................................................... 8.1
APU LOW OIL PRESSURE ................................7.12
APU OVERSPEED ...........................................7.12
AUTO BRAKE DISARM ....................................14.3
AUTO FAIL ..................................................... 2.4
AUTO SLAT FAIL ............................................. 9.6
AUTO UNLK .................................................... 1.3
AUTOMATIC UNLOCK ...................................... 1.3
AUTOPILOT DISENGAGE .................................. 4.1
AUTOTHROTTLE DISENGAGE ........................... 4.1
AUX PITOT ..................................................... 3.6
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BATTERY DISCHARGE ..................................... 6.1
BATTERY DISCHARGE ...................................... 6.1
BLEED TRIP OFF ............................................. 2.8
Brake Pressure Indicator Zero PSI ....................14.5
CABIN ALTITUDE WARNING .......... 2.1
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CABIN ALTITUDE............................................. 2.1
Cabin Temperature Hot .................................... 2.9
CAPT PITOT .................................................... 3.6
CARGO DOOR ................................................ 1.4
CARGO FIRE .................................................8.16
Cargo Fire Bottle Discharged............................8.19
CARGO FIRE DETECTOR FAULT .......................8.19
CDS FAULT ................................................. 10.23
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CONFIG ....................................................... 12.1
COWL ANTI-ICE ...............................................3.1
COWL VALVE OPEN - Engine Anti-ice ..................3.2
CROSSFEED SELECTOR INOPERATIVE .............. 12.2
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DC FAIL ...................................................... 11.11
DETECTOR FAULT...........................................8.19
DISCH ......................................................... 8.19
Display Failure ............................................. 10.24
DISPLAY SOURCE ........................................ 10.26
DISPLAYS CONTROL PANEL .......................... 10.25
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Ditching ..........................................................0.4
DRIVE ...........................................................6.1
DSPLY SOURCE............................................ 10.26
DUAL BLEED ................................................. 2.13
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EEC ALTERNATE MODE .................................. 7.14
ELEC .............................................................6.2
Elevator Tab Vibration ......................................9.6
ELT ...............................................................1.6
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Emergency Descent........................0.1
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EMERGENCY EXIT LIGHTS NOT ARMED ..............1.7
ENG 1 OVERHEAT.............................................8.7
ENG 2 OVERHEAT.............................................8.7
ENG FAIL (both) ..............................................7.6
ENG FAIL (single)...........................................7.16
Engine 1 - Fire and FIRE WARN ..........................8.2
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Engine 2 - Fire and FIRE WARN ......................... 8.2
ENGINE CONTROL .........................................7.15
ENGINE COWL ANTI-ICE ................................. 3.1
ENGINE COWL VALVE OPEN OR TAI INDICATION 3.2
Engine Failure or Shutdown .............................7.16
Engine Fire Bottle Discharged L/R .....................8.20
Engine Fire on the Ground............. Back Cover.2
ENGINE FIRE.................................................8.2
ENGINE FIRE/OVERHEAT DETECTOR FAULT ......8.19
Engine High Oil Temperature ...........................7.20
Engine High Vibration .....................................7.24
Engine In-Flight Start .....................................7.26
Engine Limit or Surge or Stall .......................7.2
ENGINE LOW OIL PRESSURE............................7.30
ENGINE OIL FILTER BYPASS ...........................7.32
ENGINE OVERHEAT .................................... 8.7
Engine Severe Damage or Separation ...........8.2
Engine Tailpipe Fire.......................................8.8
ENTRY DOOR ................................................. 1.8
EQUIP............................................................ 1.9
EQUIPMENT COOLING OFF .............................2.14
EQUIPMENT DOOR .......................................... 1.9
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Evacuation ..................... Back Cover.4
F
F/O PITOT ...................................................... 3.6
FAULT - APU ..................................................7.11
FAULT - Engine Fire/Overheat Detector .............8.19
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FAULT - IRS ................................................ 11.12
FAULT and ALIGN - IRS................................. 11.12
FEEL DIFF PRESS .............................................9.7
FEEL DIFFERENTIAL PRESSURE .........................9.7
FILTER BYPASS.............................................. 12.5
FIRE WARN and AFT - Cargo Fire......................8.16
FIRE WARN and APU - Fire ................................8.1
FIRE WARN and Engine 1 - Fire ..........................8.2
FIRE WARN and Engine 2 - Fire ..........................8.2
FIRE WARN and FWD - Cargo Fire .................... 8.16
FIRE WARN and WHEEL WELL - Fire.................. 8.26
FLAP LOAD RELIEF ..........................................9.7
FLIGHT CONTROL LOW PRESSURE .....................9.8
FLIGHT RECORDER OFF ............................... 10.27
FMC - CDU Alerting ........................................ 11.9
FMC - FMC DISAGREE - VERTICAL .................... 11.3
FMC - FMC DISAGREE ..................................... 11.2
FMC - FMC FAIL (With Dual FMC Option) ........... 11.6
FMC - FMC FAIL (With Single FMC Option) .........11.4
FMC and MSG - CDU Alerting ........................... 11.9
FMC and MSG - FMC DISAGREE - VERTICAL....... 11.3
FMC and MSG - FMC DISAGREE........................ 11.2
FMC DISAGREE - VERTICAL ............................ 11.3
FMC DISAGREE ............................................. 11.2
FMC FAIL ..................................................... 11.4
FMC FAIL ..................................................... 11.6
FMC/CDU ALERTING MESSAGE ........................ 11.9
FUEL FILTER BYPASS ..................................... 12.5
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Fuel Leak Engine ............................................12.6
FUEL PUMP LOW PRESSURE .......................... 12.12
Fuel Quantity Indication Inoperative ............... 12.13
Fuel Temperature Low .................................. 12.14
FWD - Cargo Fire and FIRE WARN.....................8.16
FWD CARGO ................................................... 1.4
FWD ENTRY .................................................... 1.8
FWD SERVICE................................................1.14
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GEAR DISAGREE ...........................................14.6
GEN OFF BUS, SOURCE OFF and TRANSFER BUS OFF
(both sides) ................................................ 6.3
GLS .............................................................11.9
GPS ........................................................... 11.10
GROUND PROXIMITY GPWS INOPERATIVE ........15.3
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HYDRAULIC PUMP LOW PRESSURE ..................13.1
HYDRAULIC PUMP OVERHEAT .........................13.2
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IAS DISAGREE ............................................ 10.28
Ice Crystal Icing.............................................. 3.3
ILS ............................................................ 11.10
IMBAL ........................................................ 12.15
INOP - Ground Proximity .................................15.3
IRS DC FAIL ............................................... 11.11
IRS FAULT .................................................. 11.12
IRS ON DC ................................................. 11.14
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J
Jammed or Restricted Flight Controls ..................9.8
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L
L ALPHA VANE .................................................3.6
L BOTTLE DISCHARGED .................................. 8.20
L ELEV PITOT ..................................................3.6
L VALVE OPEN - Wing Anti-ice..........................3.10
L VALVE OPEN - Wing Anti-ice............................3.8
L/R BOTTLE DISCHARGED .............................. 8.20
LANDING CONFIGURATION ...................... 15.1
Landing Gear Lever Jammed in the Up Position 14.10
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Landing Gear Lever Will Not Move Up After Takeoff...
14.14
LE FLAPS TRANSIT ......................................... 9.12
LEADING EDGE FLAPS TRANSIT ......................9.12
LEFT AFT OVERWING ...................................... 1.12
LEFT FWD OVERWING..................................... 1.12
LEFT GEAR .................................................... 14.6
LOCK FAIL .................................................... 1.12
LOSS OF BOTH ENGINE DRIVEN GENERATORS ....6.3
LOSS OF SYSTEM A ....................................... 13.3
LOSS OF SYSTEM A AND SYSTEM B ................ 13.12
LOSS OF SYSTEM B ....................................... 13.6
Loss Of Thrust On Both Engines ....................7.6
LOW .......................................................... 12.18
LOW OIL PRESSURE - APU............................... 7.12
LOW OIL PRESSURE - Engine ........................... 7.30
LOW PRESSURE - Flight Control .........................9.8
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LOW PRESSURE - Fuel Pump.......................... 12.12
LOW PRESSURE - Hydraulic Pump - Standby .... 13.18
LOW PRESSURE - Hydraulic Pump System A (both) .........................................13.3
LOW PRESSURE - Hydraulic Pump System A and B ........................................ 13.12
LOW PRESSURE - Hydraulic Pump System B (both) .........................................13.6
LOW PRESSURE - Hydraulic Pump (single) .........13.1
LOW QUANTITY............................................ 13.18
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MACH TRIM FAIL ...........................................9.16
Manual Gear Extension.................................. 14.18
MANUAL REVERSION .................................... 13.12
MSG and FMC - CDU Alerting ...........................11.9
MSG and FMC - FMC DISAGREE - VERTICAL.......11.3
MSG and FMC - FMC DISAGREE........................11.2
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NO AUTOLAND ............................................... 4.1
NO LAND 3 .................................................... 4.2
NOSE GEAR ...................................................14.6
NOT ARMED ................................................... 1.7
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OFF
OFF
OFF
OFF
- Equipment Cooling .................................2.14
- Flight Recorder .................................... 10.27
SCHED DESCENT .....................................2.14
SCHEDULE DESCENT ...............................2.14
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OIL FILTER BYPASS ........................................ 7.32
ON DC ........................................................ 11.14
One Engine Inoperative Landing ....................... 7.34
One Engine Inoperative Landing ....................... 7.38
OVER SPEED - APU......................................... 7.12
OVERHEAT - Hydraulic Pump ........................... 13.2
OVERHEAT - Window ........................................3.6
Overspeed .................................................... 15.3
OVERWING DOOR ......................................... 1.12
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PACK ........................................................... 2.16
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Partial or All Gear Up Landing ........................ 14.20
PASS OXY ON - Chemical oxygen ..................... 1.13
PASSENGER OXYGEN ON ................................ 1.13
PROBE HEAT ...................................................3.6
PSEU ........................................................... 15.4
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R ALPHA VANE .................................................3.6
R BOTTLE DISCHARGED.................................. 8.20
R ELEV PITOT ..................................................3.6
R VALVE OPEN - Wing Anti-ice ......................... 3.10
R VALVE OPEN - Wing Anti-ice ...........................3.8
Radio Transmit Continuous (Stuck Microphone Switch)
5.2
Rapid Depressurization ................. 2.1
REV.............................................................. 7.43
REVERSER .................................................... 7.42
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REVERSER UNLOCKED (IN FLIGHT) .................7.43
RIGHT AFT OVERWING....................................1.12
RIGHT FWD OVERWING ..................................1.12
RIGHT GEAR..................................................14.6
Runaway Stabilizer .......................................9.1
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SERVICE DOOR .............................................1.14
Smoke or Fumes Removal ...............................8.22
Smoke, Fire or Fumes.................. 8.10
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SOURCE OFF ................................................6.10
SOURCE OFF (both)......................................... 6.3
SOURCE OFF, TRANSFER BUS OFF and GEN OFF BUS
(both sides) ................................................ 6.3
SPEED BRAKE DO NOT ARM ............................9.16
SPEED TRIM FAIL ..........................................9.17
SPEEDBRAKES EXTENDED ..............................9.18
STAB OUT OF TRIM ........................................9.20
STABILIZER OUT OF TRIM ..............................9.20
Stabilizer Trim Inoperative ..............................9.22
STANDBY HYDRAULIC LOW PRESSURE ........... 13.18
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STANDBY HYDRAULIC LOW QUANTITY ........... 13.18
STANDBY POWER OFF ....................................6.12
STANDBY PWR OFF.........................................6.12
STANDBY RUDDER ON ...................................9.26
START VALVE OPEN .......................................7.44
STBY RUD ON ................................................9.26
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TAI ................................................................3.2
Tail Strike ..................................................... 15.5
TAKEOFF CONFIGURATION ...................... 15.1
TEMP PROBE ...................................................3.6
TR UNIT ....................................................... 6.12
Trailing Edge Flap Asymmetry ..........................9.27
Trailing Edge Flap Disagree ............................. 9.32
Trailing Edge Flaps Up Landing......................... 9.40
TRANSFER BUS OFF ....................................... 6.14
TRANSFER BUS OFF, SOURCE OFF and GEN OFF (both
sides)..........................................................6.3
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UNABLE REQD NAV PERF - RNP ..................... 11.16
Unscheduled Pressurization Change ....................2.4
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VALVE OPEN - Crossfeed ................................. 12.2
Volcanic Ash .................................................. 7.46
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WARNING HORN (INTERMITTENT) .......... 15.2
WARNING LIGHT - CABIN ALTITUDE OR
TAKEOFF CONFIGURATION ................... 15.2
WHEEL WELL - Fire and FIRE WARN.................. 8.26
WHEEL WELL FIRE ......................................... 8.26
Window Damage - Forward (L1, L2, R1, R2) ...... 1.15
Window Damage - Heated Side (L3, R3)............ 1.18
Window Damage - Unheated Side (L3, R3) ........ 1.22
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Window Open ................................................1.25
WINDOW OVERHEAT ...................................... 3.6
WING ANTI-ICE VALVE OPEN ..........................3.10
WING ANTI-ICE VALVE OPEN ........................... 3.8
WING-BODY OVERHEAT .................................2.20
Y
YAW DAMPER ...............................................9.44
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ZONE TEMP ..................................................2.26
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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737 Flight Crew Operations Manual
Normal Checklists
Chapter NC
Normal
File
Highlight
Checklists
PREFLIGHT
Oxygen. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Tested, 100%
or
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Navigation transfer
and display switches . . . . . . . . . . . . . . . . . . . . NORMAL, AUTO
Window heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
Pressurization mode
selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
Flight instruments . . . . . . . . . . . . . Heading ___, Altimeter ___
ad
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Parking brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Set
Engine start levers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
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BEFORE START
Flight deck door . . . . . . . . . . . . . . . . . . . . . . Closed and locked
Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___ KGS, Pumps ON
if
Passenger signs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___
d
Windows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Locked
on
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MCP . . . . . . . . . . . . . . . . V2 ___, HEADING ___, ALTITUDE ___
Takeoff speeds . . . . . . . . . . . . . . . . . . . . V1 ___, VR ___, V2 ___
CDU preflight. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Completed
nc
Rudder and aileron trim . . . . . . . . . . . . . . . . . . . . . . . Free and 0
U
Taxi and takeoff briefing . . . . . . . . . . . . . . . . . . . . . . Completed
Anti-collision light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
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Normal Checklists
737 Flight Crew Operations Manual
BEFORE TAXI
Generators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On
Probe heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Anti-ice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___
or
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Isolation valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
Engine start switches. . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONT
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .RTO
Engine start levers . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE detent
ad
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Flight controls. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
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Ground equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Clear
BEFORE TAKEOFF
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___, Green light
if
Stabilizer trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___ Units
d
AFTER TAKEOFF
on
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Engine bleeds . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Packs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP and OFF
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Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP, No lights
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DESCENT
Pressurization . . . . . . . . . . . . . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___
or
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Landing data . . . . . . . . . . . . . . . . . . . .VREF ___, Minimums ___
Approach briefing. . . . . . . . . . . . . . . . . . . . . . . . . . . . Completed
APPROACH
ad
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Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___
LANDING
Engine start switches. . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONT
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Speedbrake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ARMED
Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Down
SHUTDOWN
d
if
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___, Green light
on
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Fuel pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Probe heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
Hydraulic panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Set
nc
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
U
Parking brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Engine start levers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
Weather radar . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
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Normal Checklists
737 Flight Crew Operations Manual
SECURE
IRSs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Emergency exit lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Window heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
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Packs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
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NNC.0-Miscellaneous
Non-Normal
0
Miscellaneous
Checklists
(tab)
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Miscellaneous
Section 0
Table of Contents
Emergency Descent........................0.1
NNC. 3
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Ditching ..........................................................0.4
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Emergency Descent........................0.1
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Non-Normal Checklists Miscellaneous
737 Flight Crew Operations Manual
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0.1
737 Flight Crew Operations Manual
File Highlight
Miscellaneous
Emergency Descent
Condition:
One or more of these occur:
•Cabin altitude cannot be controlled
•A rapid descent is needed.
or
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1 Announce the emergency descent. The pilot flying
will advise the cabin crew, on the PA system, of
impending rapid descent. The pilot monitoring will
advise ATC and obtain the area altimeter setting.
2 Passenger signs . . . . . . . . . . . . . . . . . . . . . . ON
ad
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3 Without delay, descend to the lowest safe
altitude or 10,000 feet, whichever is higher.
4 ENGINE START switches (both) . . . . . . . . . CONT
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5 Thrust levers (both) . . . . . . . . . Reduce thrust to
minimum or as
needed for anti-ice
6 Speedbrake . . . . . . . . . . . . . . . . FLIGHT DETENT
on
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if
If structural integrity is in doubt, limit speed as
much as possible and avoid high maneuvering
loads.
Set target speed to Mmo/Vmo.
7
-----------------------
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8 When approaching the level off altitude:
Smoothly lower the SPEED BRAKE lever to the
DOWN detent and level off. Add thrust and
stabilize on altitude and airspeed.
▼ Continued on next page ▼
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0.2
737 Flight Crew Operations Manual
▼Emergency Descent continued▼
9 Crew oxygen regulators. . . . . . . . . . . . . . Normal
Flight crew must use oxygen when cabin altitude
is above 10,000 feet. To conserve oxygen, move
the regulator to Normal.
or
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10 ENGINE START switches (both) . . . . . .As needed
11 The new course of action is based on weather,
oxygen, fuel remaining and available airports. Use
of long range cruise may be needed.
12 Choose one:
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►►Go to step 13
ad
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Pressurization mode selector is in MAN:
Pressurization mode selector is not in MAN:
■■■■
if
13 Checklist Complete Except Deferred Items
d
Deferred Items
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Descent Checklist
U
nc
Use momentary actuation of the outflow valve
switch to avoid large and rapid pressurization
changes.
Pressurization . . . . . Move to OPEN or CLOSE
as needed to control
cabin altitude and rate
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing data . . . . . . . . . VREF ___, Minimums ___
▼ Continued on next page ▼
0.2
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737 Flight Crew Operations Manual
▼Emergency Descent continued▼
Approach briefing . . . . . . . . . . . . . . . . Completed
Approach Checklist
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Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
At Pattern Altitude
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Landing Checklist
ad
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Outflow VALVE switch . . . . . . . Move to OPEN until
the outflow VALVE
indication shows fully open
to depressurize the airplane
ENGINE START switches . . . . . . . . . . . . . . . CONT
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
if
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
■■■■
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Flaps . . . . . . . . . . . . . . . . . . . . . ___, Green light
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0.4
737 Flight Crew Operations Manual
Ditching
Condition:
Airplane ditching and evacuation are
needed.
or
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1 Send distress signals. Determine position, course,
speed, altitude, situation, intention, time and
position of intended touchdown and transmit
mayday. Report type of aircraft and request
intercept.
2 Alert the cabin crew to prepare for ditching and
seat passengers as far forward as possible.
ad
ed
3 Burn off fuel to reduce touchdown speed and
increase buoyancy.
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4 Plan to touch down on the windward side and
parallel to waves and swells.
6 Set VREF 40.
if
5 Plan a flaps 40 landing unless another configuration
is needed.
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7 Do not arm the autobrake.
8 Do not accomplish the normal landing checklist.
9 Checklist Complete Except Deferred Items
nc
Deferred Items
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Descent Checklist
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
Landing data . . . . . . . . . . . . . . . . . VREF 40 ___
▼ Continued on next page ▼
0.4
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737 Flight Crew Operations Manual
▼Ditching continued▼
Approach briefing . . . . . . . . . . . . . . . . Completed
Approach Checklist
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Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Below 5000 feet
LANDING GEAR AURAL WARN
circuit breaker (P6-3:D18) . . . . . . . . . . . . . . . Pull
ad
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This prevents the warning horn with gear
retracted and landing flaps selected.
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The flight deck chime for an incoming call from
the cabin crew is unavailable.
Passenger signs . . . . . . . . . . . . . . . . . . . . . . . ON
Engine BLEED air switches (both) . . . . . . . . . . OFF
on
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if
This allows the airplane to be depressurized with
the outflow valve closed.
Pressurization mode selector . . . . . . . . . . . . . MAN
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Outflow VALVE switch . . . . . . . . . . . Hold in CLOSE
until the outflow VALVE
indication shows fully closed
This prevents water from entering the airplane.
Note: The outflow valve takes up to 20 seconds to
close.
APU switch . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
GROUND PROXIMITY GEAR
INHIBIT switch . . . . . . . . . . . . . . . . GEAR INHIBIT
▼ Continued on next page ▼
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0.5
0.6
737 Flight Crew Operations Manual
▼Ditching continued▼
GROUND PROXIMITY TERR
INHIBIT switch . . . . . . . . . . . . . . . . TERR INHIBIT
Life vests, shoulder harnesses and seat belts . . . On
or
pr
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Confirm that passenger cabin preparations are
complete.
Caution! Do not open aft entry or service doors
as they may be partially submerged.
ad
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Transmit all pertinent information regarding final
ditching position.
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After Impact Procedure Review
Set both engine start levers to CUTOFF. This closes
fuel shutoff valves to prevent discharge of fuel from
ruptured fuel lines.
on
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if
Open flight deck windows. This ensures no cabin
differential pressure prevents the opening of the
doors or emergency exits.
Start the evacuation.
nc
Proceed to assigned ditching stations, launch rafts
and evacuate the airplane as soon as practicable.
U
The airplane may stay afloat indefinitely if fuel load
is minimal and no serious damage was sustained
during landing.
Ditching Final
LANDING GEAR lever. . . . . . . . . . . . . . UP and OFF
▼ Continued on next page ▼
0.6
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737 Flight Crew Operations Manual
▼Ditching continued▼
Flaps . . . . . . . . . . . . . . . . . . . . . ___, Green light
At 500 feet, advise the cabin crew that ditching is
imminent.
or
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At 50 feet, advise the cabin crew to brace for
impact.
Maintain airspeed at VREF. Flare the airplane to
achieve the minimum rate of descent at touchdown.
Maintain 200-300 fpm rate of descent until the start
of the flare.
ad
ed
At flare, rotate smoothly to a touchdown attitude of
10-12°. Maintain airspeed and rate of descent with
thrust.
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At touchdown, reduce thrust to idle.
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1 Airplane Gen., Gen.,
NNC.1-Airplane
Emer.Emer.
Equip.,Equip.,
Doors,Doors,
Windows
Windows
(tab)
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Airplane Gen., Emer. Equip., Doors, Windows
Section 1
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Table of Contents
AIRSTAIR........................................................1.1
AUTOMATIC UNLOCK ........................................1.3
CARGO DOOR ..................................................1.4
ELT ................................................................1.6
EMERGENCY EXIT LIGHTS NOT ARMED ...............1.7
ENTRY DOOR ...................................................1.8
EQUIPMENT DOOR ...........................................1.9
LOCK FAIL..................................................... 1.12
OVERWING DOOR .......................................... 1.12
PASSENGER OXYGEN ON................................. 1.13
SERVICE DOOR.............................................. 1.14
Tail Strike .............................................................. ►►15.5
Window Damage - Forward (L1, L2, R1, R2) ...... 1.15
Window Damage - Heated Side (L3, R3)............ 1.18
Window Damage - Unheated Side (L3, R3) ........ 1.22
Window Open ................................................ 1.25
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1.TOC.1
Non-Normal Checklists Airplane Gen., Emer. Equip.,
Doors, Windows
737 Flight Crew Operations Manual
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1.1
737 Flight Crew Operations Manual
Airplane
File
AIR
Highlight
STAIR
General, Emer. Equip., Doors, Windows
AIR
STAIR
AIRSTAIR
YK820
Condition:
The airstair door is not secure.
Pressurization is normal:
or
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1 Choose one:
The door is in a safe configuration.
Continue normal operation.
■■■■
ad
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Pressurization is not normal:
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►►Go to step 2
2 Don oxygen masks.
3 Establish crew communications.
4 Passenger signs . . . . . . . . . . . . . . . . . . . . . . ON
if
5 Choose one:
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Airplane has reached the planned cruise altitude:
►►Go to step 6
U
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Airplane has not reached the planned cruise
altitude:
Do not continue the climb.
Reset the FLT ALT indicator to the actual
airplane altitude.
►►Go to step 6
6 LAND ALT indicator . . . . . . . . . . . . . . . 9000 feet
▼ Continued on next page ▼
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1.1
1.2
737 Flight Crew Operations Manual
▼AIRSTAIR continued▼
7 Choose one:
Minimum safe altitude is at or below 9,000
feet:
or
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►►Go to step 8
Minimum safe altitude is between 9,000 feet
and 13,000 feet:
►►Go to step 10
ad
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Minimum safe altitude is at or above 13,000
feet:
►►Go to step 12
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8 Descend to 9,000 feet.
9 Maintain a cabin differential pressure of 0 psi by
limiting flight altitude to 9,000 feet.
if
►►Go to step 15
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10 Descend to the minimum safe altitude.
11 LAND ALT indicator . . . . . Select a higher altitude
(maximum 13,000 feet) to
maintain a cabin differential
pressure of 0 psi
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Note: The intermittent cabin altitude/configuration
warning horn will sound and the CABIN
ALTITUDE lights (if installed and operative)
will illuminate at a cabin altitude of
approximately 10,000 feet.
►►Go to step 15
▼ Continued on next page ▼
1.2
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737 Flight Crew Operations Manual
▼AIRSTAIR continued▼
12 Descend to the minimum safe altitude.
13 Pressurization mode selector . . . . . . . . . . . . MAN
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Use momentary actuation of the outflow valve
switch to avoid large and rapid pressurization
changes.
14 Outflow VALVE switch . . . . Move to OPEN until
the outflow VALVE
indication shows fully open
to depressurize the airplane
Note: The intermittent cabin altitude/configuration
warning horn will sound and the CABIN
ALTITUDE lights (if installed and operative)
will illuminate at a cabin altitude of
approximately 10,000 feet.
15 Plan to land at the nearest suitable airport.
16 When the cabin altitude is at or below 10,000 feet:
on
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Oxygen masks may be removed.
■■■■
AUTO UNLK
AUTO
UNLK
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Condition:
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Objective:
AUTOMATIC UNLOCK
The correct emergency access code is
entered.
To deny unauthorized access to the flight
deck before the door automatically unlocks.
1 FLT DK DOOR lock selector . . . . . Rotate to DENY
and hold for 1 second
■■■■
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1.3
1.4
737 Flight Crew Operations Manual
FWDCARGO
AFT
CARGO
CARGO DOOR
Condition:
AFT
CARGO
One or more cargo doors are not closed and
secure.
1 Choose one:
Pressurization is normal:
or
pr
in
te
d
FWD
CARGO
The door is in a safe configuration.
Continue normal operation.
ad
ed
■■■■
Pressurization is not normal:
do
w
nl
o
►►Go to step 2
2 Don oxygen masks.
3 Establish crew communications.
if
4 Passenger signs . . . . . . . . . . . . . . . . . . . . . . ON
on
tro
lle
d
5 Choose one:
Airplane has reached the planned cruise altitude:
►►Go to step 6
U
nc
Airplane has not reached the planned cruise
altitude:
Do not continue the climb.
Reset the FLT ALT indicator to the actual
airplane altitude.
►►Go to step 6
▼ Continued on next page ▼
1.4
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1.5
737 Flight Crew Operations Manual
▼CARGO DOOR continued▼
6 LAND ALT indicator . . . . . . . . . . . . . . . 9000 feet
7 Choose one:
►►Go to step 8
or
pr
in
te
d
Minimum safe altitude is at or below 9,000
feet:
Minimum safe altitude is between 9,000 feet
and 13,000 feet:
ad
ed
►►Go to step 10
Minimum safe altitude is at or above 13,000
feet:
do
w
nl
o
►►Go to step 12
8 Descend to 9,000 feet.
if
9 Maintain a cabin differential pressure of 0 psi by
limiting flight altitude to 9,000 feet.
on
tro
lle
d
►►Go to step 15
10 Descend to the minimum safe altitude.
U
nc
11 LAND ALT indicator . . . . . .Select a higher altitude
(maximum 13,000 feet) to
maintain a cabin differential
pressure of 0 psi
Note: The intermittent cabin altitude/configuration
warning horn will sound and the CABIN
ALTITUDE lights (if installed and operative)
will illuminate at a cabin altitude of
approximately 10,000 feet.
►►Go to step 15
▼ Continued on next page ▼
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March 26, 2015
D6-27370-8AS-NOK
1.5
1.6
737 Flight Crew Operations Manual
▼CARGO DOOR continued▼
12 Descend to the minimum safe altitude.
13 Pressurization mode selector . . . . . . . . . . . . MAN
do
w
nl
o
ad
ed
or
pr
in
te
d
Use momentary actuation of the outflow valve
switch to avoid large and rapid pressurization
changes.
14 Outflow VALVE switch. . . . . Move to OPEN until
the outflow VALVE
indication shows fully open
to depressurize the airplane
Note: The intermittent cabin altitude/configuration
warning horn will sound and the CABIN
ALTITUDE lights (if installed and operative)
will illuminate at a cabin altitude of
approximately 10,000 feet.
15 Plan to land at the nearest suitable airport.
16 When the cabin altitude is at or below 10,000 feet:
ELT
on
tro
lle
d
if
Oxygen masks may be removed.
ELT
ELT
The emergency locator transmitter is on.
■■■■
U
nc
Condition:
■■■■
1.6
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1.7
737 Flight Crew Operations Manual
NOT ARMED
A
N R
O M
T E
D
EMERGENCY EXIT LIGHTS
NOT ARMED
The emergency exit lights switch is not
ARMED.
or
pr
in
te
d
Condition:
1 Choose one:
EMER EXIT LIGHTS switch is ON:
Individual emergency exit light batteries
supply a minimum of 10 minutes of
lighting.
ad
ed
■■■■
do
w
nl
o
EMER EXIT LIGHTS switch is OFF:
Emergency lighting is not available.
U
nc
on
tro
lle
d
if
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 26, 2015
D6-27370-8AS-NOK
1.7
1.8
737 Flight Crew Operations Manual
FWDENTRY
AFT
ENTRY
ENTRY DOOR
Condition:
AFT
ENTRY
One or more entry doors are not closed and
secure.
or
pr
in
te
d
FWD
ENTRY
1 Instruct the cabin crew to verify that the door
handle is in the closed position or to move the
handle to the closed position if possible.
2 Choose one:
►►Go to step 3
ad
ed
Handle is in the closed position:
do
w
nl
o
Handle is not in the closed position:
Plan to land at the nearest suitable airport.
■■■■
if
3 Choose one:
d
Pressurization is normal:
on
tro
lle
The door is in a safe configuration.
Continue normal operation.
■■■■
U
nc
Pressurization is not normal:
1.8
Plan to land at the nearest suitable airport.
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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September 17, 2020
1.9
737 Flight Crew Operations Manual
EQUIP
EQUIPMENT DOOR
EQUIP
Condition:
The equipment door is not closed and
secure.
Pressurization is normal:
or
pr
in
te
d
1 Choose one:
The door is in a safe configuration.
Continue normal operation.
■■■■
ad
ed
Pressurization is not normal:
►►Go to step 2
do
w
nl
o
2 Don oxygen masks.
3 Establish crew communications.
4 Passenger signs . . . . . . . . . . . . . . . . . . . . . . ON
5 Choose one:
d
if
Airplane has reached the planned cruise altitude:
on
tro
lle
►►Go to step 6
U
nc
Airplane has not reached the planned cruise
altitude:
Do not continue the climb.
Reset the FLT ALT indicator to the actual
airplane altitude.
►►Go to step 6
6 LAND ALT indicator . . . . . . . . . . . . . . . 9000 feet
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 19, 2020
D6-27370-8AS-NOK
1.9
1.10
737 Flight Crew Operations Manual
▼EQUIPMENT DOOR continued▼
7 Choose one:
Minimum safe altitude is at or below 9,000
feet:
or
pr
in
te
d
►►Go to step 8
Minimum safe altitude is between 9,000 feet
and 13,000 feet:
►►Go to step 10
ad
ed
Minimum safe altitude is at or above 13,000
feet:
►►Go to step 12
do
w
nl
o
8 Descend to 9,000 feet.
9 Maintain a cabin differential pressure of 0 psi by
limiting flight altitude to 9,000 feet.
if
►►Go to step 15
on
tro
lle
d
10 Descend to the minimum safe altitude.
11 LAND ALT indicator . . . . . Select a higher altitude
(maximum 13,000 feet) to
maintain a cabin differential
pressure of 0 psi
U
nc
Note: The intermittent cabin altitude/configuration
warning horn will sound and the CABIN
ALTITUDE lights (if installed and operative)
will illuminate at a cabin altitude of
approximately 10,000 feet.
►►Go to step 15
▼ Continued on next page ▼
1.10
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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1.11
737 Flight Crew Operations Manual
▼EQUIPMENT DOOR continued▼
12 Descend to the minimum safe altitude.
13 Pressurization mode selector . . . . . . . . . . . . MAN
do
w
nl
o
ad
ed
or
pr
in
te
d
Use momentary actuation of the outflow valve
switch to avoid large and rapid pressurization
changes.
14 Outflow VALVE switch . . . . Move to OPEN until
the outflow VALVE
indication shows fully open
to depressurize the airplane
Note: The intermittent cabin altitude/configuration
warning horn will sound and the CABIN
ALTITUDE lights (if installed and operative)
will illuminate at a cabin altitude of
approximately 10,000 feet.
15 Plan to land at the nearest suitable airport.
16 When the cabin altitude is at or below 10,000 feet:
■■■■
U
nc
on
tro
lle
d
if
Oxygen masks may be removed.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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D6-27370-8AS-NOK
1.11
1.12
737 Flight Crew Operations Manual
LOCK FAIL
LOCK
FAIL
LOCK FAIL
One or more of these occur:
•The FLIGHT DECK ACCESS SYSTEM switch
is OFF
•The lock is failed.
Objective:
To remove electrical power from the lock to
prevent a possible overheat.
Do if conditions allow a crew
member to leave the seat.
1
or
pr
in
te
d
Condition:
ad
ed
FLIGHT DECK ACCESS SYSTEM switch . . . . OFF
Note: The door can be locked with the dead bolt.
do
w
nl
o
■■■■
LEFT AFT
RIGHT
FWD
FWD
AFTOVERWING
OVERWING
OVERWING
OVERWING
OVERWING DOOR
LEFT AFT
OVERWING
One or more overwing doors are not closed
and secure.
on
tro
lle
Condition:
RIGHT AFT
OVERWING
d
if
LEFT FWD RIGHT FWD
OVERWING OVERWING
1 Choose one:
U
nc
Pressurization is normal:
The door is in a safe configuration.
Continue normal operation.
■■■■
Pressurization is not normal:
Plan to land at the nearest suitable airport.
■■■■
1.12
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1.13
737 Flight Crew Operations Manual
PASS OXY ON - Chemical oxygen
PASS OXY
ON
Condition:
PASSENGER OXYGEN ON
The passenger oxygen system is on.
U
nc
on
tro
lle
d
if
do
w
nl
o
ad
ed
or
pr
in
te
d
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 17, 2020
D6-27370-8AS-NOK
1.13
1.14
737 Flight Crew Operations Manual
FWDSERVICE
AFT
SERVICE
SERVICE DOOR
Condition:
AFT
SERVICE
One or more service doors are not closed
and secure.
or
pr
in
te
d
FWD
SERVICE
1 Instruct the cabin crew to verify that the door
handle is in the closed position or to move the
handle to the closed position if possible.
2 Choose one:
►►Go to step 3
ad
ed
Handle is in the closed position:
do
w
nl
o
Handle is not in the closed position:
Plan to land at the nearest suitable airport.
■■■■
if
3 Choose one:
d
Pressurization is normal:
on
tro
lle
The door is in a safe configuration.
Continue normal operation.
■■■■
U
nc
Pressurization is not normal:
Plan to land at the nearest suitable airport.
■■■■
Tail Strike ►►15.5
1.14
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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1.15
737 Flight Crew Operations Manual
Window Damage - Forward
(L1, L2, R1, R2)
A forward flight deck window has one or
more of these:
•An electrical arc
•A delamination
•A crack
•Is shattered.
Objective:
To remove electrical power, if needed, to
prevent arcing. To reduce differential pressure and descend if the inner pane is shattered or cracked.
L2
L1
R1
R2
R3
if
L3
do
w
nl
o
ad
ed
or
pr
in
te
d
Condition:
on
tro
lle
d
1 Choose one:
Window is delaminated only:
Continue normal operation.
nc
■■■■
U
Window is arcing:
►►Go to step 2
Window is cracked or shattered:
►►Go to step 5
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 19, 2020
D6-27370-8AS-NOK
1.15
1.16
737 Flight Crew Operations Manual
▼Window Damage - Forward (L1, L2, R1, R2) continued▼
2 WINDOW HEAT switch
(affected window). . . . . . . . . . . . . . . . . . . . OFF
Limit airspeed to 250 knots maximum below
10,000 feet.
4 Continue normal operation.
ad
ed
■■■■
or
pr
in
te
d
3 Pull both WINDSHIELD AIR controls. This vents
conditioned air to the inside of the windshield for
defogging.
5 Don seat belts and shoulder harnesses.
do
w
nl
o
6 WINDOW HEAT switch
(affected window). . . . . . . . . . . . . . . . . . . . OFF
Limit airspeed to 250 knots maximum below
10,000 feet.
on
tro
lle
d
if
7 Pull both WINDSHIELD AIR controls. This vents
conditioned air to the inside of the windshield for
defogging.
8 Choose one:
Damage is on the outer pane:
U
nc
►►Go to step 9
Damage is on the inner pane:
►►Go to step 11
9 Continue normal operation.
▼ Continued on next page ▼
1.16
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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1.17
737 Flight Crew Operations Manual
▼Window Damage - Forward (L1, L2, R1, R2) continued▼
10 Shoulder harnesses may be removed.
■■■■
11 Don oxygen masks.
or
pr
in
te
d
12 Establish crew communications.
13 Passenger signs . . . . . . . . . . . . . . . . . . . . . . ON
14 Choose one:
Airplane has reached the planned cruise altitude:
ad
ed
►►Go to step 15
do
w
nl
o
Airplane has not reached the planned cruise
altitude:
Do not continue the climb.
Reset the FLT ALT indicator to the actual
airplane altitude.
d
if
►►Go to step 15
on
tro
lle
15 LAND ALT indicator . . . . . . . . . . . . . . . 9000 feet
16 Start a normal descent to below 14,000 feet or to
the minimum safe altitude, whichever is higher.
nc
17 Plan to land at the nearest suitable airport.
U
18 When cabin differential pressure is 2 psi or less:
Oxygen masks and shoulder harnesses may be
removed.
19 Sustained flight below 10,000 feet is not
recommended due to the greater risk of a bird
strike.
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 19, 2020
D6-27370-8AS-NOK
1.17
1.18
737 Flight Crew Operations Manual
Window Damage - Heated Side
(L3, R3)
YL061 - YR339
A heated side flight deck window has one or
more of these:
•An electrical arc
•A delamination
•A crack
•Is shattered.
Objective:
To remove electrical power, if needed, to
prevent arcing. To reduce differential pressure and descend if the inner pane is shattered or cracked.
L1
L2
R1
R2
R3
on
tro
lle
d
if
L3
do
w
nl
o
ad
ed
or
pr
in
te
d
Condition:
U
nc
▼ Continued on next page ▼
1.18
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 19, 2020
1.19
737 Flight Crew Operations Manual
▼Window Damage - Heated Side (L3, R3) continued▼
1 Choose one:
Window is delaminated only:
■■■■
Window is arcing:
►►Go to step 2
or
pr
in
te
d
Continue normal operation.
Window is cracked or shattered:
ad
ed
►►Go to step 5
do
w
nl
o
2 WINDOW HEAT switch
(affected window). . . . . . . . . . . . . . . . . . . . OFF
Limit airspeed to 250 knots maximum below
10,000 feet.
on
tro
lle
d
if
3 Pull both WINDSHIELD AIR controls. This vents
conditioned air to the inside of the windshield for
defogging.
4 Continue normal operation.
■■■■
nc
5 Don seat belts and shoulder harnesses.
U
6 WINDOW HEAT switch
(affected window). . . . . . . . . . . . . . . . . . . . OFF
Limit airspeed to 250 knots maximum below
10,000 feet.
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 19, 2020
D6-27370-8AS-NOK
1.19
1.20
737 Flight Crew Operations Manual
▼Window Damage - Heated Side (L3, R3) continued▼
7 Pull both WINDSHIELD AIR controls. This vents
conditioned air to the inside of the windshield for
defogging.
Damage is on the outer pane:
►►Go to step 9
Damage is on the inner pane:
ad
ed
►►Go to step 11
or
pr
in
te
d
8 Choose one:
9 Continue normal operation.
10 Shoulder harnesses may be removed.
do
w
nl
o
■■■■
11 Don oxygen masks.
if
12 Establish crew communications.
d
13 Passenger signs . . . . . . . . . . . . . . . . . . . . . . ON
on
tro
lle
14 Choose one:
Airplane has reached the planned cruise altitude:
►►Go to step 15
U
nc
Airplane has not reached the planned cruise
altitude:
Do not continue the climb.
Reset the FLT ALT indicator to the actual
airplane altitude.
►►Go to step 15
▼ Continued on next page ▼
1.20
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1.21
737 Flight Crew Operations Manual
▼Window Damage - Heated Side (L3, R3) continued▼
15 LAND ALT indicator . . . . . . . . . . . . . . . 9000 feet
16 Start a normal descent to below 14,000 feet or to
the minimum safe altitude, whichever is higher.
or
pr
in
te
d
17 Plan to land at the nearest suitable airport.
18 When cabin differential pressure is 2 psi or less:
Oxygen masks and shoulder harnesses may be
removed.
ad
ed
19 Sustained flight below 10,000 feet is not
recommended due to the greater risk of a bird
strike.
U
nc
on
tro
lle
d
if
do
w
nl
o
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 19, 2020
D6-27370-8AS-NOK
1.21
1.22
737 Flight Crew Operations Manual
Window Damage - Unheated Side
(L3, R3)
YK820, YR591 - YW351
An unheated side flight deck window has one
or more of these:
•A crack
•Is shattered.
Objective:
To reduce differential pressure to 0 psi if
both panes are shattered or cracked.
ad
ed
L1
L2
R1
do
w
nl
o
L3
or
pr
in
te
d
Condition:
R2
R3
d
2 Choose one:
if
1 Don seat belts and shoulder harnesses.
on
tro
lle
Damage is only on the inner or outer pane:
►►Go to step 3
►►Go to step 5
U
nc
Damage is on both the inner and outer panes:
3 Continue normal operation.
4 Shoulder harnesses may be removed.
■■■■
▼ Continued on next page ▼
1.22
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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1.23
737 Flight Crew Operations Manual
▼Window Damage - Unheated Side (L3, R3) continued▼
5 Don oxygen masks.
6 Establish crew communications.
8 Choose one:
or
pr
in
te
d
7 Passenger signs . . . . . . . . . . . . . . . . . . . . . . ON
Airplane has reached the planned cruise altitude:
►►Go to step 9
ad
ed
Airplane has not reached the planned cruise
altitude:
Do not continue the climb.
do
w
nl
o
Reset the FLT ALT indicator to the actual
airplane altitude.
►►Go to step 9
9 LAND ALT indicator . . . . . . . . . . . . . . . 9000 feet
if
10 Choose one:
on
tro
lle
d
Minimum safe altitude is at or below 9,000
feet:
Minimum safe altitude is between 9,000 feet
and 13,000 feet:
►►Go to step 13
U
nc
►►Go to step 11
Minimum safe altitude is at or above 13,000
feet:
►►Go to step 15
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 19, 2020
D6-27370-8AS-NOK
1.23
1.24
737 Flight Crew Operations Manual
▼Window Damage - Unheated Side (L3, R3) continued▼
11 Descend to 9,000 feet.
12 Maintain a cabin differential pressure of 0 psi by
limiting flight altitude to 9,000 feet.
or
pr
in
te
d
►►Go to step 18
13 Descend to the minimum safe altitude.
14 LAND ALT indicator . . . . . Select a higher altitude
(maximum 13,000 feet) to
maintain a cabin differential
pressure of 0 psi
►►Go to step 18
do
w
nl
o
ad
ed
Note: The intermittent cabin altitude/configuration
warning horn will sound and the CABIN
ALTITUDE lights (if installed and operative)
will illuminate at a cabin altitude of
approximately 10,000 feet.
if
15 Descend to the minimum safe altitude.
on
tro
lle
d
16 Pressurization mode selector . . . . . . . . . . . . MAN
U
nc
Use momentary actuation of the outflow valve
switch to avoid large and rapid pressurization
changes.
17 Outflow VALVE switch. . . . . Move to OPEN until
the outflow VALVE
indication shows fully open
to depressurize the airplane
Note: The intermittent cabin altitude/configuration
warning horn will sound and the CABIN
ALTITUDE lights (if installed and operative)
will illuminate at a cabin altitude of
approximately 10,000 feet.
▼ Continued on next page ▼
1.24
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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1.25
737 Flight Crew Operations Manual
▼Window Damage - Unheated Side (L3, R3) continued▼
18 When the cabin altitude is at or below 10,000 feet:
Oxygen masks may be removed.
■■■■
Window Open
A side window opens during takeoff or in
flight.
ad
ed
Condition:
or
pr
in
te
d
19 Shoulder harnesses may be removed.
1 Maintain the maneuvering speed for the existing
flap setting until the window is closed.
do
w
nl
o
2 The force needed to close the window increases
with airspeed. It may not be possible to close the
window at speeds above 250 knots.
3 Close and lock the window.
if
4 Choose one:
on
tro
lle
d
Window locks and the pressurization is normal:
Continue normal operation.
■■■■
U
nc
Window does not lock or the pressurization is
not normal:
Level off at the lowest safe altitude.
The airplane can fly unpressurized and land
safely with the window open.
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 19, 2020
D6-27370-8AS-NOK
1.25
1.26
do
w
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o
ad
ed
or
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in
te
d
737 Flight Crew Operations Manual
U
nc
on
tro
lle
d
if
Intentionally
Blank
1.26
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
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2 Air Systems
NNC.2-Air
Systems
(tab)
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Air Systems
Section 2
Table of Contents
or
pr
in
te
d
CABIN ALTITUDE WARNING or Rapid
Depressurization .........................2.1
Emergency Descent ............................. ►►0.1
Smoke, Fire or Fumes ........................ ►►8.10
NNC. 3
AUTO FAIL or Unscheduled Pressurization Change 2.4
BLEED TRIP OFF...............................................2.8
ad
ed
CABIN ALTITUDE WARNING or Rapid
Depressurization .........................2.1
do
w
nl
o
Cabin Temperature Hot .....................................2.9
DUAL BLEED.................................................. 2.13
Emergency Descent ............................. ►►0.1
on
tro
lle
d
if
EQUIPMENT COOLING OFF .............................. 2.14
OFF SCHEDULE DESCENT ................................ 2.14
PACK ............................................................2.16
Smoke, Fire or Fumes ........................ ►►8.10
U
nc
WING-BODY OVERHEAT .................................. 2.20
ZONE TEMP ................................................... 2.26
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
2
D6-27370-8AS-NOK
2.TOC.1
Non-Normal Checklists Air Systems
737 Flight Crew Operations Manual
do
w
nl
o
ad
ed
or
pr
in
te
d
Table of Contents
U
nc
on
tro
lle
d
if
Intentionally
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Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
2.TOC.2
D6-27370-8AS-NOK
March 31, 2023
2.1
737 Flight Crew Operations Manual
Air Systems
File
CABIN
Highlight
ALTITUDE
CABIN ALTITUDE WARNING
or
Rapid Depressurization
CABIN ALTITUDE WARNING or Rapid Depressurization
One or more of these occur:
•A cabin altitude exceedance
•In flight, the intermittent cabin
altitude/configuration warning horn
sounds or a CABIN ALTITUDE light (if
installed and operative) illuminates.
ad
ed
Condition:
(If installed and operative)
or
pr
in
te
d
CABIN
ALTITUDE
1 Don oxygen masks and set regulators to 100%.
2 Establish crew communications.
do
w
nl
o
3 Pressurization mode selector . . . . . . . . . . . . MAN
if
4 Outflow VALVE switch . . . . . . . . . . Hold in CLOSE
until the outflow VALVE
indication shows fully closed
d
5 If cabin altitude is uncontrollable:
on
tro
lle
Passenger signs . . . . . . . . . . . . . . . . . . . . ON
►►Go to the Emergency Descent checklist
on page 0.1
■■■■
U
nc
PASS OXYGEN switch . . . . . . . . . . . . . . . . ON
----------------------▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 26, 2015
D6-27370-8AS-NOK
2.1
2.2
737 Flight Crew Operations Manual
▼CABIN ALTITUDE WARNING or Rapid Depressurization
continued▼
6 If cabin altitude is controllable:
Continue manual operation to maintain correct
cabin altitude.
or
pr
in
te
d
When the cabin altitude is at or below 10,000
feet:
Oxygen masks may be removed.
7 Checklist Complete Except Deferred Items
do
w
nl
o
Descent Checklist
ad
ed
Deferred Items
on
tro
lle
d
if
Use momentary actuation of the outflow valve
switch to avoid large and rapid pressurization
changes.
Pressurization . . Move outflow VALVE switch
to OPEN or CLOSE as needed
to control cabin altitude and rate
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing data . . . . . . . . . VREF ___, Minimums ___
U
nc
Approach briefing . . . . . . . . . . . . . . . . Completed
Approach Checklist
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
▼ Continued on next page ▼
2.2
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D6-27370-8AS-NOK
March 31, 2023
2.3
737 Flight Crew Operations Manual
▼CABIN ALTITUDE WARNING or Rapid Depressurization
continued▼
At Pattern Altitude
or
pr
in
te
d
Outflow VALVE switch . . . . . . . Move to OPEN until
the outflow VALVE
indication shows fully open
to depressurize the airplane
Landing Checklist
ad
ed
ENGINE START switches . . . . . . . . . . . . . . . CONT
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
do
w
nl
o
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps . . . . . . . . . . . . . . . . . . . . . ___, Green light
■■■■
U
nc
on
tro
lle
d
if
Smoke, Fire or Fumes ►►8.10
Emergency Descent ►►0.1
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March 31, 2023
D6-27370-8AS-NOK
2.3
2.4
737 Flight Crew Operations Manual
AUTO FAIL
AUTO FAIL
or
Unscheduled Pressurization Change
AUTO FAIL or Unscheduled Pressurization Change
AUTO
FAIL
May or may not be illuminated
One or more of these occur:
•Automatic pressurization mode has failed
•The cabin altitude is uncontrollable.
Objective:
To maintain control of cabin altitude.
or
pr
in
te
d
Condition:
ad
ed
1 Increasing thrust may ensure sufficient air supply
to control cabin altitude.
2 Pressurization mode selector . . . . . . . . . . . ALTN
do
w
nl
o
3 Choose one:
AUTO FAIL light is extinguished and cabin
altitude is controllable:
■■■■
on
tro
lle
d
if
Continue normal operation.
AUTO FAIL light is illuminated or cabin altitude
is uncontrollable:
nc
►►Go to step 4
U
4 Pressurization mode selector . . . . . . . . . . . . MAN
2.4
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
2.5
737 Flight Crew Operations Manual
▼AUTO FAIL or Unscheduled Pressurization Change continued▼
or
pr
in
te
d
Use momentary actuation of the outflow valve
switch to avoid large and rapid pressurization
changes.
Outflow
VALVE
5
switch . . . . . . . . . . . . Move to OPEN or CLOSE
as needed to control
cabin altitude and rate
6 Choose one:
Cabin altitude is controllable:
ad
ed
►►Go to step 11
Cabin altitude is uncontrollable:
do
w
nl
o
►►Go to step 7
7 Don oxygen masks and set regulators to 100%.
8 Establish crew communications.
if
9 Passenger signs . . . . . . . . . . . . . . . . . . . . . . ON
on
tro
lle
d
10 PASS OXYGEN switch . . . . . . . . . . . . . . . . . . ON
►►Go to the Emergency Descent checklist on
page 0.1
■■■■
U
nc
11 Checklist Complete Except Deferred Items
Deferred Items
▼ Continued on next page ▼
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March 31, 2023
D6-27370-8AS-NOK
2.5
2.6
737 Flight Crew Operations Manual
▼AUTO FAIL or Unscheduled Pressurization Change continued▼
Descent Checklist
or
pr
in
te
d
Use momentary actuation of the outflow valve
switch to avoid large and rapid pressurization
changes.
Pressurization . . Move outflow VALVE switch
to OPEN or CLOSE as needed
to control cabin altitude and rate
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
ad
ed
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing data . . . . . . . . . VREF ___, Minimums ___
do
w
nl
o
Approach briefing . . . . . . . . . . . . . . . . Completed
Approach Checklist
if
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
on
tro
lle
d
At Pattern Altitude
nc
Outflow VALVE switch . . . . . . . Move to OPEN until
the outflow VALVE
indication shows fully open
to depressurize the airplane
U
Landing Checklist
ENGINE START switches. . . . . . . . . . . . . . . . CONT
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
▼ Continued on next page ▼
2.6
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D6-27370-8AS-NOK
March 31, 2023
2.7
737 Flight Crew Operations Manual
▼AUTO FAIL or Unscheduled Pressurization Change continued▼
Flaps . . . . . . . . . . . . . . . . . . . . . ___, Green light
U
nc
on
tro
lle
d
if
do
w
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o
ad
ed
or
pr
in
te
d
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
2.7
2.8
737 Flight Crew Operations Manual
BLEED TRIP OFF
BLEED
TRIP OFF
Condition:
BLEED TRIP OFF
One or more of these occur:
•An engine bleed air overheat
•An engine bleed air overpressure.
or
pr
in
te
d
1 WING ANTI-ICE switch . . . . . . . . . . . . . . . . OFF
2 TRIP RESET switch . . . . . . . . . . . . . . . . . . Push
The BLEED TRIP OFF light extinguishes if the
bleed air temperature has cooled below limits.
3 Choose one:
ad
ed
BLEED TRIP OFF light stays illuminated:
PACK switch (affected side). . . . . . . . OFF
do
w
nl
o
This causes the operating pack to
regulate to high flow in flight with
flaps up.
■■■■
on
tro
lle
d
if
Avoid icing conditions where wing anti-ice is
needed.
BLEED TRIP OFF light extinguishes:
►►Go to step 4
nc
4 WING ANTI-ICE switch . . . . . . . . . . . .As needed
U
Caution! Use of wing anti-ice above
approximately FL350 may cause bleed
trip off and possible loss of cabin
pressure.
■■■■
2.8
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
2.9
737 Flight Crew Operations Manual
Cabin Temperature Hot
Flight deck or passenger cabin temperature
is excessively hot. The temperature can
cause incapacitation.
Objective:
To regain temperature control. If unable to
regain control, to descend and configure to
provide alternate ventilation.
1 Choose one:
or
pr
in
te
d
Condition:
Flight deck temperature is too high:
ad
ed
►►Go to step 2
Passenger cabin temperature is too high:
do
w
nl
o
►►Go to step 8
2 TRIM AIR switch . . . . . . . . . . . . . . . . . . . . . OFF
3 Wait 1 minute.
if
4 Choose one:
on
tro
lle
d
Air from the flight deck outlets is still too warm:
►►Go to step 5
The flight deck temperature gradually
cools.
■■■■
U
nc
Air from the flight deck outlets is cool:
5 L PACK switch . . . . . . . . . . . . . . . . . . . . . . OFF
6 Wait 1 minute.
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
2.9
2.10
737 Flight Crew Operations Manual
▼Cabin Temperature Hot continued▼
7 Choose one:
Air from the flight deck outlets is still too warm:
►►Go to step 14
or
pr
in
te
d
Air from the flight deck outlets is cool:
The flight deck temperature gradually
cools.
■■■■
ad
ed
8 TRIM AIR switch . . . . . . . . . . . . . . . . . . . . . OFF
9 Wait 1 minute.
do
w
nl
o
10 Choose one:
Air from the passenger cabin outlets is still too
warm:
►►Go to step 11
d
if
Air from the passenger cabin outlets is cool:
on
tro
lle
The passenger cabin temperature gradually
cools.
■■■■
nc
11 R PACK switch . . . . . . . . . . . . . . . . . . . . . . OFF
U
12 Wait 1 minute.
2.10
▼ Continued on next page ▼
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D6-27370-8AS-NOK
March 31, 2023
2.11
737 Flight Crew Operations Manual
▼Cabin Temperature Hot continued▼
13 Choose one:
Air from the passenger cabin outlets is still too
warm:
or
pr
in
te
d
►►Go to step 14
Air from the passenger cabin outlets is cool:
The passenger cabin temperature gradually
cools.
ad
ed
■■■■
do
w
nl
o
14 Start a descent to the lowest safe altitude, or
10,000 feet, whichever is higher. Use the
speedbrakes to increase the rate of descent, if
needed. Monitor cabin altitude and rate.
15 R RECIRC FAN switch . . . . . . . . . . . . . . . . AUTO
16 L RECIRC FAN switch . . . . . . . . . . . . . . . . . OFF
if
17 Minimize the flight deck lighting intensity.
on
tro
lle
d
18 Open the flight deck door.
19 During daylight:
Instruct the cabin crew to close cabin window
shades.
U
nc
Use flight deck window shades, as needed.
YK820, YL061
20 Instruct the cabin crew to dim cabin lighting.
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
2.11
2.12
737 Flight Crew Operations Manual
▼Cabin Temperature Hot continued▼
YR323 - YW351
21 Advise the cabin crew that the cabin lighting will be
extinguished, but passenger reading lights will
continue to work.
or
pr
in
te
d
22 CAB/UTIL switch. . . . . . . . . . . . . . . . . . . . . OFF
23 IFE/PASS SEAT switch . . . . . . . . . . . . . . . . . OFF
24 When at level off:
ad
ed
Maintain 290 knots minimum. Flight deck and
passenger cabin temperatures can increase
rapidly at speeds below 290 knots.
25 Choose one:
do
w
nl
o
Airplane altitude is at or below 10,000 feet:
►►Go to step 26
Airplane altitude is above 10,000 feet:
if
Don oxygen masks.
on
tro
lle
d
Establish crew communications.
►►Go to step 26
26 PACK switch (operating pack) . . . . . . . . . . . OFF
U
nc
27 Pressurization mode selector . . . . . . . . . . . . MAN
2.12
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
2.13
737 Flight Crew Operations Manual
▼Cabin Temperature Hot continued▼
28
or
pr
in
te
d
Use momentary actuation of the outflow valve
switch to avoid large and rapid pressurization
changes.
Outflow VALVE switch . . . . Move to OPEN until
the outflow VALVE
indication shows fully open
This increases airplane ventilation.
29 Plan to land at the nearest suitable airport.
ad
ed
■■■■
DUAL BLEED
DUAL
BLEED
DUAL BLEED
The APU bleed valve is open and one of
these occurs:
•BLEED 1 air switch is on
•BLEED 2 air switch is on and the
ISOLATION VALVE is open.
Objective:
To prevent possible backpressure of the
APU.
on
tro
lle
d
if
do
w
nl
o
Condition:
1 Limit engine thrust to idle while the light is
illuminated.
APU BLEED air switch . . . . . . . . . . . . . . . OFF
■■■■
U
nc
2 After engine start:
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
2.13
2.14
737 Flight Crew Operations Manual
OFF - Equipment Cooling
EQUIPMENT COOLING OFF
OFF
The equipment cooling supply or exhaust fan
is failed.
Condition:
or
pr
in
te
d
1 EQUIP COOLING SUPPLY or EXHAUST
switch (affected side) . . . . . . . . . . . . . . . . ALTN
Note: Illumination of the EQUIP COOLING SUPPLY
or EXHAUST OFF light may be an indication of
a pressurization problem. Ensure the
pressurization system is operating normally.
ad
ed
2 No further action is necessary in flight if the
equipment cooling OFF light does not extinguish.
■■■■
OFF SCHED DESCENT
OFF SCHED
DESCENT
do
w
nl
o
A descent is started before reaching the
planned cruise altitude set in the FLT ALT
indicator.
d
1 Choose one:
if
Condition:
OFF SCHEDULE DESCENT
on
tro
lle
Landing at airport of departure:
Continue normal operation.
■■■■
U
nc
Not landing at airport of departure:
FLT ALT indicator . . . . . . . Reset to actual
airplane altitude
■■■■
2.14
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March 31, 2023
2.15
do
w
nl
o
ad
ed
or
pr
in
te
d
737 Flight Crew Operations Manual
U
nc
on
tro
lle
d
if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
2.15
2.16
737 Flight Crew Operations Manual
PACK
PACK
PACK
Condition:
One or more of these occur:
•The primary and standby pack controls
are failed
•A pack overheat.
or
pr
in
te
d
1 Temperature
selectors (all) . . . . . . Select warmer temperature
This reduces the workload on the affected air
conditioning pack.
ad
ed
2 TRIP RESET switch . . . . . . . . . . . . . . . . . . Push
do
w
nl
o
If the PACK light illuminated as a result of the
pack temperature exceeding limits, the light
extinguishes if the pack temperature has cooled
below limits.
U
nc
on
tro
lle
d
if
▼ Continued on next page ▼
2.16
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D6-27370-8AS-NOK
March 31, 2023
2.17
737 Flight Crew Operations Manual
▼PACK continued▼
3 Choose one:
Both PACK lights are extinguished:
■■■■
or
pr
in
te
d
Continue normal operation.
A single PACK light stays illuminated:
ISOLATION VALVE switch . . . . . . . CLOSE
PACK switch (affected side) . . . . . . . OFF
ad
ed
■■■■
Both PACK lights stay illuminated:
do
w
nl
o
Note: Both pack valves may have closed
resulting in a gradual loss of cabin
pressure and an eventual CABIN
ALTITUDE warning.
if
►►Go to step 4
on
tro
lle
d
4 Descend to the lowest safe altitude, or 10,000 feet,
whichever is higher. Monitor cabin altitude and
rate.
U
nc
5 When at level off:
Maintain 290 knots minimum. Flight deck and
cabin temperatures may increase rapidly at
speeds below 290 knots.
▼ Continued on next page ▼
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March 31, 2023
D6-27370-8AS-NOK
2.17
2.18
737 Flight Crew Operations Manual
▼PACK continued▼
6 Choose one:
Airplane altitude is at or below 10,000 feet:
►►Go to step 7
Don oxygen masks.
or
pr
in
te
d
Airplane altitude is above 10,000 feet:
Establish crew communications.
►►Go to step 7
ad
ed
7 Pressurization mode selector . . . . . . . . . . . . MAN
do
w
nl
o
Use momentary actuation of the outflow valve
switch to avoid large and rapid pressurization
changes.
Outflow VALVE switch. . . . . Move to OPEN until
the outflow VALVE
indication shows fully open
This increases airplane ventilation.
d
if
8
on
tro
lle
9 R RECIRC FAN switch . . . . . . . . . . . . . . . . AUTO
10 L RECIRC FAN switch . . . . . . . . . . . . . . . . . OFF
11 Minimize the flight deck lighting intensity.
nc
12 Open the flight deck door.
U
13 During daylight:
Use flight deck window shades, as needed.
Instruct the cabin crew to close cabin window
shades.
▼ Continued on next page ▼
2.18
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D6-27370-8AS-NOK
March 31, 2023
2.19
737 Flight Crew Operations Manual
▼PACK continued▼
YK820, YL061
14 Instruct the cabin crew to dim cabin lighting.
or
pr
in
te
d
YR323 - YW351
15 Advise the cabin crew that the cabin lighting will be
extinguished, but passenger reading lights will
continue to work.
16 CAB/UTIL switch . . . . . . . . . . . . . . . . . . . . OFF
17 IFE/PASS SEAT switch. . . . . . . . . . . . . . . . . OFF
18 Plan to land at the nearest suitable airport.
U
nc
on
tro
lle
d
if
do
w
nl
o
ad
ed
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
2.19
2.20
737 Flight Crew Operations Manual
WING-BODY OVERHEAT
WING-BODY
OVERHEAT
WING-BODY OVERHEAT
Condition:
An overheat from a bleed duct leak occurs.
Objective:
To isolate the bleed duct leak.
or
pr
in
te
d
1 ISOLATION VALVE switch. . . . . . . . . . . . . CLOSE
2 Choose one:
Both WING-BODY OVERHEAT lights illuminated:
TRIM AIR switch . . . . . . . . . . . . . . . OFF
ad
ed
Note: Passenger cabin temperature
control may be less accurate.
■■■■
do
w
nl
o
Only right WING-BODY OVERHEAT light
illuminated:
►►Go to step 3
d
if
Only left WING-BODY OVERHEAT light
illuminated:
on
tro
lle
►►Go to step 8
3 R PACK switch . . . . . . . . . . . . . . . . . . . . . . OFF
nc
This causes the operating pack to regulate to
high flow in flight with the flaps up.
U
4 BLEED 2 air switch . . . . . . . . . . . . . . . . . . . OFF
5 WING ANTI-ICE switch . . . . . . . . . . . . . . . . OFF
This prevents possible asymmetrical ice buildup
on the wings.
▼ Continued on next page ▼
2.20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
2.21
737 Flight Crew Operations Manual
▼WING-BODY OVERHEAT continued▼
6 Avoid icing conditions where wing anti-ice is
needed.
7 Choose one:
■■■■
or
pr
in
te
d
WING-BODY OVERHEAT light extinguishes:
WING-BODY OVERHEAT light stays illuminated:
TRIM AIR switch . . . . . . . . . . . . . . . OFF
ad
ed
Note: Passenger cabin temperature
control may be less accurate.
■■■■
do
w
nl
o
8 L PACK switch . . . . . . . . . . . . . . . . . . . . . . OFF
This causes the operating pack to regulate to
high flow in flight with the flaps up.
if
9 BLEED 1 air switch . . . . . . . . . . . . . . . . . . . OFF
d
10 WING ANTI-ICE switch . . . . . . . . . . . . . . . . OFF
on
tro
lle
This prevents possible asymmetrical ice buildup
on the wings.
nc
11 Avoid icing conditions where wing anti-ice is
needed.
U
▼ Continued on next page ▼
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March 31, 2023
D6-27370-8AS-NOK
2.21
2.22
737 Flight Crew Operations Manual
▼WING-BODY OVERHEAT continued▼
12 Choose one:
WING-BODY OVERHEAT light extinguishes:
■■■■
or
pr
in
te
d
WING-BODY OVERHEAT light stays
illuminated:
►►Go to step 13
13 Choose one:
►►Go to step 14
do
w
nl
o
APU is not running:
ad
ed
APU is running:
TRIM AIR switch . . . . . . . . . . . . . . . OFF
■■■■
d
if
Note: Passenger cabin temperature
control may be less accurate.
U
nc
on
tro
lle
▼ Continued on next page ▼
2.22
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
2.23
737 Flight Crew Operations Manual
▼WING-BODY OVERHEAT continued▼
14 Choose one:
APU BLEED air switch is ON:
APU BLEED air switch . . . . . . . . . . . OFF
►►Go to step 15
APU BLEED air switch is OFF:
or
pr
in
te
d
This stops the flow of bleed air from
the APU to the left side of the
pneumatic ducting.
ad
ed
APU switch . . . . . . . . . . . . . . . . . . . OFF
15 Choose one:
do
w
nl
o
►►Go to step 16
WING-BODY OVERHEAT light extinguishes:
►►Go to step 17
on
tro
lle
d
if
WING-BODY OVERHEAT light stays
illuminated:
APU switch . . . . . . . . . . . . . . . . . . . OFF
▼ Continued on next page ▼
U
nc
►►Go to step 16
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
2.23
2.24
737 Flight Crew Operations Manual
▼WING-BODY OVERHEAT continued▼
16 Choose one:
WING-BODY OVERHEAT light extinguishes:
►►Go to step 17
or
pr
in
te
d
WING-BODY OVERHEAT light stays illuminated:
TRIM AIR switch . . . . . . . . . . . . . . . OFF
Note: Passenger cabin temperature
control may be less accurate.
ad
ed
■■■■
17 ISOLATION VALVE switch. . . . . . . . . . . . . . AUTO
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18 BLEED 1 air switch . . . . . . . . . . . . . . . . . . . . ON
19 L PACK switch . . . . . . . . . . . . . . . . . . . . . AUTO
20 WING ANTI-ICE switch . . . . . . . . . . . .As needed
21 Choose one:
on
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if
WING-BODY OVERHEAT light stays
extinguished:
►►Go to step 22
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WING-BODY OVERHEAT light illuminates
again:
2.24
►►Go to step 23
▼ Continued on next page ▼
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2.25
737 Flight Crew Operations Manual
▼WING-BODY OVERHEAT continued▼
22 Choose one:
APU switch is ON:
■■■■
APU switch is OFF:
or
pr
in
te
d
The APU can be used during the rest of the
flight, as an electrical source only, if
needed.
ad
ed
Do not start the APU for the rest of the
flight.
■■■■
do
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23 ISOLATION VALVE switch . . . . . . . . . . . . CLOSE
24 L PACK switch . . . . . . . . . . . . . . . . . . . . . . OFF
25 BLEED 1 air switch . . . . . . . . . . . . . . . . . . . OFF
if
26 WING ANTI-ICE switch . . . . . . . . . . . . . . . . OFF
on
tro
lle
d
27 Avoid icing conditions where wing anti-ice is
needed.
28 The APU can be used during the rest of the flight,
as an electrical source only, if needed.
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nc
■■■■
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2.25
2.26
737 Flight Crew Operations Manual
ZONE TEMP
ZONE
TEMP
Condition:
ZONE TEMP
One or more of these occur:
•A zone duct overheat
•Flight deck temperature control is failed.
or
pr
in
te
d
1 Temperature selector
(affected cabin) . . . . . . . . . . . . . Select a cooler
temperature
This prevents the trim air modulating valve from
returning to an overheat condition.
ad
ed
2 TRIP RESET switch . . . . . . . . . . . . . . . . . . Push
The ZONE TEMP light extinguishes if the duct
temperature has cooled below limits.
do
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3 Monitor duct temperature.
If the duct temperature increases rapidly, set
the TRIM AIR switch to OFF.
4 Choose one:
d
if
Affected cabin temperature is excessively high:
on
tro
lle
►►Go to the Cabin Temperature Hot
checklist on page 2.9
■■■■
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Affected cabin temperature is normal:
2.26
■■■■
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3 Anti-Ice, Rain (tab)
NNC.3-Anti-Ice,
Rain
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Anti-Ice, Rain
Section 3
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Table of Contents
ENGINE COWL ANTI-ICE ...................................3.1
ENGINE COWL VALVE OPEN OR TAI INDICATION..3.2
Ice Crystal Icing...............................................3.3
PROBE HEAT....................................................3.6
WINDOW OVERHEAT ........................................3.6
WING ANTI-ICE VALVE OPEN .............................3.8
WING ANTI-ICE VALVE OPEN ........................... 3.10
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3.TOC.1
Non-Normal Checklists Anti-Ice, Rain
737 Flight Crew Operations Manual
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Table of Contents
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3.1
737 Flight Crew Operations Manual
Anti-Ice,
File
COWL
Highlight
ANTI-ICE
Rain
COWL
ANTI-ICE
ENGINE COWL ANTI-ICE
An engine cowl anti-ice duct overpressure
occurs.
Objective:
To reduce cowl duct pressure by reducing
thrust.
or
pr
in
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d
Condition:
1 Reduce thrust only when flight conditions allow.
2 Autothrottle (if engaged). . . . . . . . . . .Disengage
ad
ed
3 Thrust lever
(affected engine) . . . Confirm . . . Retard until the
COWL ANTI-ICE
light extinguishes
do
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4 Run the engine at reduced thrust to keep the light
extinguished.
Note: Do not use FMC performance predictions.
if
YK820, YL061, YR591 - YS823
5 Transponder mode selector . . . . . . . . . . . . . . TA
on
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This step prevents climb commands which can
exceed reduced thrust performance capability.
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YR323, YR339, YV081 - YW351
6 Transponder mode selector . . . . . . . . . . TA ONLY
This step prevents climb commands which can
exceed reduced thrust performance capability.
■■■■
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3.1
3.2
737 Flight Crew Operations Manual
COWL VALVE OPEN - Engine Anti-ice
TAI
COWL VALVE
OPEN
One or both of the following occurs:
•An engine COWL VALVE OPEN light stays
illuminated bright blue
•An amber TAI indication is shown.
1 Choose one:
ENG ANTI-ICE switch is ON:
or
pr
in
te
d
Condition:
ENGINE COWL VALVE OPEN
OR TAI INDICATION
The cowl anti-ice valve is failed closed.
Avoid icing conditions.
ad
ed
■■■■
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ENG ANTI-ICE switch is OFF:
The cowl anti-ice valve is failed open.
■■■■
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on
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d
if
If TAT is above 10°C, limit thrust on the
affected engine to 80% N1 if possible.
3.2
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3.3
737 Flight Crew Operations Manual
Ice Crystal Icing
Engine ice crystal or TAT probe icing is
suspected. Ice crystal icing conditions exist
when in visible moisture, and one or more of
the following indications are present:
•Amber or red weather radar returns below
the airplane
•Appearance of liquid water on the
windshield at temperatures too cold for
rain (the sound is different than rain)
•The autothrottle is unable to maintain the
selected airspeed
•TAT indication stays near 0°C
ad
ed
or
pr
in
te
d
Condition:
To exit the ice crystal icing conditions and
reduce the operational effects of the icing.
if
Objective:
do
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(Additional items that can indicate ice crystal
icing are listed in the Additional Information
section.)
on
tro
lle
d
Note: TAT probe icing can cause the reference N1
bugs to increase or decrease while flying at a
constant altitude and airspeed.
nc
Caution! Do not use engine anti-ice when TAT is
above 10°C.
U
1 ENGINE START switches (both) . . . . . . . . . CONT
2 ENG ANTI-ICE switches (both) . . . . . . . . . . . . ON
3 Minimize time above amber and red weather radar
returns.
▼ Continued on next page ▼
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D6-27370-8AS-NOK
3.3
3.4
737 Flight Crew Operations Manual
▼Ice Crystal Icing continued▼
4 If conditions allow, exit the ice crystal icing
conditions laterally. Climbing or descending to exit
ice crystal icing conditions is not recommended.
5 Choose one:
or
pr
in
te
d
Autothrottle response or TAT indication is
normal:
►►Go to step 8
►►Go to step 6
ad
ed
Autothrottle is unable to maintain the selected
airspeed and TAT indication stays near 0°C:
do
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6 Autothrottle (if engaged) . . . . . . . . . . .Disengage
7 Thrust levers (both) . . . . . . . . . . Set to maintain
airspeed and
airplane flight path
d
if
8 When in ice crystal icing conditions, the following
can be unreliable:
on
tro
lle
Reference N1 bugs and reference N1 readouts
TAS, TAT, SAT, ECON SPD, and LRC.
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9 When ice crystal icing conditions are no longer
present:
Use engine anti-ice normally.
The autothrottle can be re-engaged, if needed.
■■■■
▼ Continued on next page ▼
3.4
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3.5
737 Flight Crew Operations Manual
▼Ice Crystal Icing continued▼
Additional Information
One or more of the following can indicate ice crystal
icing:
or
pr
in
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•Light to moderate turbulence
•Static discharge around the windshield (St. Elmo’s
fire)
•Smell of sulfur
•Smell of ozone
•Humidity increase
do
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ad
ed
An erroneous TAT indication can occur as a result of
ice crystals blocking the sensor. The erroneous
indication can last from one minute to more than 20
minutes. TAT normally should increase
approximately 2°C per 1000 ft of descent.
U
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on
tro
lle
d
if
Vibration indication due to fan hub icing can be 4
units or greater. Fan ice removal procedures have no
effect on fan hub icing. When clear of clouds, fan hub
ice evaporates and engine vibration decreases over
time. Fan hub ice can remain into descent.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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D6-27370-8AS-NOK
3.5
3.6
737 Flight Crew Operations Manual
CAPT
L
TEMP
F/O
R
AUX
ELEV
ALPHA
PITOT
PITOT
PITOT
PROBE
PITOT
VANE
PROBE HEAT
CAPT
PITOT
L ELEV
PITOT
L ALPHA
VANE
TEMP
PROBE
F/O
PITOT
R ELEV
PITOT
R ALPHA
VANE
AUX
PITOT
1 Avoid icing conditions.
or
pr
in
te
d
One or more probe heats are failed.
Condition:
Note: Flight in icing conditions may result in
erroneous flight instrument indications.
ad
ed
■■■■
OVERHEAT - Window
WINDOW OVERHEAT
OVERHEAT
A window overheat occurs.
do
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Condition:
1 WINDOW HEAT switch (affected window) . . . OFF
2 Wait 2 - 5 minutes.
d
if
3 WINDOW HEAT switch (affected window) . . . . ON
on
tro
lle
4 Choose one:
Window OVERHEAT light stays extinguished:
U
nc
Continue normal operation.
■■■■
Window OVERHEAT light illuminates again:
►►Go to step 5
▼ Continued on next page ▼
3.6
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3.7
737 Flight Crew Operations Manual
▼WINDOW OVERHEAT continued▼
5 WINDOW HEAT switch (affected window) . . . OFF
Limit airspeed to 250 knots maximum below
10,000 feet.
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if
do
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ad
ed
■■■■
or
pr
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6 Pull both WINDSHIELD AIR controls. This vents
conditioned air to the inside of the windshield for
defogging.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 19, 2020
D6-27370-8AS-NOK
3.7
3.8
737 Flight Crew Operations Manual
L VALVE OPEN - Wing Anti-ice
R
WING ANTI-ICE VALVE OPEN
YR323 - YW351
Condition:
R VALVE
OPEN
A wing anti-ice L VALVE OPEN or R VALVE
OPEN light stays illuminated bright blue. The
wing anti-ice valve is not in the commanded
position.
1 Choose one:
ad
ed
WING ANTI-ICE switch is ON:
or
pr
in
te
d
L VALVE
OPEN
The wing anti-ice valve is failed closed.
do
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WING ANTI-ICE switch . . . . . . . . . . . OFF
Avoid icing conditions where wing anti-ice is
needed.
if
■■■■
d
WING ANTI-ICE switch is OFF:
on
tro
lle
The wing anti-ice valve is failed open.
►►Go to step 2
nc
2 ISOLATION VALVE switch. . . . . . . . . . . . . CLOSE
U
3 PACK switch (affected side) . . . . . . . . . . . . . OFF
This causes the operating pack to regulate to
high flow in flight with the flaps up.
▼ Continued on next page ▼
3.8
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3.9
737 Flight Crew Operations Manual
▼WING ANTI-ICE VALVE OPEN continued▼
4 Choose one:
WING ANTI-ICE is needed:
►►Go to step 5
►►Go to step 8
or
pr
in
te
d
WING ANTI-ICE is not needed:
5 Engine BLEED air switch
(affected side) . . . . . . . . . . . . . . . . . . . . . . . ON
ad
ed
6 WING ANTI-ICE switch . . . . . . . . . . . . . . . . . ON
7 When wing anti-ice is no longer needed:
do
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►►Go to step 8
8 WING ANTI-ICE switch . . . . . . . . . . . . Verify OFF
9 Engine BLEED air switch (affected side) . . . . OFF
on
tro
lle
d
if
Wing anti-ice is not available on the affected
side with the ISOLATION VALVE switch closed.
Note: Repeat steps 4 through 9 as needed.
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■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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3.9
3.10
737 Flight Crew Operations Manual
L VALVE OPEN - Wing Anti-ice
R
WING ANTI-ICE VALVE OPEN
YK820, YL061
Condition:
R VALVE
OPEN
A wing anti-ice L VALVE OPEN or R VALVE
OPEN light stays illuminated bright blue. The
wing anti-ice valve is not in the commanded
position.
1 Choose one:
ad
ed
WING ANTI-ICE switch is ON:
or
pr
in
te
d
L VALVE
OPEN
The wing anti-ice valve is failed closed.
do
w
nl
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WING ANTI-ICE switch . . . . . . . . . . . OFF
Avoid icing conditions where wing anti-ice is
needed.
if
►►Go to step 10
d
WING ANTI-ICE switch is OFF:
on
tro
lle
The wing anti-ice valve is failed open.
►►Go to step 2
nc
2 ISOLATION VALVE switch. . . . . . . . . . . . . CLOSE
U
3 PACK switch (affected side) . . . . . . . . . . . . . OFF
This causes the operating pack to regulate to
high flow in flight with the flaps up.
▼ Continued on next page ▼
3.10
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3.11
737 Flight Crew Operations Manual
▼WING ANTI-ICE VALVE OPEN continued▼
4 Choose one:
WING ANTI-ICE is needed:
►►Go to step 5
►►Go to step 8
or
pr
in
te
d
WING ANTI-ICE is not needed:
5 Engine BLEED air switch
(affected side) . . . . . . . . . . . . . . . . . . . . . . . ON
ad
ed
6 WING ANTI-ICE switch . . . . . . . . . . . . . . . . . ON
7 When wing anti-ice is no longer needed:
do
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►►Go to step 8
8 WING ANTI-ICE switch . . . . . . . . . . . . Verify OFF
9 Engine BLEED air switch (affected side) . . . . OFF
on
tro
lle
d
if
Wing anti-ice is not available on the affected
side with the ISOLATION VALVE switch closed.
Note: Repeat steps 4 through 9 as needed.
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▼ Continued on next page ▼
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3.11
3.12
737 Flight Crew Operations Manual
▼WING ANTI-ICE VALVE OPEN continued▼
10 Choose one:
Temperature at landing airport is below 10°C or
ice formations are observed on airplane surfaces:
or
pr
in
te
d
►►Go to step 11
Temperature at landing airport is 10°C or above
and ice formations are not observed on airplane
surfaces:
ad
ed
■■■■
11 Set VREF 30 + 10 knots or VREF 40 + 10 knots.
do
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Note: The maximum wind additive should not
exceed 5 knots.
12 Checklist Complete Except Deferred Items
Deferred Items
if
Descent Checklist
on
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lle
d
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
U
nc
Landing data . . . . . . . . . . VREF 30 + 10 knots or
VREF 40 + 10 knots ___
Minimums ___
Approach briefing . . . . . . . . . . . . . . . . Completed
▼ Continued on next page ▼
3.12
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3.13
737 Flight Crew Operations Manual
▼WING ANTI-ICE VALVE OPEN continued▼
Approach Checklist
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
or
pr
in
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Landing Checklist
ENGINE START switches . . . . . . . . . . . . . . . CONT
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
ad
ed
Flaps . . . . . . . . . . . . . . . . . . . . . ___, Green light
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■■■■
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3.13
3.14
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737 Flight Crew Operations Manual
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Blank
3.14
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4 Automatic Flight Flight
NNC.4-Automatic
(tab)
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Automatic Flight
Section 4
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Table of Contents
AUTOPILOT DISENGAGE ...................................4.1
AUTOTHROTTLE DISENGAGE .............................4.1
NO AUTOLAND.................................................4.1
NO LAND 3......................................................4.2
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4.TOC.1
Non-Normal Checklists Automatic Flight
737 Flight Crew Operations Manual
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Table of Contents
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4.1
737 Flight Crew Operations Manual
Automatic
File
A/P
Highlight
Flight
AUTOPILOT DISENGAGE
A/P
P/RST
All autopilots are disengaged. The red light
flashes and the aural tone sounds.
or
pr
in
te
d
Condition:
1 Fly the airplane manually or re–engage an
autopilot.
■■■■
A/T
ad
ed
AUTOTHROTTLE DISENGAGE
A/T
Condition:
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P/RST
The autothrottle is disengaged. The red light
flashes.
on
tro
lle
d
if
1 Control thrust manually or re–engage the
autothrottle.
■■■■
nc
NO AUTOLAND
YR323
Autoland is not available.
U
Condition:
NO AUTOLAND
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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D6-27370-8AS-NOK
4.1
4.2
737 Flight Crew Operations Manual
NO LAND 3
NO LAND 3
YR323
The autoland system does not have the
redundancy needed for LAND 3 operations.
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■■■■
or
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Condition:
4.2
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NNC.5-Communications
5
Communications (tab)
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Communications
Section 5
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Table of Contents
ACARS Electrical Power Loss ..............................5.1
ACARS MU Fail or DU Fail ..................................5.1
Radio Transmit Continuous (Stuck Microphone Switch)
5.2
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5.TOC.1
Non-Normal Checklists Communications
737 Flight Crew Operations Manual
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5.1
737 Flight Crew Operations Manual
File Highlight
Communications
ACARS Electrical Power Loss
YR323, YR339
Condition:
ACARS AC power is lost.
■■■■
or
pr
in
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Note: The ACARS automatically reverts to VOX
MODE. The DATA MODE is inoperative.
ad
ed
ACARS MU Fail or DU Fail
YR323, YR339
The ACARS system is failed.
do
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Condition:
1 Use normal voice procedures for reporting.
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if
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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D6-27370-8AS-NOK
5.1
5.2
737 Flight Crew Operations Manual
Radio Transmit Continuous
(Stuck Microphone Switch)
Condition:
A radio transmits continuously without crew
input.
or
pr
in
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d
1 MIC SELECTOR switches
(all audio selector panels) . . . . . . . . . . . .FLT INT
This deselects radios and stops radio
transmissions.
ad
ed
Note: The microphone/interphone with the stuck
switch continuously transmits on flight
interphone.
do
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2 The associated audio selector panel should stay on
flight interphone. All other audio selector panels
may be used normally.
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■■■■
5.2
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NNC.6-Electrical
6
Electrical (tab)
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Electrical
Section 6
Table of Contents
Smoke, Fire or Fumes ........................ ►►8.10
NNC. 1
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BATTERY DISCHARGE .......................................6.1
DRIVE ............................................................6.1
ELEC ..............................................................6.2
LOSS OF BOTH ENGINE DRIVEN GENERATORS.....6.3
Smoke, Fire or Fumes ........................ ►►8.10
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SOURCE OFF ................................................. 6.10
STANDBY POWER OFF..................................... 6.12
TR UNIT........................................................ 6.12
TRANSFER BUS OFF........................................ 6.14
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737 Flight Crew Operations Manual
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Table of Contents
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6.1
737 Flight Crew Operations Manual
BATTERY DISCHARGE
BAT
DISCHARGE
BATTERY DISCHARGE
File Highlight
Electrical
Smoke,
Fire or Fumes ►►8.10
Condition:
A battery discharge exceedance occurs.
■■■■
DRIVE
DRIVE
DRIVE
A generator drive malfunction occurs.
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Condition:
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Note: Fully charged batteries supply a minimum of
60 minutes of standby power.
Action is irreversible.
Generator drive
DISCONNECT switch
(affected side) . . . . . Confirm . . . . Hold in the
DISCONNECT
position momentarily
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1
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This prevents generator drive damage.
2 Choose one:
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APU is available for start:
APU . . . . . . . . . . . . . . . . . . . . . . START
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When APU is running:
APU GEN switch
(affected side) . . . . . . . . . . . . . ON
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■■■■
APU is not available:
Plan to land at the nearest suitable airport.
Only one main AC power source remains.
■■■■
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6.1
6.2
737 Flight Crew Operations Manual
ELEC
ELEC
ELEC
Condition:
A standby power or DC system fault occurs.
1 Do not takeoff.
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Note: The ELEC light illuminates on the ground
only.
6.2
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6.3
737 Flight Crew Operations Manual
TRANSFER
SOURCE
GEN
OFF OFF
OFF,
BUS,
BUS
(both)
TRANSFER
SOURCE
OFF, SOURCE
OFF
BUS
andOFF
TRANSFER
and GEN BUS
OFF BUS
(both
OFF (both
sides)sides)
LOSS OF BOTH ENGINE DRIVEN
GENERATORS
GEN 1 & 2
GEN 1 & 2
GEN 1 & 2
SOURCE
OFF
GEN OFF
BUS
TRANSFER
BUS OFF
Both engine driven generators are off.
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Condition:
Note: At high altitude, thrust deterioration or
engine flameout can occur.
1 Engine GEN switches (both). . . ON, one at a time
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2 Choose one:
A single SOURCE OFF light stays illuminated:
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►►Go to step 3
Both SOURCE OFF lights stay illuminated:
►►Go to step 5
if
Both SOURCE OFF lights extinguish:
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YAW DAMPER switch . . . . . . . . . . . . . ON
►►Go to step 17
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A single SOURCE OFF light stays illuminated
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3 YAW DAMPER switch . . . . . . . . . . . . . . . . . . . ON
▼ Continued on next page ▼
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6.3
6.4
737 Flight Crew Operations Manual
▼LOSS OF BOTH ENGINE DRIVEN GENERATORS continued▼
4 Choose one:
APU is available for start:
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Note: APU start attempts are not
recommended above 25,000 feet.
APU . . . . . . . . . . . . . . . . . . . . . . START
When APU is running:
►►Go to step 17
APU is not available:
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APU GEN switch
(affected side) . . . . . . . . . . . . . ON
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Plan to land at the nearest suitable airport.
Only one main AC power source remains.
►►Go to step 17
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▼ Continued on next page ▼
6.4
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6.5
737 Flight Crew Operations Manual
▼LOSS OF BOTH ENGINE DRIVEN GENERATORS continued▼
Both SOURCE OFF lights stay illuminated
5 Choose one:
APU is available for start:
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BUS TRANSFER switch . . . . . . . . . . . OFF
ELEC HYD PUMP switches (both) . . . . OFF
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Note: APU start attempts are not
recommended above 25,000 feet.
With both buses off, only one start
attempt is recommended. Multiple
start attempts reduce standby
power capacity.
APU . . . . . . . . . . . . . . . . . . . . . . START
►►Go to step 6
APU is not available:
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►►Go to step 14
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6 When APU is running:
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APU GEN
switches (both) . . . . . . . . . . . . . . . . . . . ON,
one at a time
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7 Check for the REMOTE CONTROL Circuit Breaker
(RCCB Remote P6-SPCU-A-4).
▼ Continued on next page ▼
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6.5
6.6
737 Flight Crew Operations Manual
▼LOSS OF BOTH ENGINE DRIVEN GENERATORS continued▼
8 Choose one:
RCCB REMOTE circuit breaker is tripped:
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Reset circuit breaker. Only one reset is
allowed.
►►Go to step 9
RCCB REMOTE circuit breaker is not tripped:
9 Choose one:
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►►Go to step 9
A single or both SOURCE OFF lights
extinguish:
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►►Go to step 10
Both SOURCE OFF lights stay illuminated:
if
►►Go to step 14
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10 BUS TRANSFER switch . . . . . . . . . . . . . . . AUTO
on
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This restores power to the remaining transfer
bus if one SOURCE OFF light stays illuminated.
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11 ELEC HYD PUMP
switches (both) . . . . . . . . . . . ON, one at a time
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12 YAW DAMPER switch . . . . . . . . . . . . . . . . . . . ON
13 Plan to land at the nearest suitable airport. Only
one main AC power source remains.
►►Go to step 17
▼ Continued on next page ▼
6.6
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6.7
737 Flight Crew Operations Manual
▼LOSS OF BOTH ENGINE DRIVEN GENERATORS continued▼
Both SOURCE OFF lights stay illuminated
14 Avoid icing conditions.
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Note: Flight in icing conditions can result in
erroneous flight instrument indications.
15 Plan to land at the nearest suitable airport.
Note: Fully charged batteries supply a minimum of
60 minutes of standby power.
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16 The right IRS will operate on DC power for 5
minutes.
17 Choose one:
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Both the captain’s and first officer’s primary
attitude displays are operative and ATT flags are
not shown:
■■■■
on
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if
Both the captain’s and first officer’s primary
attitude displays are failed:
►►Go to step 19
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Only the first officer’s primary attitude display
is failed:
IRS TRANSFER switch . . . . . . BOTH ON L
Do not engage either autopilot.
►►Go to step 18
▼ Continued on next page ▼
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6.7
6.8
737 Flight Crew Operations Manual
▼LOSS OF BOTH ENGINE DRIVEN GENERATORS continued▼
18 Choose one:
A single SOURCE OFF light is illuminated:
■■■■
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Plan to land at the nearest suitable airport.
Only one main AC power source remains.
Both SOURCE OFF lights are extinguished:
■■■■
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Both SOURCE OFF lights are illuminated:
The left IRS will operate as long as battery
power remains.
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Plan to land at the nearest suitable airport.
■■■■
19
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Action is irreversible. Do this step only if both
the captain’s and first officer’s primary attitude
displays are failed.
IRS MODE selectors (both). . . . . . . . . . . . ATT
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Maintain straight and level, constant airspeed
flight until attitude displays recover
(approximately 30 seconds).
The primary attitude displays stay failed and the
SET IRS HDG prompt on the POS INIT page is
blank until the attitude mode alignment is
complete.
▼ Continued on next page ▼
6.8
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6.9
737 Flight Crew Operations Manual
▼LOSS OF BOTH ENGINE DRIVEN GENERATORS continued▼
20 Enter magnetic heading on the POS INIT page or
on the overhead IRS display unit by selecting
HDG/STS.
Note: The MAP display is not available.
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Note: Periodically enter updated heading on the
POS INIT page or on the overhead IRS
display unit by selecting HDG/STS.
21 Do not engage either autopilot.
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6.9
6.10
737 Flight Crew Operations Manual
SOURCE OFF (single)
SOURCE
OFF
Condition:
SOURCE OFF
The transfer bus is not powered by the last
selected source.
1 Choose one:
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Both SOURCE OFF lights are illuminated:
►►Go to the LOSS OF BOTH ENGINE
DRIVEN GENERATORS checklist on
page 6.3
■■■■
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►►Go to step 2
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Only one SOURCE OFF light is illuminated:
2 Engine GEN switch (affected side) . . . . . . . . . ON
3 Choose one:
■■■■
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SOURCE OFF light extinguishes:
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SOURCE OFF light stays illuminated:
►►Go to step 4
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▼ Continued on next page ▼
6.10
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6.11
737 Flight Crew Operations Manual
▼SOURCE OFF continued▼
4 Choose one:
APU is available for start:
When APU is running:
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APU . . . . . . . . . . . . . . . . . . . . . . START
APU GEN switch
(affected side) . . . . . . . . . . . . . ON
APU is not available:
ad
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►►Go to step 5
Plan to land at the nearest suitable airport.
Only one main AC power source remains.
5 Choose one:
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■■■■
■■■■
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SOURCE OFF light extinguishes:
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SOURCE OFF light stays illuminated:
■■■■
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Plan to land at the nearest suitable airport.
Only one main AC power source remains.
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6.11
6.12
737 Flight Crew Operations Manual
STANDBY PWR OFF
STANDBY
PWR OFF
One or more of these busses are not
energized:
•AC standby bus
•DC standby bus
•Battery bus.
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Condition:
STANDBY POWER OFF
1 STANDBY POWER switch . . . . . . . . . . . . . . . BAT
■■■■
TR UNIT
TR UNIT
TR UNIT
One or more transformer rectifiers are
failed.
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Condition:
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YR323, YR339
1 Do not use the AFDS approach mode during an ILS
or GLS approach.
d
if
YK820, YL061, YR591 - YW351
2 Do not use the AFDS approach mode during an ILS
approach.
on
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Note: Autoland is not available.
YR323, YR339
■■■■
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Note: The AFDS approach mode can be used during
an instrument approach using IAN.
6.12
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6.13
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6.13
6.14
737 Flight Crew Operations Manual
TRANSFER BUS OFF
TRANSFER
BUS OFF
Condition:
TRANSFER BUS OFF
The transfer bus is not energized.
1 Engine GEN switch (affected side) . . . . . . . . . ON
2 Choose one:
■■■■
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TRANSFER BUS OFF light extinguishes:
TRANSFER BUS OFF light stays illuminated:
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►►Go to step 3
3 Choose one:
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APU is available for start:
APU . . . . . . . . . . . . . . . . . . . . . . START
When APU is running:
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if
APU GEN switch
(affected side) . . . . . . . . . . . . . ON
on
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►►Go to step 4
Plan to land at the nearest suitable airport.
Only one main AC power source remains.
■■■■
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APU is not available:
▼ Continued on next page ▼
6.14
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6.15
737 Flight Crew Operations Manual
▼TRANSFER BUS OFF continued▼
4 Choose one:
TRANSFER BUS OFF light extinguishes:
■■■■
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TRANSFER BUS OFF light stays illuminated:
Plan to land at the nearest suitable airport.
Only one main AC power source remains.
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■■■■
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6.15
6.16
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6.16
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7 Engines, APU (tab)
NNC.7-Engines,
APU
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Engines, APU
Section 7
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Table of Contents
Aborted Engine Start.....................................7.1
APU FIRE .................................................................. ►►8.1
Engine Fire on the Ground.................... ►►Back Cover.2
ENGINE FIRE or Engine Severe Damage or
Separation ................................................................ ►►8.2
Engine Limit or Surge or Stall .......................7.2
ENGINE OVERHEAT ................................................ ►►8.7
Engine Tailpipe Fire................................................. ►►8.8
Loss Of Thrust On Both Engines ....................7.6
NNC. 11
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Aborted Engine Start.....................................7.1
APU DETECTION INOPERATIVE ........................ ►►8.14
APU FAULT .................................................... 7.11
APU FIRE .................................................................. ►►8.1
APU LOW OIL PRESSURE................................. 7.12
APU OVERSPEED ............................................ 7.12
EEC ALTERNATE MODE ................................... 7.14
ENGINE CONTROL .......................................... 7.15
Engine Failure or Shutdown ............................. 7.16
Engine Fire on the Ground.................... ►►Back Cover.2
ENGINE FIRE or Engine Severe Damage or
Separation ................................................................ ►►8.2
ENGINE FIRE/OVERHEAT DETECTOR FAULT . ►►8.19
Engine High Oil Temperature ........................... 7.20
Engine High Vibration ..................................... 7.24
Engine In-Flight Start ..................................... 7.26
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737 Flight Crew Operations Manual
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Table of Contents
Engine Limit or Surge or Stall .......................7.2
ENGINE LOW OIL PRESSURE............................7.30
ENGINE OIL FILTER BYPASS ............................7.32
ENGINE OVERHEAT................................................. ►►8.7
Engine Tailpipe Fire ................................................. ►►8.8
Fuel Leak Engine................................................... ►►12.6
Loss Of Thrust On Both Engines ....................7.6
One Engine Inoperative Landing .......................7.34
One Engine Inoperative Landing .......................7.38
REVERSER.....................................................7.42
REVERSER UNLOCKED (IN FLIGHT) ..................7.43
START VALVE OPEN ........................................7.44
Volcanic Ash ..................................................7.46
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7.1
737 Flight Crew Operations Manual
Engines,
File
Highlight
APU
Aborted Engine Start
Condition:
On the ground, an aborted engine start is
needed.
Objective:
To shut down the engine and motor it.
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1 Engine start lever (affected engine) . . . . CUTOFF
----------------------2 Choose one:
ENGINE START switch is in GRD:
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Motor the engine for 60 seconds.
ENGINE START switch
(affected engine) . . . . . . . . . . . . . . . OFF
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■■■■
ENGINE START switch is in OFF:
if
►►Go to step 3
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3 After N2 decreases below 20%:
ENGINE START switch
(affected engine) . . . . . . . . . . . . . . . . . . GRD
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Motor the engine for 60 seconds.
ENGINE START switch
(affected engine) . . . . . . . . . . . . . . . . . . OFF
■■■■
ENGINE FIRE or Engine Severe Damage or Separation ►►8.2
Engine Fire on the Ground ►►Back Cover.2
APU FIRE ►►8.1
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7.1
7.2
737 Flight Crew Operations Manual
Engine Limit or Surge or Stall
One or more of these occur:
•Engine indications are abnormal
•Engine indications are rapidly approaching
or exceeding limits
•Abnormal engine noises are heard,
possibly with airframe vibration
•There is no response to thrust lever
movement or the response is abnormal
•Flames in the engine inlet or exhaust are
reported.
Objective:
To attempt to recover normal engine operation or shut down the engine if recovery is
not possible.
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Condition:
1 Autothrottle (if engaged) . . . . . . . . . . .Disengage
d
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2 Thrust lever
(affected engine) . . . . Confirm. . . . .Retard until
engine indications
stay within limits or
the thrust lever is closed
on
tro
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----------------------3 Choose one:
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Engine indications are stabilized and EGT is
stabilized or decreasing:
►►Go to step 4
Engine indications are abnormal or EGT
continues to increase:
►►Go to step 7
▼ Continued on next page ▼
7.2
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737 Flight Crew Operations Manual
▼Engine Limit or Surge or Stall continued▼
Check that RPM and EGT follow
thrust lever movement.
4
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Thrust lever
(affected engine). . . . . . . . . . . Advance slowly
5 Run the engine normally or at a reduced thrust
setting that is surge and stall free.
6 Choose one:
Engine runs normally:
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Engine runs at reduced thrust:
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Note: Do not use FMC performance
predictions.
YK820, YL061, YR591 - YS823
Transponder mode selector . . . . . . . . . TA
on
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This step prevents climb commands
which can exceed reduced thrust
performance capability.
nc
YR323, YR339, YV081 - YW351
Transponder mode selector . . . . . TA ONLY
This step prevents climb commands
which can exceed reduced thrust
performance capability.
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7 Engine start lever
(affected engine) . . . . . . Confirm . . . . . CUTOFF
▼ Continued on next page ▼
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7.3
7.4
737 Flight Crew Operations Manual
▼Engine Limit or Surge or Stall continued▼
8 PACK switch (affected side) . . . . . . . . . . . . . OFF
This causes the operating pack to regulate to
high flow in flight with flaps up.
APU is available for start:
or
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9 Choose one:
APU . . . . . . . . . . . . . . . . . . . . . . START
When APU is running:
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►►Go to step 10
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APU GEN switch
(affected side) . . . . . . . . . . . . . ON
APU is not available:
►►Go to step 10
if
10 Balance fuel as needed.
on
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YK820, YL061, YR591 - YS823
11 Transponder mode selector . . . . . . . . . . . . . . TA
This prevents climb commands which can
exceed single engine performance capability.
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YR323, YR339, YV081 - YW351
12 Transponder mode selector . . . . . . . . . . TA ONLY
This prevents climb commands which can
exceed single engine performance capability.
13 ISOLATION VALVE switch. . . . . . . . . Verify AUTO
This ensures bleed air is available to both wings
if wing anti-ice is needed.
▼ Continued on next page ▼
7.4
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7.5
737 Flight Crew Operations Manual
▼Engine Limit or Surge or Stall continued▼
14 A restart may be attempted if there is N1 rotation
and no abnormal airframe vibration.
15 Choose one:
or
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Restart will be attempted:
►►Go to the Engine In-Flight Start
checklist on page 7.26
■■■■
Restart will not be attempted:
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►►Go to step 16
16 Plan to land at the nearest suitable airport.
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Note: Do not use FMC performance predictions.
YK820, YL061, YR339 - YW351
on
tro
lle
YR323
■■■■
d
if
►►Go to the One Engine Inoperative
Landing checklist on page 7.34
►►Go to the One Engine Inoperative
Landing checklist on page 7.38
nc
■■■■
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Engine Tailpipe Fire ►►8.8
ENGINE OVERHEAT ►►8.7
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7.5
7.6
737 Flight Crew Operations Manual
ENG FAIL (both)
Objective:
To restart at least one engine.
or
pr
in
te
d
Condition:
Loss Of Thrust On Both Engines
Both of these occur:
•Both engines have a loss of thrust
•Both ENG FAIL alerts show.
1 ENGINE START switches (both) . . . . . . . . . . FLT
2 Engine start levers (both) . . . . . . . . . . . CUTOFF
3 When EGT decreases:
ad
ed
Engine start levers (both) . . . . . . IDLE detent
4 If EGT reaches a redline or there is no increase in
EGT within 30 seconds:
do
w
nl
o
Engine start lever
(affected engine) . . . . Confirm . . . . . CUTOFF,
then IDLE detent
d
if
If EGT again reaches a redline or there is no
increase in EGT within 30 seconds, repeat as
needed.
on
tro
lle
----------------------5 At or above FL270, set airspeed to 275 knots.
Below FL270, set airspeed to 300 knots.
U
nc
6 Engines can accelerate to idle very slowly,
especially at high altitudes or in heavy
precipitation. If N2 is steadily increasing and EGT
stays within limits, do not interrupt the start.
7 Do not wait for a successful engine start before
starting the APU.
▼ Continued on next page ▼
7.6
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7.7
737 Flight Crew Operations Manual
▼Loss Of Thrust On Both Engines continued▼
8 Choose one:
APU is available for start:
►►Go to step 9
APU is not available:
►►Go to step 10
9 When APU is running:
or
pr
in
te
d
APU . . . . . . . . . . . . . . . . . . . . . . START
do
w
nl
o
10 Choose one:
ad
ed
APU GEN switches
(both) . . . . . . . . . . . . . . . . ON, one at a time
One or both engines start:
►►Go to step 15
if
Neither engine starts:
on
tro
lle
d
►►Go to step 11
11 Choose one:
U
nc
N2 is at or above 11%:
Attempt a windmill start.
►►Go to step 13
N2 is below 11%:
►►Go to step 12
▼ Continued on next page ▼
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March 31, 2023
D6-27370-8AS-NOK
7.7
7.8
737 Flight Crew Operations Manual
▼Loss Of Thrust On Both Engines continued▼
12 Choose one:
APU bleed air is available:
►►Go to step 16
APU bleed air is not available:
Attempt a windmill start.
►►Go to step 13
or
pr
in
te
d
Attempt a starter assist start.
ad
ed
13 Thrust levers (both) . . . . . . . . . . . . . . . . . Close
do
w
nl
o
14 Engine start
lever (either) . . . . . . Confirm. . . . . . . CUTOFF,
then IDLE detent
on
tro
lle
d
if
The engine can accelerate to idle very slowly
especially at high altitudes or in heavy
precipitation. If N2 is steadily increasing and
EGT stays within limits, do not interrupt the
start.
15 When engine parameters have stabilized:
ENGINE START switch
(operating engine) . . . . . . . . . . . . .As needed
U
nc
Thrust lever
(operating engine) . . . . . . . . . Advance slowly
Engine GEN switch
(operating engine side) . . . . . . . . . . . . . . . ON
►►Go to step 25
16 Thrust levers (both) . . . . . . . . . . . . . . . . . Close
▼ Continued on next page ▼
7.8
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7.9
737 Flight Crew Operations Manual
▼Loss Of Thrust On Both Engines continued▼
17 WING ANTI–ICE switch . . . . . . . . . . . . . . . . OFF
18 PACK switches (both) . . . . . . . . . . . . . . . . . OFF
19 APU BLEED air switch . . . . . . . . . . . . . . . . . . ON
or
pr
in
te
d
20 Ignition select switch . . . . . . . . . . . . . . . . BOTH
21 Engine start
lever (either) . . . . . . Confirm. . . . . . . CUTOFF
22 ENGINE START switch . . . . . . . . . . . . . . . . GRD
23 When N2 is at or above 11%:
ad
ed
Engine start lever . . . . . . . . . . . .IDLE detent
do
w
nl
o
The engine can accelerate to idle very
slowly especially at high altitudes or in
heavy precipitation. If N2 is steadily
increasing and EGT stays within limits, do
not interrupt the start.
d
if
24 When engine parameters have stabilized:
on
tro
lle
APU BLEED air switch . . . . . . . . . . . . . . . OFF
U
nc
ENGINE START switch
(operating engine) . . . . . . . . . . . . .As needed
Thrust lever
(operating engine) . . . . . . . . . Advance slowly
Engine GEN switch
(operating engine side) . . . . . . . . . . . . . . . ON
PACK switch
(operating engine side) . . . . . . . . . . . . . AUTO
▼ Continued on next page ▼
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March 31, 2023
D6-27370-8AS-NOK
7.9
7.10
737 Flight Crew Operations Manual
▼Loss Of Thrust On Both Engines continued▼
25 Choose one:
Both the captain’s and first officer’s primary
attitude displays are operative and ATT flags are
not shown:
or
pr
in
te
d
►►Go to step 30
Both the captain’s and first officer’s primary
attitude displays are failed:
►►Go to step 26
ad
ed
Only the first officer’s primary attitude display
is failed:
do
w
nl
o
IRS TRANSFER switch. . . . . . . BOTH ON L
Do not engage either autopilot.
►►Go to step 30
26
on
tro
lle
d
if
Action is irreversible. Do this step only if both
the captain’s and first officer’s primary attitude
displays are failed.
IRS MODE selectors (both). . . . . . . . . . . . ATT
U
nc
Maintain straight and level, constant airspeed
flight until attitude displays recover
(approximately 30 seconds).
The primary attitude displays stay failed and the
SET IRS HDG prompt on the POS INIT page is
blank until the attitude mode alignment is
complete.
▼ Continued on next page ▼
7.10
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7.11
737 Flight Crew Operations Manual
▼Loss Of Thrust On Both Engines continued▼
27 Enter magnetic heading on the POS INIT page or
on the overhead IRS display unit by selecting
HDG/STS.
28 The MAP display is not available.
or
pr
in
te
d
Note: Periodically enter updated heading on the
POS INIT page or on the overhead IRS
display unit by selecting HDG/STS.
29 Do not engage either autopilot.
30 Choose one:
ad
ed
Both engines are running:
Run the APU as needed.
do
w
nl
o
■■■■
One engine stays failed:
on
tro
lle
d
if
►►Go to the Engine In-Flight Start
checklist on page 7.26
FAULT - APU
APU DETECTION INOPERATIVE ►►8.14
FAULT
Condition:
■■■■
APU FAULT
An APU malfunction occurs.
nc
Note: The APU shuts down automatically.
U
1 APU switch . . . . . . . . . . . . . . . . . . . . . . . . OFF
If the APU FAULT light extinguishes after 5
minutes, restarts may be attempted.
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
7.11
7.12
737 Flight Crew Operations Manual
LOW OIL PRESSURE - APU
LOW OIL
PRESSURE
Condition:
APU LOW OIL PRESSURE
The APU oil pressure is low.
Note: The APU shuts down automatically.
or
pr
in
te
d
1 APU switch. . . . . . . . . . . . . . . . . . . . . . . . . OFF
The LOW OIL PRESSURE light extinguishes in 5
minutes.
■■■■
OVER SPEED - APU
OVER
SPEED
ad
ed
One of these occurs:
•An APU RPM limit exceedance causes
automatic shutdown
•During a normal APU shutdown the
overspeed shutdown protection logic fails
a self-test.
do
w
nl
o
Condition:
APU OVERSPEED
if
1 APU switch. . . . . . . . . . . . . . . . . . . . . . . . . OFF
■■■■
U
nc
on
tro
lle
d
The APU OVERSPEED light extinguishes in 5
minutes.
7.12
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D6-27370-8AS-NOK
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7.13
do
w
nl
o
ad
ed
or
pr
in
te
d
737 Flight Crew Operations Manual
U
nc
on
tro
lle
d
if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
7.13
7.14
737 Flight Crew Operations Manual
ALTN - EEC
EEC ALTERNATE MODE
ALTN
Condition:
An EEC operates in the alternate control
mode.
1 Autothrottle (if engaged) . . . . . . . . . . .Disengage
or
pr
in
te
d
2 Thrust levers (both) . . . . . Retard to mid position
This prevents exceeding thrust limits when
switching to the EEC alternate mode.
3 EEC mode switches (one at a time). . . . . . . ALTN
ad
ed
This ensures both engines operate in alternate
mode.
4 Autothrottle (if needed). . . . . . . . . . . . . . Engage
do
w
nl
o
Note: Maximum thrust limiting is available with
autothrottle engaged.
d
6 Choose one:
if
5 Do not exceed engine limits. Engine limit protection
in alternate mode is not the same as in normal
mode.
on
tro
lle
DSPLY SOURCE 1 or DSPLY SOURCE 2
annunciation is shown:
►►Go to step 7
U
nc
DSPLY SOURCE 1 and DSPLY SOURCE 2
annunciations are not shown:
■■■■
▼ Continued on next page ▼
7.14
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D6-27370-8AS-NOK
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7.15
737 Flight Crew Operations Manual
▼EEC ALTERNATE MODE continued▼
7 Choose one:
DISPLAY SOURCE checklist has been completed:
■■■■
or
pr
in
te
d
DISPLAY SOURCE checklist has not been
completed:
►►Go to the DISPLAY SOURCE
checklist on page 10.26
ad
ed
■■■■
ENGINE CONTROL
ENGINE
CONTROL
An engine control system fault occurs.
do
w
nl
o
Condition:
ENGINE CONTROL
Note: An ENGINE CONTROL light illuminates on the
ground only.
■■■■
U
nc
on
tro
lle
d
if
1 Do not takeoff.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
7.15
7.16
737 Flight Crew Operations Manual
ENG FAIL (single)
Engine Failure or Shutdown
One of these occurs:
•An engine failure
•An ENG FAIL alert shows
•An engine flameout
•Another checklist directs an engine
shutdown.
or
pr
in
te
d
Condition:
1 Choose one:
Airframe vibrations with abnormal engine
indications exist:
ad
ed
►►Go to the ENGINE FIRE or Engine
Severe Damage or Separation
checklist on page 8.2
do
w
nl
o
■■■■
An engine has separated:
on
tro
lle
d
if
►►Go to the ENGINE FIRE or Engine
Severe Damage or Separation
checklist on page 8.2
■■■■
►►Go to step 2
U
nc
Airframe vibrations with abnormal engine
indications do not exist and an engine has not
separated:
2 Do an engine shutdown only when flight conditions
allow.
3 Autothrottle (if engaged) . . . . . . . . . . .Disengage
▼ Continued on next page ▼
7.16
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7.17
737 Flight Crew Operations Manual
▼Engine Failure or Shutdown continued▼
4 Thrust lever
(affected engine) . . . . . . Confirm . . . . . . . Close
5 When the affected engine is at idle thrust:
or
pr
in
te
d
Engine start lever
(affected engine) . . . . Confirm . . . . . CUTOFF
6 PACK switch (affected side) . . . . . . . . . . . . . OFF
This causes the operating pack to regulate to
high flow in flight with flaps up.
ad
ed
7 Choose one:
APU is available for start:
do
w
nl
o
APU . . . . . . . . . . . . . . . . . . . . . . START
When APU is running:
if
APU GEN switch
(affected side) . . . . . . . . . . . . . ON
on
tro
lle
d
►►Go to step 8
APU is not available:
►►Go to step 8
nc
8 Balance fuel as needed.
U
YK820, YL061, YR591 - YS823
9 Transponder mode selector . . . . . . . . . . . . . . TA
This prevents climb commands which can
exceed single engine performance capability.
▼ Continued on next page ▼
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September 30, 2022
D6-27370-8AS-NOK
7.17
7.18
737 Flight Crew Operations Manual
▼Engine Failure or Shutdown continued▼
YR323, YR339, YV081 - YW351
10 Transponder mode selector . . . . . . . . . . TA ONLY
This prevents climb commands which can
exceed single engine performance capability.
or
pr
in
te
d
11 ISOLATION VALVE switch. . . . . . . . . Verify AUTO
This ensures bleed air is available to both wings
if wing anti-ice is needed.
12 A restart may be attempted if there is N1 rotation
and no abnormal airframe vibration.
ad
ed
13 Choose one:
A restart will be attempted:
do
w
nl
o
►►Go to the Engine In-Flight Start
checklist on page 7.26
■■■■
if
A restart will not be attempted:
on
tro
lle
d
►►Go to step 14
14 Plan to land at the nearest suitable airport.
Note: Do not use FMC performance predictions.
YK820, YL061, YR339 - YW351
U
nc
►►Go to the One Engine Inoperative
Landing checklist on page 7.34
■■■■
▼ Continued on next page ▼
7.18
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D6-27370-8AS-NOK
September 30, 2022
7.19
737 Flight Crew Operations Manual
▼Engine Failure or Shutdown continued▼
YR323
►►Go to the One Engine Inoperative
Landing checklist on page 7.38
or
pr
in
te
d
■■■■
U
nc
on
tro
lle
d
if
do
w
nl
o
ad
ed
ENGINE FIRE/OVERHEAT DETECTOR FAULT ►►8.19
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 14, 2017
D6-27370-8AS-NOK
7.19
7.20
737 Flight Crew Operations Manual
Engine High Oil Temperature
Condition:
The engine oil temperature is high.
1 Choose one:
or
pr
in
te
d
Temperature is at or above the redline:
►►Go to the Engine Failure or
Shutdown checklist on page 7.16
■■■■
►►Go to step 2
ad
ed
Temperature is in the amber band:
2 Autothrottle (if engaged) . . . . . . . . . . .Disengage
d
if
do
w
nl
o
3 Thrust lever
(affected engine) . . . . . . Confirm . . . . . . Retard
slowly until the
engine oil temperature
is within the normal operating range
or the thrust lever is closed
U
nc
on
tro
lle
▼ Continued on next page ▼
7.20
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D6-27370-8AS-NOK
September 14, 2017
7.21
737 Flight Crew Operations Manual
▼Engine High Oil Temperature continued▼
YK820, YL061, YR591 - YS823
4 Choose one:
Oil temperature is in the amber band for 45
minutes or less:
or
pr
in
te
d
Note: Run the affected engine at a thrust
setting that keeps the engine oil
temperature within the normal
operating range.
ad
ed
Do not use FMC performance
predictions.
Transponder mode selector . . . . . . . . . TA
do
w
nl
o
This step prevents climb commands
which can exceed reduced thrust
performance capability.
■■■■
d
if
Oil temperature is in the amber band for more
than 45 minutes:
nc
on
tro
lle
►►Go to the Engine Failure or
Shutdown checklist on page 7.16
■■■■
U
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
7.21
7.22
737 Flight Crew Operations Manual
▼Engine High Oil Temperature continued▼
YR323, YR339, YV081 - YW351
5 Choose one:
Oil temperature is in the amber band for 45
minutes or less:
or
pr
in
te
d
Note: Run the affected engine at a thrust
setting that keeps the engine oil
temperature within the normal
operating range.
ad
ed
Do not use FMC performance
predictions.
Transponder mode selector . . . . . TA ONLY
do
w
nl
o
This step prevents climb commands
which can exceed reduced thrust
performance capability.
■■■■
d
if
Oil temperature is in the amber band for more
than 45 minutes:
■■■■
U
nc
on
tro
lle
►►Go to the Engine Failure or
Shutdown checklist on page 7.16
7.22
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D6-27370-8AS-NOK
March 21, 2019
7.23
do
w
nl
o
ad
ed
or
pr
in
te
d
737 Flight Crew Operations Manual
U
nc
on
tro
lle
d
if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 14, 2017
D6-27370-8AS-NOK
7.23
7.24
737 Flight Crew Operations Manual
Engine High Vibration
Condition:
The vibration level is 4.0 units or greater.
Airframe vibration may or may not be felt.
1 Choose one:
or
pr
in
te
d
In icing conditions:
►►Go to step 2
Not in icing conditions:
►►Go to step 8
ad
ed
2 ENGINE START switches (both) . . . . . . . . . . FLT
do
w
nl
o
3 Autothrottle (if engaged) . . . . . . . . . . .Disengage
on
tro
lle
d
if
Do the next two steps on one engine at a time.
Thrust lever
4
(selected engine) . . . . . . . . . Retard to 45% N1
for five seconds,
then slowly advance
to a minimum of 80% N1
for approximately 1 second
5 Thrust lever
(selected engine) . . . . . . . . . . Reduce as needed
for flight conditions
U
nc
6 Wait 15 seconds. This allows the engine vibration
level to stabilize.
7.24
▼ Continued on next page ▼
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D6-27370-8AS-NOK
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7.25
737 Flight Crew Operations Manual
▼Engine High Vibration continued▼
7 Choose one:
Vibration level is less than 4 units:
■■■■
or
pr
in
te
d
Continue normal operation.
Vibration level is 4 units or greater:
►►Go to step 9
ad
ed
8 Autothrottle (if engaged). . . . . . . . . . .Disengage
do
w
nl
o
9 Thrust lever
(affected engine) . . . . Confirm. . . . . . Retard to
maintain vibration
levels below 4 units or
until the thrust lever is closed
on
tro
lle
d
if
Note: If the VIB indication does not decrease when
the thrust lever is retarded, check other
engine indications on the affected engine. If
other engine indications are normal, run the
engine at reduced thrust.
Note: Do not use FMC performance predictions.
U
nc
YK820, YL061, YR591 - YS823
10 Transponder mode selector . . . . . . . . . . . . . . TA
This step prevents climb commands which can
exceed reduced thrust performance capability.
YR323, YR339, YV081 - YW351
11 Transponder mode selector . . . . . . . . . . TA ONLY
This step prevents climb commands which can
exceed reduced thrust performance capability.
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
7.25
7.26
737 Flight Crew Operations Manual
Engine In-Flight Start
An engine start is needed and all of the
following are true:
•There was no engine fire
•There is N1 rotation
•There is no abnormal airframe vibration.
or
pr
in
te
d
Condition:
Note: Oil quantity indication as low as zero is
normal if windmilling N2 RPM is below
approximately 8%.
ad
ed
1 Do this checklist only after completion of the
Engine Failure or Shutdown checklist or as directed
by the Engine Limit or Surge or Stall checklist or by
the Loss of Thrust on Both Engines checklist.
do
w
nl
o
2 Check the In-Flight Start Envelope. X-BLD or XB
indication may not match the envelope. Starts are
not assured outside of the In-flight Start Envelope.
if
Note: If the N2 is less than 8%, ENGINE START
switch must be in CONT to display the EGT.
U
nc
on
tro
lle
d
Note: For engines shut down one hour or more, or
if EGT is less than 30°C, attempt a restart:
7.26
•At an altitude at or below 20,000 feet
•With airspeed at or above 220 knots
•Using a crossbleed start.
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
September 20, 2018
7.27
737 Flight Crew Operations Manual
▼Engine In-Flight Start continued▼
24
20
15
WINDMILL
or
pr
in
te
d
PRESSURE ALTITUDE
1000 FEET
IN-FLIGHT START ENVELOPE
CROSSBLEED
140
ad
ed
281
220
300
340
do
w
nl
o
INDICATED AIRSPEED – KNOTS
3 Thrust lever
(affected engine) . . . . . . Confirm . . . . . . . Close
if
4 Engine start lever
(affected engine) . . . . . . Confirm . . . . . CUTOFF
▼ Continued on next page ▼
U
nc
on
tro
lle
d
5 Engines can accelerate to idle very slowly,
especially at high altitudes or in heavy
precipitation. If N2 is steadily increasing and EGT
stays within limits, do not interrupt the start.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 20, 2018
D6-27370-8AS-NOK
7.27
7.28
737 Flight Crew Operations Manual
▼Engine In-Flight Start continued▼
6 Choose one:
Windmill start:
or
pr
in
te
d
ENGINE START switch
(affected engine) . . . . . . . . . . . . . . . FLT
►►Go to step 7
Crossbleed start:
PACK switch (affected side). . . . . . . . OFF
ad
ed
DUCT PRESSURE . . . . . . Minimum 30 PSI
Advance the thrust lever to increase
duct pressure if needed.
do
w
nl
o
ENGINE START switch
(affected engine) . . . . . . . . . . . . . . . GRD
►►Go to step 7
if
7 When N2 is at or above 11%:
on
tro
lle
d
Engine start lever
(affected engine) . . . . . . . . . . . . IDLE detent
▼ Continued on next page ▼
U
nc
Monitor EGT to ensure it does not rise rapidly or
exceed the start limit during the start attempt.
7.28
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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September 20, 2018
7.29
737 Flight Crew Operations Manual
▼Engine In-Flight Start continued▼
8 Choose one:
EGT increases within 30 seconds and a normal
start occurs:
or
pr
in
te
d
►►Go to step 10
EGT does not increase within 30 seconds or
another abort start condition as listed in the
Normal Procedures occurs:
ad
ed
Engine start lever
(affected engine) . . . Confirm . . . CUTOFF
ENGINE START switch
(affected engine) . . . . . . . . . . . . . . . OFF
do
w
nl
o
Note: If the engine has been shutdown for
more than one hour, multiple start
attempts can be needed.
►►Go to step 9
if
9 Plan to land at the nearest suitable airport.
on
tro
lle
d
Note: Do not use FMC performance predictions.
YK820, YL061, YR339 - YW351
U
nc
►►Go to the One Engine Inoperative
Landing checklist on page 7.34
■■■■
YR323
►►Go to the One Engine Inoperative
Landing checklist on page 7.38
■■■■
10 Engine GEN switch (affected side) . . . . . . . . . ON
▼ Continued on next page ▼
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D6-27370-8AS-NOK
7.29
7.30
737 Flight Crew Operations Manual
▼Engine In-Flight Start continued▼
11 PACK switch (affected side) . . . . . . . . . . . . AUTO
12 ENGINE START switch . . . . . . . . . . . . .As needed
13 APU . . . . . . . . . . . . . . . . . . . . . . . . .As needed
■■■■
LOW OIL PRESSURE - Engine
or
pr
in
te
d
14 Transponder mode selector . . . . . . . . . . . .TA/RA
ENGINE LOW OIL PRESSURE
Condition:
ad
ed
LOW OIL May or may not be shown
PRESSURE
The engine oil pressure is low.
do
w
nl
o
1 Choose one:
Engine oil pressure is in the amber band with
takeoff thrust set:
■■■■
d
if
Do not takeoff.
on
tro
lle
Engine oil pressure is at or below the redline:
►►Go to the Engine Failure or
Shutdown checklist on page 7.16
U
nc
■■■■
7.30
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7.31
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or
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in
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d
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if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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7.31
7.32
737 Flight Crew Operations Manual
OIL FILTER BYPASS
OIL FILTER
BYPASS
Condition:
ENGINE OIL FILTER BYPASS
The OIL FILTER BYPASS alert indicates oil
filter contamination can cause oil to bypass
the oil filter.
or
pr
in
te
d
1 Autothrottle (if engaged) . . . . . . . . . . .Disengage
ad
ed
2 Thrust lever
(affected engine) . . . . . . Confirm . . . . . . Retard
slowly until the
OIL FILTER BYPASS
alert extinguishes or
the thrust lever is closed
3 Choose one:
do
w
nl
o
OIL FILTER BYPASS alert extinguishes:
►►Go to step 4
OIL FILTER BYPASS alert stays illuminated:
on
tro
lle
d
if
►►Go to the Engine Failure or
Shutdown checklist on page 7.16
■■■■
4 Run the engine at reduced thrust to keep the alert
extinguished.
nc
Note: Do not use FMC performance predictions.
U
YK820, YL061, YR591 - YS823
5 Transponder mode selector . . . . . . . . . . . . . . TA
This step prevents climb commands which can
exceed reduced thrust performance capability.
▼ Continued on next page ▼
7.32
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7.33
737 Flight Crew Operations Manual
▼ENGINE OIL FILTER BYPASS continued▼
YR323, YR339, YV081 - YW351
6 Transponder mode selector . . . . . . . . . . TA ONLY
■■■■
U
nc
on
tro
lle
d
if
do
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ad
ed
Fuel Leak Engine ►►12.6
or
pr
in
te
d
This step prevents climb commands which can
exceed reduced thrust performance capability.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 19, 2020
D6-27370-8AS-NOK
7.33
7.34
737 Flight Crew Operations Manual
One Engine Inoperative Landing
YK820, YL061, YR339 - YW351
Condition:
Landing must be made with one engine
inoperative.
or
pr
in
te
d
1 Plan a flaps 15 landing.
2 Set VREF 15 or VREF ICE.
Note: If any of the following conditions apply,
set VREF ICE = VREF 15 + 10 knots:
do
w
nl
o
ad
ed
•Engine anti–ice will be used during
landing
•Wing anti–ice has been used any
time during the flight
•Icing conditions were encountered
during the flight and the landing
temperature is below 10° C.
d
if
Note: When VREF ICE is needed, the wind
additive should not exceed 5 knots.
on
tro
lle
3 Check the Non-Normal Configuration Landing
Distance tables in the Performance Inflight-QRH
chapter or other approved source.
U
nc
4 Maintain VREF 15 + wind additive or VREF ICE +
wind additive on final approach to assure sufficient
maneuver margin and speed for go-around. The
minimum wind additive is 5 knots.
5 When engine anti-ice is needed, use on the
operating engine only.
6 Checklist Complete Except Deferred Items
▼ Continued on next page ▼
7.34
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September 30, 2022
7.35
737 Flight Crew Operations Manual
▼One Engine Inoperative Landing continued▼
Deferred Items
Descent Checklist
Pressurization. . . . . . . . . . . . . . . . . LAND ALT ___
or
pr
in
te
d
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing data . . . . . . . VREF 15 or VREF ICE ___,
Minimums ___
ad
ed
Approach briefing . . . . . . . . . . . . . . . . Completed
Additional Go-Around Thrust
do
w
nl
o
Choose one:
Additional go-around thrust is needed:
if
►►Go to No Engine Bleed Landing
below
d
Additional go-around thrust is not needed:
on
tro
lle
►►Go to Go-Around Procedure Review
below
nc
No Engine Bleed Landing
U
When below 10,000 feet:
WING ANTI-ICE switch . . . . . . . . . . . . . . OFF
ISOLATION VALVE switch . . . . . . . . . . CLOSE
BLEED 1 air switch . . . . . . . . . . . . . . . . . OFF
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 14, 2017
D6-27370-8AS-NOK
7.35
7.36
737 Flight Crew Operations Manual
▼One Engine Inoperative Landing continued▼
Do not open the APU bleed air valve if the
engine fire switch is illuminated.
APU BLEED air switch . . . . . . . . . . . . . . ON
or
pr
in
te
d
Left PACK switch . . . . . . . . . . . . . . . . . AUTO
BLEED 2 air switch . . . . . . . . . . . . . . . . . OFF
Go-Around Procedure Review
Do the normal go–around procedure except:
ad
ed
Use flaps 1.
do
w
nl
o
Maintain VREF 15 + 5 knots or VREF ICE + 5
knots until reaching flap retraction altitude.
if
Limit bank angle to 15° when airspeed is less
than VREF 15 + 15 knots or VREF ICE + 5 knots
or the minimum maneuver speed, whichever is
lower.
on
tro
lle
d
Accelerate to flaps 1 maneuvering speed before
flap retraction.
Approach Checklist
U
nc
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Additional Deferred Item
GROUND PROXIMITY
FLAP INHIBIT switch . . . . . . . . . . . . FLAP INHIBIT
▼ Continued on next page ▼
7.36
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7.37
737 Flight Crew Operations Manual
▼One Engine Inoperative Landing continued▼
Landing Checklist
ENGINE START switch
(operating engine). . . . . . . . . . . . . . . . . . CONT
or
pr
in
te
d
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps. . . . . . . . . . . . . . . . . . . . . . 15, Green light
U
nc
on
tro
lle
d
if
do
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ad
ed
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 14, 2017
D6-27370-8AS-NOK
7.37
7.38
737 Flight Crew Operations Manual
One Engine Inoperative Landing
YR323
Condition:
Landing must be made with one engine
inoperative.
or
pr
in
te
d
1 Choose one:
Landing using flaps 30 (if performance allows):
Use flaps 30 and VREF 30 for landing and
flaps 15 for go-around.
Landing using flaps 15:
do
w
nl
o
►►Go to step 2
ad
ed
►►Go to step 4
2 Use flaps 15 and VREF 15 or VREF ICE for landing
and flaps 1 for go-around.
if
Note: If any of the following conditions apply,
set VREF ICE = VREF 15 + 10 knots:
U
nc
on
tro
lle
d
•Engine anti–ice will be used during
landing
•Wing anti–ice has been used any
time during the flight
•Icing conditions were encountered
during the flight and the landing
temperature is below 10° C.
Note: When VREF ICE is needed, the wind
additive should not exceed 5 knots.
▼ Continued on next page ▼
7.38
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September 20, 2018
7.39
737 Flight Crew Operations Manual
▼One Engine Inoperative Landing continued▼
3 Maintain VREF 15 + wind additive or VREF ICE +
wind additive on final approach to assure sufficient
maneuver margin and speed for go-around. The
minimum wind additive is 5 knots.
or
pr
in
te
d
Note: Autoland operations are not authorized when
landing with flaps 15.
4 When engine anti-ice is needed, use on the
operating engine only.
ad
ed
5 Check the Non-Normal Configuration Landing
Distance tables in the Performance Inflight-QRH
chapter or other approved source.
6 Checklist Complete Except Deferred Items
do
w
nl
o
Deferred Items
Descent Checklist
Pressurization. . . . . . . . . . . . . . . . . LAND ALT ___
if
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
on
tro
lle
d
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing data . . . . . . . . . . . VREF ___ as directed
by checklist, Minimums ___
Approach briefing . . . . . . . . . . . . . . . . Completed
U
nc
Note: Check authorized autoland weather
minima.
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 14, 2017
D6-27370-8AS-NOK
7.39
7.40
737 Flight Crew Operations Manual
▼One Engine Inoperative Landing continued▼
Additional Go-Around Thrust
Choose one:
Additional go-around thrust is needed:
or
pr
in
te
d
►►Go to No Engine Bleed Landing
below
Additional go-around thrust is not needed:
do
w
nl
o
No Engine Bleed Landing
ad
ed
►►Go to Go-Around Procedure Review
below
When below 10,000 feet:
WING ANTI-ICE switch . . . . . . . . . . . . . . OFF
ISOLATION VALVE switch . . . . . . . . . . CLOSE
d
if
BLEED 1 air switch . . . . . . . . . . . . . . . . . OFF
on
tro
lle
Do not open the APU bleed air valve if the
engine fire switch is illuminated.
APU BLEED air switch . . . . . . . . . . . . . . ON
nc
Left PACK switch . . . . . . . . . . . . . . . . . AUTO
U
BLEED 2 air switch . . . . . . . . . . . . . . . . . OFF
Go-Around Procedure Review
Do the normal go-around procedure except:
▼ Continued on next page ▼
7.40
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D6-27370-8AS-NOK
September 14, 2017
7.41
737 Flight Crew Operations Manual
▼One Engine Inoperative Landing continued▼
Choose one:
Landing using flaps 30:
Use flaps 15.
or
pr
in
te
d
Maintain VREF 30 + 5 knots and limit bank
angle to 15° until initial maneuvering is
complete and a safe altitude is reached.
►►Go to Approach Checklist below
Use flaps 1.
ad
ed
Landing using flaps 15:
do
w
nl
o
Maintain VREF 15 + 5 knots or VREF ICE +
5 knots until reaching flap retraction
altitude.
d
if
Limit bank angle to 15° when airspeed is
less than VREF 15 + 15 knots or VREF ICE
+ 5 knots or the minimum maneuver
speed, whichever is lower.
on
tro
lle
Accelerate to flaps 1 maneuvering speed
before flap retraction.
►►Go to Approach Checklist below
U
nc
Approach Checklist
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 14, 2017
D6-27370-8AS-NOK
7.41
7.42
737 Flight Crew Operations Manual
▼One Engine Inoperative Landing continued▼
Additional Deferred Item
Choose one:
Landing using flaps 30:
or
pr
in
te
d
►►Go to Landing Checklist below
Landing using flaps 15:
GROUND PROXIMITY FLAP
INHIBIT switch . . . . . . . . . FLAP INHIBIT
ad
ed
►►Go to Landing Checklist below
do
w
nl
o
Landing Checklist
ENGINE START switch
(operating engine) . . . . . . . . . . . . . . . . . . CONT
if
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
d
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
REVERSER
on
tro
lle
Flaps . . . . . . . . . . . . . . . . . . . . . ___, Green light
nc
REVERSER
U
Condition:
■■■■
REVERSER
A fault occurs in the thrust reverser system.
1 Expect normal reverser operation after landing.
■■■■
7.42
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7.43
737 Flight Crew Operations Manual
REV
REVERSER UNLOCKED (IN FLIGHT)
Condition:
The amber REV indication shows with
uncommanded reverse thrust.
or
pr
in
te
d
Note: Only multiple failures could allow the engine
to go into reverse thrust.
Unstowed reverser sleeves produce buffet,
yaw, roll and increased airplane drag.
1 Check movement of the forward thrust lever on the
affected engine.
do
w
nl
o
ad
ed
The EECs prevent power above idle if the related
thrust reverser has moved from the stowed
position.
Warning! Do not actuate the reverse thrust
lever.
2 Choose one:
on
tro
lle
d
if
Engine responds to forward thrust lever
movement and no buffet or yaw exists:
Continue normal operation.
■■■■
U
nc
Engine does not respond to forward thrust lever
movement or buffet or yaw exists:
►►Go to the Engine Failure or
Shutdown checklist on page 7.16
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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D6-27370-8AS-NOK
7.43
7.44
737 Flight Crew Operations Manual
START VALVE OPEN
START VALVE
OPEN
Condition:
START VALVE OPEN
The START VALVE OPEN alert indicates the
start valve fails to close.
2 Choose one:
or
pr
in
te
d
1 ENGINE START switch . . . . . . . . . . . . . . . . . OFF
START VALVE OPEN alert extinguishes:
■■■■
►►Go to step 3
ad
ed
START VALVE OPEN alert stays illuminated:
3 ISOLATION VALVE switch. . . . . . . . . . . . . CLOSE
do
w
nl
o
4 PACK switch (affected side) . . . . . . . . . . . . . OFF
This causes the operating pack to regulate to
high flow in flight with flaps up.
d
if
5 Engine BLEED air switch
(affected side) . . . . . . . . . . . . . . . . . . . . . . OFF
U
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on
tro
lle
▼ Continued on next page ▼
7.44
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D6-27370-8AS-NOK
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7.45
737 Flight Crew Operations Manual
▼START VALVE OPEN continued▼
6 Choose one:
START VALVE OPEN alert stays illuminated for
engine 1:
►►Go to step 7
or
pr
in
te
d
APU BLEED air switch . . . . . . . . . . . OFF
START VALVE OPEN alert stays illuminated for
engine 2:
ad
ed
►►Go to step 7
START VALVE OPEN alert extinguishes:
7 Choose one:
In flight:
do
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o
►►Go to step 7
WING ANTI-ICE switch . . . . . . . . . . . OFF
on
tro
lle
d
if
This prevents possible asymmetrical
ice buildup on the wings.
Avoid icing conditions where wing anti-ice is
needed.
nc
■■■■
U
On the ground:
Ground air source
(if in use) . . . . . . . . . . . . . . . Disconnect
Engine start lever
(affected engine) . . . . . . . . . . . . CUTOFF
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 21, 2019
D6-27370-8AS-NOK
7.45
7.46
737 Flight Crew Operations Manual
Volcanic Ash
Volcanic ash is suspected when one or more
of these occur:
•A static discharge around the windshield
•A bright glow in the engine inlets
•Smoke or dust on the flight deck
•An acrid odor.
Objective:
To exit the ash cloud and restart engines if
needed.
or
pr
in
te
d
Condition:
do
w
nl
o
ad
ed
Caution! Exit the volcanic ash as quickly as
possible. Consider a 180° turn.
Consider a descending turn.
1 Don oxygen masks and smoke goggles, as needed.
2 Establish crew communications, as needed.
if
3 Autothrottle (if engaged) . . . . . . . . . . .Disengage
4
on
tro
lle
d
If conditions allow, run the engines at idle
thrust.
Thrust levers (both) . . . . . . . . . . . . . . . . Close
nc
This reduces possible engine damage or
flameout, or both, by decreasing EGT.
5 ENGINE START switches (both) . . . . . . . . . . FLT
U
6 PACK switches . . . . . . . . . . . . . . . . . . . . . HIGH
7 ENG ANTI–ICE switches (both). . . . . . . . . . . . ON
8 WING ANTI–ICE switch . . . . . . . . . . . . . . . . . ON
▼ Continued on next page ▼
7.46
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D6-27370-8AS-NOK
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7.47
737 Flight Crew Operations Manual
▼Volcanic Ash continued▼
9 APU switch
(if APU available) . . . . . . . . . . . . . . . . . . START
This supplies backup electrical and pneumatic
sources, if needed.
or
pr
in
te
d
Note: Volcanic ash can cause non-normal system
reactions such as:
ad
ed
•Engine malfunctions, increasing EGT,
engine stall or flameout
•Decrease in indicated airspeed or loss of
airspeed indications
•Equipment cooling OFF light.
do
w
nl
o
10 If failed, engines can accelerate to idle very slowly,
especially at high altitudes. If N2 is steadily
increasing and EGT stays within limits, the start is
progressing normally.
11 Plan to land at the nearest suitable airport.
if
12 Choose one:
on
tro
lle
d
Engines run normally:
■■■■
►►Go to the Loss Of Thrust On Both
Engines checklist on page 7.6
■■■■
U
nc
Engines do not run normally:
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 14, 2017
D6-27370-8AS-NOK
7.47
7.48
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7.48
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
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8 Fire Protection
NNC.8-Fire
Protection
(tab)
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Fire Protection
Section 8
or
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in
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d
Table of Contents
APU FIRE ......................................................8.1
Engine Fire on the Ground.................... ►►Back Cover.2
ENGINE FIRE or Engine Severe Damage or
Separation .................................................8.2
ENGINE OVERHEAT .......................................8.7
Engine Tailpipe Fire ......................................8.8
ad
ed
Smoke, Fire or Fumes ..................8.10
NNC. 13
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d
if
do
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APU BOTTLE DISCHARGED .............................. 8.14
APU DETECTION INOPERATIVE ........................ 8.14
APU FIRE ......................................................8.1
CARGO FIRE .................................................. 8.16
CARGO FIRE DETECTOR FAULT ........................ 8.19
DISCH .......................................................... 8.19
Engine Fire on the Ground.................... ►►Back Cover.2
ENGINE FIRE or Engine Severe Damage or
Separation .................................................8.2
ENGINE FIRE/OVERHEAT DETECTOR FAULT ....... 8.19
ENGINE OVERHEAT .......................................8.7
Engine Tailpipe Fire ......................................8.8
L/R BOTTLE DISCHARGED ............................... 8.20
Smoke or Fumes Removal ............................... 8.22
Smoke, Fire or Fumes ..................8.10
WHEEL WELL FIRE.......................................... 8.26
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
2
D6-27370-8AS-NOK
8.TOC.1
Non-Normal Checklists Fire Protection
737 Flight Crew Operations Manual
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Table of Contents
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Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
8.TOC.2
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March 31, 2023
8.1
737 Flight Crew Operations Manual
Fire Highlight
File
FIRE
APU
Protection
-WARN
Fire andand
FIRE
APU
WARN
- Fire
APU FIRE
Condition:
Fire is detected in the APU.
or
pr
in
te
d
1 APU fire switch . . . Confirm . . . .Pull, rotate to the
stop, and hold
for 1 second
2 APU switch . . . . . . . . . . . . . . . . . . . . . . . . OFF
----------------------3 Choose one:
APU fire switch extinguishes:
ad
ed
■■■■
APU fire switch stays illuminated:
do
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o
►►Go to step 4
4 Plan to land at the nearest suitable airport.
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on
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d
Engine Fire on the Ground ►►Back Cover.2
if
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 17, 2020
D6-27370-8AS-NOK
8.1
8.2
737 Flight Crew Operations Manual
FIRE WARN
Engine
1 - Fireand
2
andEngine
FIRE WARN
1 - Fire
2
ENGINE FIRE
or
Engine Severe Damage or
Separation
ENGINE FIRE or Engine Severe Damage or Separation
One or more of these occur:
•Engine fire warning
•Airframe vibrations with abnormal engine
indications
•Engine separation.
or
pr
in
te
d
Condition:
1 Autothrottle (if engaged) . . . . . . . . . . .Disengage
ad
ed
2 Thrust lever
(affected engine) . . . . . . Confirm . . . . . . . Close
do
w
nl
o
3 Engine start lever
(affected engine) . . . . . . Confirm . . . . . CUTOFF
4 Engine fire switch
(affected engine) . . . . . . Confirm . . . . . . . . Pull
d
if
To manually unlock the engine fire switch, press
the override and pull.
on
tro
lle
5 If the engine fire switch or ENG OVERHEAT light is
illuminated:
Engine fire switch
(affected engine) . . . . . . . . Rotate to the stop
and hold for 1 second
U
nc
----------------------▼ Continued on next page ▼
8.2
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D6-27370-8AS-NOK
March 18, 2021
8.3
737 Flight Crew Operations Manual
▼ENGINE FIRE or Engine Severe Damage or Separation continued▼
6 Choose one:
On the ground:
■■■■
In flight:
►►Go to step 7
or
pr
in
te
d
►►Go to the Engine Fire on the Ground
checklist on page Back Cover.2
ad
ed
7 If after 30 seconds the engine fire switch or ENG
OVERHEAT light stays illuminated:
do
w
nl
o
Engine fire switch
(affected engine) . . . . . . . . . . . . Rotate to the
other stop and
hold for 1 second
U
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on
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lle
d
if
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 2, 2021
D6-27370-8AS-NOK
8.3
8.4
737 Flight Crew Operations Manual
▼ENGINE FIRE or Engine Severe Damage or Separation continued▼
8 Choose one:
High airframe vibration occurs and continues
after the engine is shut down:
or
pr
in
te
d
Without delay, reduce airspeed and
descend to a safe altitude which results in
an acceptable vibration level.
►►Go to step 9
ad
ed
Note: If high vibration returns and further
airspeed reduction and descent are
not practical, increasing airspeed
can reduce the vibration.
do
w
nl
o
High airframe vibration does not occur or does
not continue after the engine is shut down:
►►Go to step 9
9 ISOLATION VALVE switch. . . . . . . . . . . . . CLOSE
d
if
10 PACK switch (affected side) . . . . . . . . . . . . . OFF
on
tro
lle
This step causes the operating pack to regulate
to high flow in flight with the flaps up.
11 APU BLEED air switch . . . . . . . . . . . . . . . . . OFF
U
nc
▼ Continued on next page ▼
8.4
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 18, 2021
8.5
737 Flight Crew Operations Manual
▼ENGINE FIRE or Engine Severe Damage or Separation continued▼
12 Choose one:
APU is available for start:
When APU is running:
or
pr
in
te
d
APU . . . . . . . . . . . . . . . . . . . . . . START
APU GEN switch
(affected side) . . . . . . . . . . . . . ON
APU is not available:
ad
ed
►►Go to step 13
►►Go to step 13
do
w
nl
o
13 Balance fuel as needed.
YK820, YL061, YR591 - YS823
14 Transponder mode selector . . . . . . . . . . . . . . TA
d
if
This prevents climb commands which can
exceed single engine performance capability.
on
tro
lle
YR323, YR339, YV081 - YW351
15 Transponder mode selector . . . . . . . . . . TA ONLY
This prevents climb commands which can
exceed single engine performance capability.
U
nc
16 ISOLATION VALVE switch
(after the fire has been extinguished) . . . . . AUTO
This step ensures bleed air is available to both
wings if wing anti-ice is needed.
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
8.5
8.6
737 Flight Crew Operations Manual
▼ENGINE FIRE or Engine Severe Damage or Separation continued▼
17 Plan to land at the nearest suitable airport.
Note: Do not use FMC performance predictions.
YK820, YL061, YR339 - YW351
■■■■
YR323
or
pr
in
te
d
►►Go to the One Engine Inoperative
Landing checklist on page 7.34
►►Go to the One Engine Inoperative
Landing checklist on page 7.38
U
nc
on
tro
lle
d
if
do
w
nl
o
ad
ed
■■■■
8.6
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
8.7
737 Flight Crew Operations Manual
ENG 2
1 OVERHEAT
ENGINE OVERHEAT
ENG 1
OVERHEAT
Condition:
ENG 2
OVERHEAT
An overheat is detected in the engine.
or
pr
in
te
d
1 Autothrottle (if engaged). . . . . . . . . . .Disengage
2 Thrust lever
(affected engine) . . . . . . Confirm . . . . . . . Close
3 If the ENG OVERHEAT light stays illuminated:
ad
ed
►►Go to the ENGINE FIRE or Engine
Severe Damage or Separation checklist
on page 8.2
do
w
nl
o
■■■■
----------------------4 If the ENG OVERHEAT light extinguishes:
d
if
Run the engine at reduced thrust to keep the
light extinguished.
on
tro
lle
Note: Do not use FMC performance predictions.
This step prevents climb commands which can
exceed reduced thrust performance capability.
U
nc
YK820, YL061, YR591 - YS823
5 Transponder mode selector . . . . . . . . . . . . . . TA
YR323, YR339, YV081 - YW351
6 Transponder mode selector . . . . . . . . . . TA ONLY
This step prevents climb commands which can
exceed reduced thrust performance capability.
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
8.7
8.8
737 Flight Crew Operations Manual
Engine Tailpipe Fire
Condition:
An engine tailpipe fire occurs on the ground
with no engine fire warning.
or
pr
in
te
d
1 Engine start lever
(affected engine) . . . . . . . . . . . . . . . . . CUTOFF
2 Advise the cabin.
3 Choose one:
Bleed air is available:
ad
ed
►►Go to step 4
Bleed air is not available:
■■■■
do
w
nl
o
Advise ATC.
4 PACK switches (both) . . . . . . . . . . . . . . . . . OFF
if
5 ISOLATION VALVE switch. . . . . . . . . . . . . . AUTO
d
6 Engine BLEED air switches (both) . . . . . . . . . . ON
on
tro
lle
7 Choose one:
APU is running:
U
nc
APU BLEED air switch . . . . . . . . . . . . . ON
►►Go to step 8
APU is not running:
►►Go to step 8
▼ Continued on next page ▼
8.8
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 18, 2021
8.9
737 Flight Crew Operations Manual
▼Engine Tailpipe Fire continued▼
8 Choose one:
Affected ENGINE START switch is in GRD:
►►Go to step 9
or
pr
in
te
d
Affected ENGINE START switch is not in GRD:
Allow the affected N2 to decrease below
20%.
ENGINE START switch
(affected engine) . . . . . . . . . . . . . . . GRD
ad
ed
►►Go to step 9
do
w
nl
o
9 Advise ATC.
10 When the tailpipe fire is extinguished:
■■■■
U
nc
on
tro
lle
d
if
ENGINE START switch
(affected engine) . . . . . . . . . . . . . . . . . . OFF
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 18, 2021
D6-27370-8AS-NOK
8.9
8.10
737 Flight Crew Operations Manual
Smoke, Fire or Fumes
Condition:
Smoke, fire or fumes occur.
1 Diversion may be needed.
3 Don smoke goggles, as needed.
or
pr
in
te
d
2 Don oxygen masks and set regulators to 100%, as
needed.
4 Establish crew and cabin communications.
5 BUS TRANSFER switch . . . . . . . . . . . . . . . . OFF
do
w
nl
o
ad
ed
YR323 - YW351
6 Advise the cabin crew that the cabin lighting will be
extinguished, but passenger reading lights will
continue to work.
7 CAB/UTIL switch. . . . . . . . . . . . . . . . . . . . . OFF
8 IFE/PASS SEAT switch . . . . . . . . . . . . . . . . . OFF
if
9 RECIRC FAN switches (both) . . . . . . . . . . . . OFF
d
10 APU BLEED air switch . . . . . . . . . . . . . . . . . OFF
on
tro
lle
11 Anytime the smoke or fumes become the greatest
threat:
U
nc
►►Go to the Smoke or Fumes Removal
checklist on page 8.22
8.10
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
September 30, 2022
8.11
737 Flight Crew Operations Manual
▼Smoke, Fire or Fumes continued▼
12 Choose one:
Source of the smoke, fire or fumes is obvious
and can be extinguished quickly:
or
pr
in
te
d
Isolate and extinguish the source.
If possible, remove power from the affected
equipment by switch or circuit breaker in
the flight deck or cabin.
►►Go to step 13
ad
ed
Source of the smoke, fire or fumes is not obvious
or cannot be extinguished quickly:
13 Choose one:
do
w
nl
o
►►Go to step 14
Source is visually confirmed to be extinguished
and the smoke or fumes are decreasing:
on
tro
lle
d
if
Continue the flight at the captain’s
discretion.
U
nc
Restore unpowered items at the captain’s
discretion.
►►Go to the Smoke or Fumes Removal
checklist on page 8.22, if needed
■■■■
Source is not visually confirmed to be
extinguished or smoke or fumes are not
decreasing:
►►Go to step 14
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
8.11
8.12
737 Flight Crew Operations Manual
▼Smoke, Fire or Fumes continued▼
14 EQUIP COOLING SUPPLY
and EXHAUST switches (both) . . . . . . . . . . ALTN
15 Instruct the cabin crew to:
or
pr
in
te
d
Turn on cabin reading lights.
Turn on galley attendants work lights.
YK820, YL061
Turn off cabin fluorescent light switches.
ad
ed
16 Divert to the nearest suitable airport while
continuing the checklist.
do
w
nl
o
17 Consider an immediate landing if the smoke, fire or
fumes situation becomes uncontrollable.
18 Do not delay landing in an attempt to complete all
of the following steps.
19 ISOLATION VALVE switch. . . . . . . . . . . . . CLOSE
if
20 R PACK switch . . . . . . . . . . . . . . . . . . . . . . OFF
on
tro
lle
d
21 Wait 2 minutes unless the smoke or fumes are
increasing. This allows time for the smoke or fumes
to clear.
U
nc
▼ Continued on next page ▼
8.12
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
September 30, 2022
8.13
737 Flight Crew Operations Manual
▼Smoke, Fire or Fumes continued▼
22 Choose one:
Smoke or fumes are decreasing:
■■■■
or
pr
in
te
d
►►Go to the Smoke or Fumes Removal
checklist on page 8.22, if needed
Smoke or fumes continue or are increasing:
R PACK switch . . . . . . . . . . . . . . . . AUTO
ad
ed
L PACK switch . . . . . . . . . . . . . . . . . OFF
►►Go to step 23
24 Choose one:
do
w
nl
o
23 Wait 2 minutes unless the smoke or fumes are
increasing. This allows time for the smoke or fumes
to clear.
if
Smoke or fumes are decreasing:
on
tro
lle
d
►►Go to the Smoke or Fumes Removal
checklist on page 8.22, if needed
■■■■
U
nc
Smoke or fumes continue or are increasing:
L PACK switch . . . . . . . . . . . . . . . . AUTO
Consider an immediate landing.
►►Go to the Smoke or Fumes Removal
checklist on page 8.22, if needed
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
8.13
8.14
737 Flight Crew Operations Manual
APU BOTTLE DISCHARGED
APU BOTTLE
DISCHARGED
APU BOTTLE
DISCHARGED
The APU fire extinguisher bottle has
discharged or pressure is low.
■■■■
APU DET INOP
APU DETECTION
INOPERATIVE
APU DET
INOP
Condition:
or
pr
in
te
d
Condition:
APU fire detection is inoperative.
ad
ed
1 APU switch. . . . . . . . . . . . . . . . . . . . . . . . . OFF
do
w
nl
o
Caution! Do not run the APU. An APU fire would
not be detected and the APU would
continue to run.
U
nc
on
tro
lle
d
if
■■■■
8.14
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
September 30, 2022
8.15
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737 Flight Crew Operations Manual
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if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 19, 2020
D6-27370-8AS-NOK
8.15
8.16
737 Flight Crew Operations Manual
FIRE-WARN
FWD
AFT
-Cargo
CargoFire
and
Fireand
FWD
AFT
andFIRE
FIRE
--Cargo
Cargo
WARN
WARN
Fire
Fire
CARGO FIRE
FWD
AFT
Fire is detected in the related cargo
compartment.
Objective:
To suppress the cargo fire.
or
pr
in
te
d
Condition:
1 CARGO FIRE ARM switch
(affected compartment) . . . Confirm . . . . . Push,
Verify ARMED
ad
ed
2 CARGO FIRE DISCH switch . . . . . . Push and hold
for 1 second
do
w
nl
o
Note: DISCH light may need up to 30 seconds to
illuminate.
on
tro
lle
d
if
Note: Halon or residual smoke can cause flight deck
cargo fire indications to remain or occur
again. More information is found in the
Additional Information section.
U
nc
▼ Continued on next page ▼
8.16
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 19, 2020
8.17
737 Flight Crew Operations Manual
▼CARGO FIRE continued▼
3 Choose one:
On the ground:
ad
ed
■■■■
or
pr
in
te
d
Warning! Inform ground personnel
NOT to open any cargo door
until all passengers and crew
have exited the airplane and
fire fighting equipment is
nearby.
In flight:
do
w
nl
o
►►Go to step 4
4 RECIRC FAN switches (both) . . . . . . . . . . . . OFF
5 PACK switches (both) . . . . . . . . . . . . . . . . HIGH
on
tro
lle
d
if
YL061
6 CAB/UTIL switch . . . . . . . . . . . . . . . . . . . . OFF
This prevents galley chiller exhaust from
carrying smoke or fumes into the cabin.
7 Plan to land at the nearest suitable airport.
U
nc
8 Checklist Complete Except Deferred Items
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 19, 2020
D6-27370-8AS-NOK
8.17
8.18
737 Flight Crew Operations Manual
▼CARGO FIRE continued▼
Deferred Items
Descent Checklist
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
or
pr
in
te
d
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing data . . . . . . . . . VREF ___, Minimums ___
Approach briefing . . . . . . . . . . . . . . . . Completed
ad
ed
Approach Checklist
do
w
nl
o
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
on
tro
lle
d
if
Warning! Inform ground personnel NOT to open
any cargo door after landing until all
passengers and crew have exited the
airplane and fire fighting equipment is
nearby.
Landing Checklist
ENGINE START switches. . . . . . . . . . . . . . . . CONT
nc
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
U
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps . . . . . . . . . . . . . . . . . . . . . ___, Green light
■■■■
▼ Continued on next page ▼
8.18
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 19, 2020
8.19
737 Flight Crew Operations Manual
▼CARGO FIRE continued▼
Additional Information
or
pr
in
te
d
The red FWD/AFT cargo fire warning light(s) can
extinguish, remain illuminated, or re-illuminate over
the remainder of the flight. If the FWD/AFT cargo fire
warning light(s) re-illuminate, both master FIRE
WARN lights also re-illuminate and the fire warning
bell sounds. These flight deck indications alone of a
cargo fire within the same compartment do not
indicate the fire is uncontrolled.
ad
ed
Illumination of the cargo fire DISCH light indicates
the fire suppression system has been fully activated.
DETECTOR FAULT
Fire detection is inoperative in one or both
cargo compartments.
DISCH
Cargo Fire Bottle Discharged
on
tro
lle
DISCH
d
if
Condition:
CARGO FIRE DETECTOR FAULT
do
w
nl
o
DETECTOR
FAULT
DISCH
A cargo fire extinguisher bottle has
discharged or pressure is low.
U
nc
Condition:
■■■■
■■■■
FAULT - Engine Fire/Overheat Detector
ENGINE FIRE/OVERHEAT
DETECTOR FAULT
FAULT
Condition:
Engine fire and overheat detection is
inoperative in one or both engines.
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
8.19
8.20
737 Flight Crew Operations Manual
L BOTTLE
R
Engine
Fire DISCHARGED
Bottle Discharged L/R
L/R BOTTLE DISCHARGED
L BOTTLE
R BOTTLE
DISCHARGED DISCHARGED
The engine fire extinguisher bottle has
discharged or pressure is low.
U
nc
on
tro
lle
d
if
do
w
nl
o
ad
ed
■■■■
or
pr
in
te
d
Condition:
8.20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
September 30, 2022
8.21
do
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in
te
d
737 Flight Crew Operations Manual
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on
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d
if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
8.21
8.22
737 Flight Crew Operations Manual
Smoke or Fumes Removal
Condition:
Smoke or fumes removal is needed.
1 Do this checklist only when directed by the Smoke,
Fire or Fumes checklist.
3 Close the flight deck door.
4 Choose one:
►►Go to step 5
ad
ed
Both PACK switches are OFF:
or
pr
in
te
d
2 Do not delay landing in an attempt to complete the
following steps.
do
w
nl
o
A single or both PACK switch(es) are in AUTO:
►►Go to step 6
U
nc
on
tro
lle
d
if
▼ Continued on next page ▼
8.22
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
September 30, 2022
8.23
737 Flight Crew Operations Manual
▼Smoke or Fumes Removal continued▼
5 Choose one:
Smoke or fumes source is confirmed to be
outside the flight deck:
or
pr
in
te
d
■■■■
Smoke or fumes source is confirmed to be on the
flight deck:
ad
ed
Caution! Window should not be
opened unless the source is
confirmed to be on the flight
deck.
do
w
nl
o
Establish normal holding speed. High
airspeed may prevent opening the window.
Open the first officer’s sliding window.
on
tro
lle
d
if
►►Go to the Smoke, Fire or Fumes
checklist on page 8.10 and do the
remaining steps
nc
6
■■■■
Do not turn on any PACK switch that was turned
off by the Smoke, Fire or Fumes checklist.
Operating PACK switch(es) . . . . . . . . . . . HIGH
U
7 LAND ALT indicator . . . . . . . . . . . . . . 10000 feet
Note: The intermittent cabin altitude/configuration
warning horn will sound and the CABIN
ALTITUDE lights (if installed and operative)
will illuminate at a cabin altitude of
approximately 10,000 feet.
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
8.23
8.24
737 Flight Crew Operations Manual
▼Smoke or Fumes Removal continued▼
8 Engine BLEED air switches (both) . . . . . Verify ON
9 Set thrust to maximum practical N1 (minimum
45%).
or
pr
in
te
d
10 Open flight deck air conditioning and
gasper outlets.
Caution! Do not open any flight deck window.
Keep the flight deck door closed.
11 Choose one:
ad
ed
Smoke or fumes are controllable:
do
w
nl
o
►►Go to the Smoke, Fire or Fumes
checklist on page 8.10 and do the
remaining steps
■■■■
if
Smoke or fumes are uncontrollable:
on
tro
lle
d
►►Go to step 12
12 Descend to the lowest safe altitude or 10,000 feet,
whichever is higher.
U
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▼ Continued on next page ▼
8.24
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
8.25
737 Flight Crew Operations Manual
▼Smoke or Fumes Removal continued▼
13 When at 14,000 feet or below:
Pressurization mode selector . . . . . . . . . . MAN
or
pr
in
te
d
Outflow VALVE switch . . . . . . . . . Hold in OPEN
until the outflow VALVE
indication shows fully OPEN
This causes the cabin airflow to carry
smoke or fumes aft.
Note: The outflow valve can take up to 20
seconds to open.
ad
ed
►►Go to the Smoke, Fire or Fumes
checklist on page 8.10 and do the
remaining steps
U
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on
tro
lle
d
if
do
w
nl
o
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
8.25
8.26
737 Flight Crew Operations Manual
WHEEL
FIRE
WARN
WELL
and- Fire
WHEEL
and FIRE
WELL
WARN
- Fire
WHEEL
WELL
Condition:
WHEEL WELL FIRE
Fire is detected in the main wheel well.
270K/.82M maximum.
1
or
pr
in
te
d
LANDING GEAR lever . . . . . . . . . . . . . . . . . DN
This attempts to remove and extinguish the fire
source.
2 Plan to land at the nearest suitable airport.
ad
ed
Note: Do not use FMC performance predictions
with gear extended.
3 Choose one:
do
w
nl
o
Gear must be retracted for airplane
performance:
►►Go to step 4
■■■■
on
tro
lle
d
if
Gear does not need to be retracted for airplane
performance:
4 When the WHEEL WELL light extinguishes:
U
nc
Wait 20 minutes.
5
235K maximum.
LANDING GEAR lever . . . . . . . . . . . . . . . . . UP
After landing gear retraction is complete:
LANDING GEAR lever . . . . . . . . . . . OFF
■■■■
8.26
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
September 30, 2022
9 Flight Controls
NNC.9-Flight
Controls
(tab)
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Flight Controls
Section 9
Table of Contents
Runaway Stabilizer .......................................9.1
NNC. 3
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All Flaps Up Landing .........................................9.4
AUTO SLAT FAIL ..............................................9.6
Elevator Tab Vibration ......................................9.6
FEEL DIFFERENTIAL PRESSURE ..........................9.7
FLAP LOAD RELIEF ...........................................9.7
FLIGHT CONTROL LOW PRESSURE......................9.8
Jammed or Restricted Flight Controls ..................9.8
LEADING EDGE FLAPS TRANSIT ....................... 9.12
MACH TRIM FAIL ............................................ 9.16
Runaway Stabilizer .......................................9.1
SPEED BRAKE DO NOT ARM............................. 9.16
SPEED TRIM FAIL ...........................................9.17
SPEEDBRAKES EXTENDED ............................... 9.18
STABILIZER OUT OF TRIM ............................... 9.20
Stabilizer Trim Inoperative .............................. 9.22
STANDBY RUDDER ON .................................... 9.26
Trailing Edge Flap Asymmetry ..........................9.27
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Trailing Edge Flap Disagree ............................. 9.32
Trailing Edge Flaps Up Landing......................... 9.40
YAW DAMPER ................................................ 9.44
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9.TOC.1
Non-Normal Checklists Flight Controls
737 Flight Crew Operations Manual
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Table of Contents
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9.TOC.2
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9.1
737 Flight Crew Operations Manual
Flight
File
Highlight
Controls
Runaway Stabilizer
Condition:
Uncommanded stabilizer trim movement
occurs continuously or in a manner not
appropriate for flight conditions.
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1 Control column. . . . . . . . . . . . . . . . . Hold firmly
2 Autopilot (if engaged) . . . . . . . . . . . . .Disengage
3 Autothrottle (if engaged). . . . . . . . . . .Disengage
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4 Control column and
thrust levers . . . . . . . . . . . Control airplane pitch
attitude and airspeed
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5 Main Electric
Stabilizer trim . . . . . . . . . . . . . . .Reduce control
column forces
6 If the runaway stops after the autopilot is
disengaged:
■■■■
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Do not re-engage the autopilot or autothrottle.
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7 If the runaway continues after the autopilot is
disengaged:
STAB TRIM cutout
switches (both) . . . . . . . . . . . . . . . . CUTOUT
If the runaway continues:
Stabilizer
trim wheel . . . . . . . . . . Grasp and hold
----------------------▼ Continued on next page ▼
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9.1
9.2
737 Flight Crew Operations Manual
▼Runaway Stabilizer continued▼
8 Stabilizer . . . . . . . . . . . . . . . . . . . Trim manually
A two-pilot effort may be used to correct an out
of trim condition.
9 Anticipate trim requirements.
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Note: Reducing airspeed reduces airloads on the
stabilizer which can reduce the effort needed
to manually trim.
10 Do not re-engage the autopilot or autothrottle.
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11 Checklist Complete Except Deferred Items
Deferred Items
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Descent Checklist
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
if
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
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Landing data . . . . . . . . . VREF ___, Minimums ___
Approach briefing . . . . . . . . . . . . . . . . Completed
Approach Checklist
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Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing Configuration and Trim
Establish landing configuration and in-trim condition
early on final approach.
▼ Continued on next page ▼
9.2
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9.3
737 Flight Crew Operations Manual
▼Runaway Stabilizer continued▼
Landing Checklist
ENGINE START switches . . . . . . . . . . . . . . . CONT
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Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps . . . . . . . . . . . . . . . . . . . . . ___, Green light
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9.3
9.4
737 Flight Crew Operations Manual
All Flaps Up Landing
The leading edge devices fail to extend and
trailing edge flaps are less than 1.
Objective:
To configure for a landing with leading edge
devices retracted and trailing edge flaps
less than 1.
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Condition:
1 Do this checklist only when directed by the Trailing
Edge Flaps Up Landing checklist.
3 Set VREF 40 + 55 knots.
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2 Consider burning off fuel to reduce touchdown
speed.
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4 Check the Non–Normal Configuration Landing
Distance tables in the Performance Inflight-QRH
chapter or other approved source.
if
5 Maintain flaps up maneuvering speed until
established on final approach.
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6 Limit bank angle to 15° when airspeed is less than
the flaps up maneuvering speed.
7 Checklist Complete Except Deferred Items
Deferred Items
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Descent Checklist
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Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing data . . . . . . . . VREF 40 + 55 knots ___,
Minimums ___
▼ Continued on next page ▼
9.4
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9.5
737 Flight Crew Operations Manual
▼All Flaps Up Landing continued▼
Approach briefing . . . . . . . . . . . . . . . . Completed
Go-Around Procedure Review
or
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Do the normal go-around procedure except:
Limit bank angle to 15° when the airspeed is
less than the flaps up maneuvering speed.
Approach Checklist
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Accelerate to flaps up maneuvering speed.
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Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Additional Deferred Items
FASTEN BELTS switch . . . . . . . . . . . . . . . . . . . ON
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GROUND PROXIMITY
FLAP INHIBIT switch . . . . . . . . . . . . FLAP INHIBIT
Landing Checklist
ENGINE START switches . . . . . . . . . . . . . . . CONT
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Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
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YL061 - YW351
Note: The SPEED BRAKE lever will not move
beyond the FLIGHT DETENT on landing and
the spoilers will not fully deploy.
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps. . . . . . . . . . . . . . . . . . . . . . .___, No lights
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9.5
9.6
737 Flight Crew Operations Manual
AUTO SLAT FAIL
AUTO SLAT
FAIL
Condition:
AUTO SLAT FAIL
The auto slat system is failed.
1 Continue normal operation.
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Elevator Tab Vibration
An elevator tab vibration occurs in flight.
One or more of the following may be an
indication of an elevator tab vibration:
•Vibration that originates, and is strongest,
in the aft part of the airplane but can be
felt throughout the airplane
•Vibration that is felt in the control wheel
and rudder pedals
•Vibration that causes items attached to
the airplane, such as sun visors, to move.
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Condition:
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1 Passenger signs . . . . . . . . . . . . . . . . . . . . . . ON
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Do not use speedbrakes or change aircraft
configuration to reduce airspeed. Do not reduce
airspeed below the minimum speed for the
existing flap setting and gross weight.
Smoothly reduce airspeed until the vibration
2
stops.
3 Consider landing at the nearest suitable airport.
4 Stay at or below the reduced airspeed at which the
vibration stopped for the rest of the flight. Limit
bank angle to 15° until below 20,000 feet.
5 Do not deploy speedbrakes in flight.
▼ Continued on next page ▼
9.6
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9.7
737 Flight Crew Operations Manual
▼Elevator Tab Vibration continued▼
Note: Flaps and landing gear can be extended
normally for the approach.
■■■■
FEEL DIFF PRESS
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The speedbrakes can be armed for landing.
FEEL DIFFERENTIAL
PRESSURE
FEEL
DIFF PRESS
High differential pressure is measured by the
elevator feel computer.
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Condition:
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Note: Column forces can be significantly higher
than normal, particularly during landing
flare.
The autopilot can disengage when pitch
changes are commanded.
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Do not attempt an autoland.
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1 Continue normal operation.
■■■■
FLAP LOAD RELIEF
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FLAP LOAD
RELIEF
Condition:
FLAP LOAD RELIEF
YL061 - YR339
Flap load relief occurs.
1 Check flap position and maintain the appropriate
airspeed.
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9.7
9.8
737 Flight Crew Operations Manual
LOW PRESSURE - Flight Control
LOW
PRESSURE
FLIGHT CONTROL LOW
PRESSURE
Hydraulic system pressure to the ailerons,
elevators and rudder is low.
Objective:
To activate the standby hydraulic system
and standby rudder PCU.
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Condition:
1 FLT CONTROL switch
(affected side) . . . . . . Confirm. . . . . .STBY RUD
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Jammed or Restricted
Flight Controls
A flight control is jammed or restricted in
roll, pitch, or yaw.
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Condition:
1 Autopilot (if engaged) . . . . . . . . . . . . .Disengage
if
2 Autothrottle (if engaged) . . . . . . . . . . .Disengage
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3 Verify that the thrust is symmetrical.
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4 Overpower the jammed or restricted system. Use
maximum force, including a combined effort of
both pilots, if needed. A maximum two-pilot effort
on the controls will not cause a cable or system
failure.
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5 Do not turn off any flight control switches.
▼ Continued on next page ▼
9.8
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9.9
737 Flight Crew Operations Manual
▼Jammed or Restricted Flight Controls continued▼
6 Choose one:
The failure could be due to freezing water and
conditions allow:
►►Go to step 7
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Consider a descent to a warmer
temperature and attempt to overpower the
jammed or restricted system again.
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The failure could not be due to freezing water or
conditions do not allow:
7 Choose one:
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►►Go to step 7
Controls are normal:
■■■■
if
Controls are not normal:
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►►Go to step 8
8 Use stabilizer or rudder trim to offload control
forces. If electric stabilizer trim is needed, move
the Stabilizer Trim Override switch to OVERRIDE.
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9 Do not make abrupt thrust changes. Extend or
retract speedbrake slowly and smoothly.
10 Limit bank angle to 15°.
11 Plan to land at the nearest suitable airport.
12 Plan a flaps 15 landing.
▼ Continued on next page ▼
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9.9
9.10
737 Flight Crew Operations Manual
▼Jammed or Restricted Flight Controls continued▼
13 Set VREF 15 or VREF ICE.
Note: If any of the following conditions apply,
set VREF ICE = VREF 15 + 10 knots:
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•Engine anti–ice will be used during
landing
•Wing anti–ice has been used any
time during the flight
•Icing conditions were encountered
during the flight and the landing
temperature is below 10° C.
Note: When VREF ICE is needed, the wind
additive should not exceed 5 knots.
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14 Check the Non–Normal Configuration Landing
Distance tables in the Performance Inflight-QRH
chapter or other approved source.
if
15 Checklist Complete Except Deferred Items
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Deferred Items
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Descent Checklist
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
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Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
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Landing data . . . . . . . VREF 15 or VREF ICE ___,
Minimums ___
Approach briefing . . . . . . . . . . . . . . . . Completed
▼ Continued on next page ▼
9.10
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9.11
737 Flight Crew Operations Manual
▼Jammed or Restricted Flight Controls continued▼
Go-Around Procedure Review
Do the normal go-around procedure.
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Advance thrust to go-around smoothly and slowly to
avoid excessive pitch-up.
Approach Checklist
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Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Additional Deferred Item
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GROUND PROXIMITY
FLAP INHIBIT switch . . . . . . . . . . . . FLAP INHIBIT
Landing Checklist
if
ENGINE START switches . . . . . . . . . . . . . . . CONT
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Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps. . . . . . . . . . . . . . . . . . . . . . 15, Green light
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9.11
9.12
737 Flight Crew Operations Manual
LE FLAPS TRANSIT
LEADING EDGE FLAPS
TRANSIT
LE FLAPS
TRANSIT
One or more of these occur:
•The leading edge devices are not in the
commanded position
•A leading edge device asymmetry is
detected
•A leading edge device skew is detected.
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Condition:
Note: Do not use FMC performance predictions
with any flaps or slats extended.
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1 Choose one:
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Trailing edge flaps are extended and the
trailing edge flap position indication disagrees
with the flap handle position:
►►Go to the Trailing Edge Flap
Disagree checklist on page 9.32
if
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Trailing edge flaps are extended and the
trailing edge flap position indication agrees with
the flap handle position:
►►Go to step 7
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Trailing edge flaps are up:
Limit airspeed to 230 knots maximum.
►►Go to step 2
▼ Continued on next page ▼
9.12
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9.13
737 Flight Crew Operations Manual
▼LEADING EDGE FLAPS TRANSIT continued▼
2 Choose one:
Roll is encountered:
Roll is not encountered:
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►►Go to step 7
Note: Roll may be difficult to identify with
the autopilot engaged.
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►►Go to step 3
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Maximum flap extension altitude 20,000 feet.
Flaps . . . . . . . . . . . . . . . . . .Extend to flaps 1,
3
then retract to flaps up
4 Choose one:
LE FLAPS TRANSIT light extinguishes after the
flaps are up:
■■■■
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Continue normal operation.
LE FLAPS TRANSIT light stays illuminated after
the flaps are up:
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►►Go to step 5
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5 Check LE DEVICES annunciator panel.
▼ Continued on next page ▼
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9.13
9.14
737 Flight Crew Operations Manual
▼LEADING EDGE FLAPS TRANSIT continued▼
6 Choose one:
Light(s) for only one leading edge device is
illuminated:
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Limit airspeed to 300 knots (280 knots for
turbulent air penetration) or 0.65 Mach,
whichever is lower.
►►Go to step 7
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Light(s) for more than one leading edge device
is illuminated:
Limit airspeed to 230 knots maximum.
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►►Go to step 7
7 Plan a flaps 15 landing.
8 Set VREF 15 + 15 knots.
d
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9 Limit bank angle to 15° when airspeed is less than
the flaps up maneuvering speed.
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Distance tables in the Performance Inflight-QRH
chapter or other approved source.
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11 Checklist Complete Except Deferred Items
Deferred Items
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Descent Checklist
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
▼ Continued on next page ▼
9.14
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9.15
737 Flight Crew Operations Manual
▼LEADING EDGE FLAPS TRANSIT continued▼
Landing data . . . . . . . . VREF 15 + 15 knots ___,
Minimums ___
Approach Checklist
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Approach briefing . . . . . . . . . . . . . . . . Completed
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Additional Deferred Item
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GROUND PROXIMITY
FLAP INHIBIT switch . . . . . . . . . . . . FLAP INHIBIT
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Note: The amber LE FLAPS TRANSIT light may be
illuminated. Operation within the lower
amber airspeed band for landing is normal
for this condition.
if
Landing Checklist
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ENGINE START switches . . . . . . . . . . . . . . . CONT
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps. . . . . . . . . . . . . . 15, Green or amber light
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Note: The light may be green or amber depending
on the cause of the failure.
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9.15
9.16
737 Flight Crew Operations Manual
MACH TRIM FAIL
MACH TRIM
FAIL
MACH TRIM FAIL
The mach trim system is failed.
Condition:
1 Limit airspeed to 280 knots/0.82 Mach.
or
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■■■■
SPEED BRAKE DO NOT ARM - Without Load Alleviation System
SPEED BRAKE
DO NOT ARM
Condition:
SPEED BRAKE DO NOT ARM
An automatic speedbrake fault occurs.
Note: Speedbrakes may be used in flight.
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1 Do not arm the speedbrake for landing. Manually
deploy the speedbrakes immediately upon landing.
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2 Checklist Complete Except Deferred Items
Deferred Items
Descent Checklist
if
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
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Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing data . . . . . . . . . VREF ___, Minimums ___
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Approach briefing . . . . . . . . . . . . . . . . Completed
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Approach Checklist
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
▼ Continued on next page ▼
9.16
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9.17
737 Flight Crew Operations Manual
▼SPEED BRAKE DO NOT ARM continued▼
Landing Checklist
ENGINE START switches . . . . . . . . . . . . . . . CONT
or
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Speedbrake . . . . . . . . . . . . . . . . . . DOWN detent
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps . . . . . . . . . . . . . . . . . . . . . ___, Green light
■■■■
SPEED TRIM FAIL
SPEED TRIM
FAIL
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Condition:
SPEED TRIM FAIL
Speed Trim function is inoperative.
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Note: The Speed Trim System will not provide
stabilizer trim inputs when deviating from a
trimmed airspeed.
■■■■
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1 Continue normal operation.
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9.17
9.18
737 Flight Crew Operations Manual
SPEEDBRAKES EXTENDED
SPEEDBRAKES
EXTENDED
In flight, the speedbrakes are extended
beyond the ARMED position and one or more
of these occur:
•The radio altitude is below 800 feet
•The flap lever setting is more than
flaps 10.
or
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Condition:
SPEEDBRAKES EXTENDED
On the ground, the SPEED BRAKE lever is
down and the speedbrakes are extended.
1 Choose one:
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In flight:
SPEED BRAKE lever . . . . . . . . . . . ARMED
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■■■■
On the ground:
SPEED BRAKE lever . . . . . . DOWN detent
■■■■
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Note: If the light stays illuminated, do not
takeoff.
9.18
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9.19
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737 Flight Crew Operations Manual
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Intentionally
Blank
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9.19
9.20
737 Flight Crew Operations Manual
STAB OUT OF TRIM
STABILIZER OUT OF TRIM
STAB
OUT OF
TRIM
The autopilot does not set the stabilizer trim
correctly.
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Condition:
Note: During large changes in trim requirements,
the STAB OUT OF TRIM light can illuminate
momentarily.
Stabilizer is trimming:
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1 Choose one:
Continue normal operation.
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■■■■
Stabilizer is not trimming:
if
►►Go to step 2
d
2 Control column. . . . . . . . . . . . . . . . . Hold firmly
on
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3 Autopilot . . . . . . . . . . . . . . . . . . . . . .Disengage
4 Autothrottle (if engaged) . . . . . . . . . . .Disengage
▼ Continued on next page ▼
U
nc
5 Main Electric
Stabilizer trim . . . . . . . . . . . . . . . . . .As needed
9.20
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March 31, 2023
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737 Flight Crew Operations Manual
▼STABILIZER OUT OF TRIM continued▼
6 Choose one:
Stabilizer responds to electric trim inputs:
■■■■
or
pr
in
te
d
Do not re-engage the autopilot or
autothrottle.
Stabilizer does not respond to electric trim
inputs:
ad
ed
►►Go to the Stabilizer Trim
Inoperative checklist on page 9.22
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if
do
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Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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D6-27370-8AS-NOK
9.21
9.22
737 Flight Crew Operations Manual
Stabilizer Trim Inoperative
Loss of electric trim through the main
electric stabilizer trim switches, or as
directed by the STAB OUT OF TRIM checklist.
Objective:
To land the airplane using manual trim or, if
manual trim is not available, to land the airplane using elevator control only.
or
pr
in
te
d
Condition:
1 Autothrottle (if engaged) . . . . . . . . . . .Disengage
ad
ed
Do not re-engage the autothrottle.
2 STAB TRIM cutout switches (both) . . . . . CUTOUT
The autopilot is not available.
do
w
nl
o
3 Stabilizer . . . . . . . . . . . . . . . . . . . Trim manually
A two-pilot effort may be used and will not cause
system damage.
on
tro
lle
d
if
Note: Reducing airspeed reduces airloads on the
stabilizer which can reduce the effort needed
to manually trim.
U
nc
If the failure could be due to ice
accumulation, descend to a warmer
temperature and attempt again to trim
manually.
9.22
▼ Continued on next page ▼
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D6-27370-8AS-NOK
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9.23
737 Flight Crew Operations Manual
▼Stabilizer Trim Inoperative continued▼
4 Choose one:
Stabilizer can be trimmed manually:
►►Go to step 5
►►Go to step 6
5 Anticipate trim requirements.
ad
ed
►►Go to step 8
or
pr
in
te
d
Stabilizer cannot be trimmed manually:
6 Expect higher than normal elevator forces during
approach and landing.
do
w
nl
o
7 The thrust reduction at flare will cause a nose down
pitch.
8 Plan a flaps 15 landing.
9 Set VREF 15 or VREF ICE.
on
tro
lle
d
if
Note: If any of the following conditions apply,
set VREF ICE = VREF 15 + 10 knots:
U
nc
•Engine anti–ice will be used during
landing
•Wing anti–ice has been used any
time during the flight
•Icing conditions were encountered
during the flight and the landing
temperature is below 10° C.
Note: When VREF ICE is needed, the wind
additive should not exceed 5 knots.
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
9.23
9.24
737 Flight Crew Operations Manual
▼Stabilizer Trim Inoperative continued▼
10 Check the Non–Normal Configuration Landing
Distance tables in the Performance Inflight-QRH
chapter or other approved source.
Deferred Items
Descent Checklist
or
pr
in
te
d
11 Checklist Complete Except Deferred Items
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
ad
ed
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
do
w
nl
o
Landing data . . . . . . . VREF 15 or VREF ICE ___,
Minimums ___
Approach briefing . . . . . . . . . . . . . . . . Completed
Go-Around Procedure Review
d
if
Do the normal go-around procedure.
on
tro
lle
Advance thrust to go-around smoothly and slowly to
avoid excessive pitch-up.
nc
Approach Checklist
U
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing Configuration
Establish landing configuration early on final
approach.
▼ Continued on next page ▼
9.24
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9.25
737 Flight Crew Operations Manual
▼Stabilizer Trim Inoperative continued▼
Additional Deferred Item
or
pr
in
te
d
GROUND PROXIMITY
FLAP INHIBIT switch . . . . . . . . . . . . FLAP INHIBIT
Landing Checklist
ENGINE START switches . . . . . . . . . . . . . . . CONT
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
ad
ed
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps. . . . . . . . . . . . . . . . . . . . . . 15, Green light
U
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■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
9.25
9.26
737 Flight Crew Operations Manual
STBY RUD ON
STBY
RUD ON
Condition:
STANDBY RUDDER ON
The standby rudder hydraulic system is
commanded on.
1 Choose one:
or
pr
in
te
d
STBY RUD ON light is illuminated with no other
flight deck indications:
Avoid large or abrupt rudder pedal inputs.
■■■■
ad
ed
STBY RUD ON light is illuminated due to the pilot
moving the FLT CONTROL A or B switch to STBY
RUD:
do
w
nl
o
■■■■
STBY RUD ON light is illuminated in response to a
hydraulic system non-normal situation:
U
nc
on
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if
■■■■
9.26
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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March 31, 2023
9.27
737 Flight Crew Operations Manual
Trailing Edge Flap Asymmetry
One or more of these occur:
•An uncommanded roll occurs when the
flaps change position
•The left and right flap indications
disagree.
Objective:
To configure the airplane for landing.
or
pr
in
te
d
Condition:
1 Set the flap lever to the nearest detent that is equal
to or less than the smallest indicated flap position.
do
w
nl
o
ad
ed
Caution! Do not attempt to move the trailing
edge flaps with the ALTERNATE FLAPS
switch because there is no asymmetry
protection.
Note: Do not use FMC performance predictions
with any flaps or slats extended.
U
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on
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if
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
9.27
9.28
737 Flight Crew Operations Manual
▼Trailing Edge Flap Asymmetry continued▼
2 Choose one:
Flap lever is set to 30:
Set VREF 30.
►►Go to step 4
►►Go to step 3
ad
ed
Flap lever is set to 15 or 25:
or
pr
in
te
d
Note: VREF + wind additive must not
exceed the flap placard speed for
flaps 40.
do
w
nl
o
Flap lever is set to 1 or greater and less than
15:
Consider burning off fuel to reduce
touchdown speed.
Set VREF 40 + 30 knots.
d
if
►►Go to step 4
on
tro
lle
Flap lever is set to UP:
U
nc
►►Go to the Trailing Edge Flaps Up
Landing checklist on page 9.40
9.28
■■■■
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
9.29
737 Flight Crew Operations Manual
▼Trailing Edge Flap Asymmetry continued▼
3 Set VREF 15 or VREF ICE.
Note: If any of the following conditions apply,
set VREF ICE = VREF 15 + 10 knots:
ad
ed
or
pr
in
te
d
•Engine anti–ice will be used during
landing
•Wing anti–ice has been used any
time during the flight
•Icing conditions were encountered
during the flight and the landing
temperature is below 10° C.
Note: When VREF ICE is needed, the wind
additive should not exceed 5 knots.
do
w
nl
o
VREF 15 + wind additive, or VREF ICE
+ wind additive if needed, must not
exceed the flap placard speed for the
next larger flap setting.
on
tro
lle
d
if
4 Check the Non–Normal Configuration Landing
Distance tables in the Performance Inflight-QRH
chapter or other approved source.
5 Checklist Complete Except Deferred Items
U
nc
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
9.29
9.30
737 Flight Crew Operations Manual
▼Trailing Edge Flap Asymmetry continued▼
Deferred Items
Descent Checklist
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
or
pr
in
te
d
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing data . . . . . . . . . . .VREF ___ as directed
by checklist, Minimums ___
Approach Checklist
ad
ed
Approach briefing . . . . . . . . . . . . . . . . Completed
do
w
nl
o
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Additional Deferred Item
if
Choose one:
d
Flap lever is set to 30:
on
tro
lle
►►Go to Landing Checklist below
U
nc
Flap lever is set to less than 30:
GROUND PROXIMITY FLAP
INHIBIT switch . . . . . . . . . FLAP INHIBIT
►►Go to Landing Checklist below
Landing Checklist
ENGINE START switches. . . . . . . . . . . . . . . . CONT
▼ Continued on next page ▼
9.30
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
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9.31
737 Flight Crew Operations Manual
▼Trailing Edge Flap Asymmetry continued▼
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps. . . . . . . . . . . . . ___, Green or amber light
U
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on
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lle
d
if
do
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ad
ed
■■■■
or
pr
in
te
d
Note: The light can be green or amber depending
on the cause of the failure.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
9.31
9.32
737 Flight Crew Operations Manual
Trailing Edge Flap Disagree
The trailing edge flaps are not in the
commanded position.
Objective:
To configure the airplane for landing.
1 Choose one:
or
pr
in
te
d
Condition:
Trailing edge flap asymmetry exists:
►►Go to the Trailing Edge Flap
Asymmetry checklist on page 9.27
ad
ed
■■■■
Trailing edge flap asymmetry does not exist:
do
w
nl
o
►►Go to step 2
2 Choose one:
if
Indicated flap position is 30 or greater and less
than 40:
d
Land using existing flaps.
on
tro
lle
►►Go to step 3
U
nc
Indicated flap position is 15 or greater and less
than 30:
Land using existing flaps.
►►Go to step 5
Indicated flap position is less than 15:
►►Go to step 4
3 Set VREF 30.
▼ Continued on next page ▼
9.32
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
9.33
737 Flight Crew Operations Manual
▼Trailing Edge Flap Disagree continued▼
Note: VREF 30 + wind additive must not exceed the
flap placard speed for flaps 40.
►►Go to step 6
or
pr
in
te
d
4 Plan to extend flaps to 15 using alternate flap
extension.
Note: Alternate flap extension time to flaps 15 is
approximately 2 minutes.
ad
ed
The drag penalty with the leading edge
devices extended can make it impossible to
reach an alternate field.
5 Set VREF 15 or VREF ICE.
do
w
nl
o
Note: If any of the following conditions apply,
set VREF ICE = VREF 15 + 10 knots:
Note: When VREF ICE is needed, the wind
additive should not exceed 5 knots.
VREF 15 + wind additive, or VREF ICE
+ wind additive if needed, must not
exceed the flap placard speed for the
next larger flap setting.
U
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on
tro
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d
if
•Engine anti–ice will be used during
landing
•Wing anti–ice has been used any
time during the flight
•Icing conditions were encountered
during the flight and the landing
temperature is below 10° C.
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
9.33
9.34
737 Flight Crew Operations Manual
▼Trailing Edge Flap Disagree continued▼
6 Check the Non–Normal Configuration Landing
Distance tables in the Performance Inflight-QRH
chapter or other approved source.
Deferred Items
Descent Checklist
or
pr
in
te
d
7 Checklist Complete Except Deferred Items
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
ad
ed
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
do
w
nl
o
Landing data . . . . . . . . . . .VREF ___ as directed
by checklist, Minimums ___
Approach briefing . . . . . . . . . . . . . . . . Completed
Approach Checklist
on
tro
lle
d
if
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
U
nc
▼ Continued on next page ▼
9.34
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
9.35
737 Flight Crew Operations Manual
▼Trailing Edge Flap Disagree continued▼
Additional Deferred Item
Choose one:
Indicated flap position is 30 or greater:
or
pr
in
te
d
►►Go to Landing Checklist below
Indicated flap position is 15 or greater and less
than 30:
ad
ed
GROUND PROXIMITY FLAP
INHIBIT switch . . . . . . . . . .FLAP INHIBIT
►►Go to Landing Checklist below
do
w
nl
o
Indicated flap position is less than 15:
GROUND PROXIMITY FLAP
INHIBIT switch . . . . . . . . . .FLAP INHIBIT
on
tro
lle
d
if
►►Go to Alternate Flap Extension
below
Alternate Flap Extension
U
nc
During flap extension, set the flap lever to the
desired flap position.
230K maximum during alternate flap extension.
ALTERNATE FLAPS master switch . . . . . . . ARM
Note: The landing gear configuration warning
can sound if the flaps are between 10 and
15 and the landing gear are retracted.
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
9.35
9.36
737 Flight Crew Operations Manual
▼Trailing Edge Flap Disagree continued▼
YL061 - YW351
Note: The amber LE FLAPS TRANSIT light stays
illuminated until the flaps approach the
flaps 15 position.
or
pr
in
te
d
YK820
Note: The amber LE FLAPS TRANSIT light stays
illuminated until the flaps approach the
flaps 10 position.
ad
ed
Note: Operation within the lower amber airspeed
band can be needed until the LE FLAPS
TRANSIT light extinguishes.
on
tro
lle
d
if
do
w
nl
o
If flap asymmetry occurs, release the switch
immediately. There is no asymmetry protection.
ALTERNATE FLAPS
position switch . . . . . . . . . . . . . . . Hold DOWN
to extend flaps
to 15 on schedule
As flaps are extending, slow to respective
maneuvering speed.
U
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▼ Continued on next page ▼
9.36
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
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9.37
737 Flight Crew Operations Manual
▼Trailing Edge Flap Disagree continued▼
Choose one:
Trailing edge flaps asymmetry occurs:
■■■■
or
pr
in
te
d
►►Go to the Trailing Edge Flap
Asymmetry checklist on page
9.27
Trailing edge flaps extend to 15:
►►Go to Landing Checklist below
ad
ed
Indicated flap position is less than 1 after
attempting alternate flap extension:
do
w
nl
o
►►Go to the Trailing Edge Flaps Up
Landing checklist on page 9.40
■■■■
on
tro
lle
d
if
Indicated flap position is 1 or greater and
less than 15 after attempting alternate flap
extension:
Land using existing flaps.
Consider burning off fuel to reduce
touchdown speed.
nc
Set VREF 40 + 30 knots.
U
Check the Non–Normal Configuration
Landing Distance tables in the
Performance Inflight-QRH chapter or
other approved source.
►►Go to Landing Checklist below
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
9.37
9.38
737 Flight Crew Operations Manual
▼Trailing Edge Flap Disagree continued▼
Landing Checklist
ENGINE START switches. . . . . . . . . . . . . . . . CONT
or
pr
in
te
d
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps . . . . . . . . . . . . . ___, Green or amber light
Note: The light can be green or amber depending
on the cause of the failure.
U
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lle
d
if
do
w
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ad
ed
■■■■
9.38
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
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9.39
do
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or
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737 Flight Crew Operations Manual
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if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
9.39
9.40
737 Flight Crew Operations Manual
Trailing Edge Flaps Up Landing
The trailing edge flaps are less than 1.
Objective:
To configure for a landing with trailing edge
flaps less than 1.
or
pr
in
te
d
Condition:
1 Choose one:
Trailing edge flap asymmetry exists:
►►Go to step 2
Trailing edge flap asymmetry does not exist:
do
w
nl
o
►►Go to step 4
ad
ed
Do this checklist only when directed by the
Trailing Edge Flap Disagree checklist.
230K maximum.
2
on
tro
lle
d
if
ALTERNATE FLAPS master switch . . . . . . . ARM
Note: This procedure extends the leading edge
devices only.
3 ALTERNATE FLAPS
position switch . . . . . . . . . . . . Momentary DOWN
U
nc
Verify that the LE DEVICES annunciator
indicates FULL EXT for all leading edge slats and
flaps.
Note: The LE FLAPS TRANSIT light can stay
illuminated after the LE devices are fully
extended.
▼ Continued on next page ▼
9.40
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
9.41
737 Flight Crew Operations Manual
▼Trailing Edge Flaps Up Landing continued▼
4 Choose one:
LE DEVICES annunciator shows FULL EXT:
►►Go to step 5
or
pr
in
te
d
LE DEVICES annunciator does not show FULL
EXT:
►►Go to the All Flaps Up Landing
checklist on page 9.4
ad
ed
■■■■
5 Consider burning off fuel to reduce touchdown
speed.
do
w
nl
o
6 Set VREF 40 + 40 knots.
7 Check the Non–Normal Configuration Landing
Distance tables in the Performance Inflight-QRH
chapter or other approved source.
if
8 Maintain flaps up maneuvering speed until on final.
on
tro
lle
d
9 Limit bank angle to 15° when airspeed is less than
the flaps up maneuvering speed.
10 Checklist Complete Except Deferred Items
nc
Deferred Items
U
Descent Checklist
Pressurization. . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
9.41
9.42
737 Flight Crew Operations Manual
▼Trailing Edge Flaps Up Landing continued▼
Landing data . . . . . . . . VREF 40 + 40 knots ___,
Minimums ___
Go-Around Procedure Review
or
pr
in
te
d
Approach briefing . . . . . . . . . . . . . . . . Completed
Do the normal go-around procedure except:
Limit bank angle to 15° when the airspeed is
less than the flaps up maneuvering speed.
ad
ed
Accelerate to flaps up maneuvering speed.
do
w
nl
o
Do not exceed 230 knots with leading edge
devices extended.
Approach Checklist
if
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
U
nc
on
tro
lle
d
▼ Continued on next page ▼
9.42
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
9.43
737 Flight Crew Operations Manual
▼Trailing Edge Flaps Up Landing continued▼
Additional Deferred Items
FASTEN BELTS switch . . . . . . . . . . . . . . . . . . . ON
or
pr
in
te
d
GROUND PROXIMITY
FLAP INHIBIT switch . . . . . . . . . . . . FLAP INHIBIT
Note: A nuisance stick shaker can occur when
slowing to VREF 40 + 40 knots at high
gross weights and/or bank angles greater
than 15°.
ad
ed
Operation within the lower amber airspeed
band for landing is normal for this
condition.
do
w
nl
o
Note: V/S and VNAV PTH modes can revert to LVL
CHG mode.
Landing Checklist
if
ENGINE START switches . . . . . . . . . . . . . . . CONT
on
tro
lle
d
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
YL061 - YW351
U
nc
Note: The SPEED BRAKE lever will not move
beyond the FLIGHT DETENT on landing and
the spoilers will not fully deploy.
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps. . . . . . . . . . . . . ___, Green or amber light
Note: The light can be green or amber depending
on the cause of the failure.
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
9.43
9.44
737 Flight Crew Operations Manual
YAW DAMPER
YAW
DAMPER
Condition:
YAW DAMPER
The yaw damper is disengaged.
1 YAW DAMPER switch . . . . . . . . . . . . OFF then ON
2 Choose one:
■■■■
or
pr
in
te
d
YAW DAMPER light extinguishes:
YAW DAMPER light stays illuminated:
►►Go to step 3
ad
ed
YAW DAMPER switch . . . . . . . . . . . . OFF
do
w
nl
o
3 Avoid areas of predicted moderate or severe
turbulence. If turbulence is encountered and
passenger comfort becomes affected, reduce
airspeed and/or descend to a lower altitude.
4 Do not exceed flaps 30.
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on
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lle
d
if
■■■■
9.44
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
10 Flight Instruments,
NNC.10-Flight
Instruments,
Displays
Displays
(tab)
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Flight Instruments, Displays
Section 10
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Table of Contents
Airspeed Unreliable..................................... 10.1
Airspeed Unreliable (Stick Shaker Deactivation
by Pulling Circuit Breaker)..................... 10.10
NNC. 19
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Airspeed Unreliable..................................... 10.1
Airspeed Unreliable (Stick Shaker Deactivation
by Pulling Circuit Breaker)..................... 10.10
ALT DISAGREE............................................. 10.20
AOA DISAGREE............................................ 10.23
CDS FAULT.................................................. 10.23
Display Failure ............................................. 10.24
DISPLAYS CONTROL PANEL ........................... 10.25
DISPLAY SOURCE......................................... 10.26
FLIGHT RECORDER OFF ................................ 10.27
IAS DISAGREE............................................. 10.28
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March 31, 2023
2
D6-27370-8AS-NOK
10.TOC.1
Non-Normal Checklists Flight Instruments, Displays
737 Flight Crew Operations Manual
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Table of Contents
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Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
10.TOC.2
D6-27370-8AS-NOK
March 31, 2023
10.1
737 Flight Crew Operations Manual
Flight
File
Highlight
Instruments, Displays
Airspeed Unreliable
YR323 - YW351
Airspeed or Mach indications are suspected
to be unreliable. (Items which might indicate
unreliable airspeed are listed in the
Additional Information section.)
Objective:
To identify a reliable airspeed indication, if
possible, or to use the Flight With Unreliable
Airspeed table in the Performance Inflight
chapter for the remainder of the flight.
ad
ed
or
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Condition:
1 Autopilot (if engaged) . . . . . . . . . . . . .Disengage
do
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2 Autothrottle (if engaged). . . . . . . . . . .Disengage
3 F/D switches (both) . . . . . . . . . . . . . . . . . . OFF
4 Set the following gear up pitch attitude and thrust:
Flaps extended . . . . . . . . . . 10° and 80% N1
if
Flaps up . . . . . . . . . . . . . . . . 4° and 75% N1
on
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----------------------5 PROBE HEAT switches . . . . . . . . . . . . . Check ON
6 The following indications are reliable:
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nc
Attitude
N1
Ground speed
Radio altitude
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
10.1
10.2
737 Flight Crew Operations Manual
▼Airspeed Unreliable continued▼
or
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Note: Stick shaker, overspeed warning and
AIRSPEED LOW (as installed) alerts may
sound erroneously or simultaneously.
Note: The Flight Path Vector and Pitch Limit
Indicator may be unreliable.
7 Choose one:
Reliable airspeed indication can be determined:
►►Go to step 11
ad
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Use the reliable airspeed indication for the
remainder of the flight.
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Reliable airspeed indication cannot be
determined:
►►Go to step 8
on
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d
if
8 Refer to the Flight With Unreliable Airspeed table in
the Performance Inflight chapter and set the pitch
attitude and thrust setting for the current airplane
configuration and phase of flight.
9 When in trim and stabilized:
U
nc
Compare the captain, first officer and standby
airspeed indicators with the airspeed shown in
the table.
An airspeed indication that differs by more
than 20 knots or 0.03 Mach from the
airspeed shown in the table should be
considered unreliable.
▼ Continued on next page ▼
10.2
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
10.3
737 Flight Crew Operations Manual
▼Airspeed Unreliable continued▼
10 Choose one:
Reliable airspeed indication can be determined:
►►Go to step 11
or
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Use the reliable airspeed indication for the
remainder of the flight.
Reliable airspeed indication cannot be
determined:
ad
ed
►►Go to step 12
11 Choose one:
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Captain’s or First Officer’s airspeed indication
is reliable:
Flight director switch
(reliable side) . . . . . . . . . . . . . . . . . . ON
if
►►Go to step 14
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Only the standby airspeed indication is
reliable:
Note: Do not use the autopilot,
autothrottle, or flight directors.
nc
►►Go to step 16
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12 Set pitch attitude and thrust from the Flight With
Unreliable Airspeed table in the Performance
Inflight chapter for the airplane configuration and
phase of flight, as needed.
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
10.3
10.4
737 Flight Crew Operations Manual
▼Airspeed Unreliable continued▼
13 Check the Non-Normal Configuration Landing
Distance tables in the Performance Inflight-QRH
chapter or other approved source.
Note: Maintain visual conditions if possible.
or
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Establish landing configuration early.
Radio altitude reference is available below
2,500 feet.
ad
ed
Use electronic and visual glideslope
indicators, where available, for approach and
landing.
►►Go to step 16
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Do not use the autopilot, autothrottle, or
flight directors.
14 Autopilot
(reliable side, if needed) . . . . . . . . . . . . . Engage
d
if
Note: Autopilot may not engage or may disengage
automatically.
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15 Do not use the autothrottle.
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▼ Continued on next page ▼
10.4
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
10.5
737 Flight Crew Operations Manual
▼Airspeed Unreliable continued▼
16 Choose one:
Captain’s or First Officer’s altitude indication is
reliable:
►►Go to step 17
or
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Use the reliable altitude indication for the
remainder of the flight.
Captain’s and First Officer’s altitude indications
are unreliable:
ad
ed
Note: Airplane does not meet RVSM
airspace requirements.
do
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►►Go to step 21
17 Airplane may not meet RVSM airspace
requirements.
if
18 Set transponder to provide reliable altitude
reporting.
nc
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YR591 - YS823
ALT selector. . . . . . . . . . . . . . . (1 or 2) Select
reliable side
YR323, YR339, YV081 - YW351
ALT SOURCE selector . . . . . . . . (1 or 2) Select
reliable side
U
YR591 - YS823
19 Transponder mode selector . . . . . . . . . . . . . . TA
YR323, YR339, YV081 - YW351
20 Transponder mode selector . . . . . . . . . . TA ONLY
►►Go to step 22
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
10.5
10.6
737 Flight Crew Operations Manual
▼Airspeed Unreliable continued▼
21 Set transponder altitude reporting off.
YR323 - YS823, YV084, YV098 - YW351
Transponder mode
selector . . . . . . . . . . . . . . . . . . . . . ALT OFF
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YV081, YV083, YV097
Transponder mode
selector . . . . . . . . . . . . . . . . . ALT RPTG OFF
22 Checklist Complete Except Deferred Items
Review Before Descent
ad
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Deferred Items
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For approach, only set the BARO minimums on the
reliable PFD. Remove the BARO minimums from the
unreliable PFD.
d
if
Note: If BARO minimums are set only on the First
Officer’s PFD, DA/MDA aural callouts are not
provided.
on
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Go-Around Procedure Review
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Refer to the Performance Inflight chapter to
determine the go-around pitch attitude and thrust
setting:
For pitch attitude, refer to the Flight with
Unreliable Airspeed Go-Around table.
For thrust setting, refer to the Go-Around
%N1 table.
▼ Continued on next page ▼
10.6
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
10.7
737 Flight Crew Operations Manual
▼Airspeed Unreliable continued▼
Choose one:
Captain’s or First Officer’s airspeed indication
is reliable:
or
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When TO/GA is pushed, the flight director
pitch bar may automatically be removed.
An AFDS pitch mode change, such as LVL
CHG, restores the flight director pitch bar.
Note: Only use flight director guidance on
the reliable PFD.
ad
ed
■■■■
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Only the standby airspeed indication is
reliable:
Do not use TO/GA.
■■■■
if
Captain’s, First Officer’s, and standby
airspeed indications are unreliable:
■■■■
▼ Continued on next page ▼
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Do not use TO/GA.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
10.7
10.8
737 Flight Crew Operations Manual
▼Airspeed Unreliable continued▼
Additional Information
One or more of the following may be associated with
unreliable airspeed or Mach indications:
on
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lle
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ed
or
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•Difference between captain and first officer airspeed
indications
•Speed/altitude information not consistent with pitch
attitude and thrust setting
•Blank or fluctuating airspeed indication
•Continuous or intermittent stick shaker
•IAS DISAGREE alert
•ALT DISAGREE alert
•AOA DISAGREE alert
•SPD failure flag
•SPD LIM failure flag
•Erroneous minimum speed bars
•Erroneous maximum speed bars
•Airspeed low aural
•Airspeed low PFD indications on one side
•Overspeed warning
•Erroneous Flight Director (FD) pitch command
•EEC ALTN light(s)
•Radome damage or loss
nc
If the AOA DISAGREE alert is shown, one or more of
the following flight deck effects can occur:
U
•Erroneous Pitch Limit Indicator (PLI)
•Windshear alerts
•Autoslat operation
10.8
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
10.9
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737 Flight Crew Operations Manual
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Intentionally
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Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
10.9
10.10
737 Flight Crew Operations Manual
Airspeed Unreliable
(Stick Shaker Deactivation by
Pulling Circuit Breaker)
YK820, YL061
Airspeed or Mach indications are suspected
to be unreliable. (Items which might indicate
unreliable airspeed are listed in the
Additional Information section.)
Objective:
To identify a reliable airspeed indication, if
possible, or to use the Flight With Unreliable
Airspeed table in the Performance Inflight
chapter for the remainder of the flight.
ad
ed
or
pr
in
te
d
Condition:
do
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1 Autopilot (if engaged) . . . . . . . . . . . . .Disengage
2 Autothrottle (if engaged) . . . . . . . . . . .Disengage
3 F/D switches (both) . . . . . . . . . . . . . . . . . . OFF
if
4 Set the following gear up pitch attitude and thrust:
d
Flaps extended. . . . . . . . . . . 10° and 80% N1
on
tro
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Flaps up . . . . . . . . . . . . . . . . 4° and 75% N1
----------------------5 PROBE HEAT switches . . . . . . . . . . . . . Check ON
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6 The following indications are reliable:
Attitude
N1
Ground speed
Radio altitude
▼ Continued on next page ▼
10.10
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
10.11
737 Flight Crew Operations Manual
▼Airspeed Unreliable (Stick Shaker Deactivation by Pulling Circuit
Breaker) continued▼
or
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in
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Note: Stick shaker, overspeed warning and
AIRSPEED LOW (as installed) alerts may
sound erroneously or simultaneously.
Note: The Flight Path Vector and Pitch Limit
Indicator may be unreliable.
7 Choose one:
Reliable airspeed indication can be determined:
ad
ed
Use the reliable airspeed indication for the
remainder of the flight.
►►Go to step 11
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Reliable airspeed indication cannot be
determined:
►►Go to step 8
on
tro
lle
d
if
8 Refer to the Flight With Unreliable Airspeed table in
the Performance Inflight chapter and set the pitch
attitude and thrust setting for the current airplane
configuration and phase of flight.
Compare the captain, first officer and standby
airspeed indicators with the airspeed shown in
the table.
An airspeed indication that differs by more
than 20 knots or 0.03 Mach from the
airspeed shown in the table should be
considered unreliable.
U
nc
9 When in trim and stabilized:
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
10.11
10.12
737 Flight Crew Operations Manual
▼Airspeed Unreliable (Stick Shaker Deactivation by Pulling Circuit
Breaker) continued▼
10 Choose one:
Reliable airspeed indication can be determined:
or
pr
in
te
d
Use the reliable airspeed indication for the
remainder of the flight.
►►Go to step 11
Reliable airspeed indication cannot be
determined:
ad
ed
►►Go to step 12
11 Choose one:
do
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Captain’s or First Officer’s airspeed indication
is reliable:
Flight director switch
(reliable side) . . . . . . . . . . . . . . . . . . ON
d
if
►►Go to step 14
on
tro
lle
Only the standby airspeed indication is
reliable:
►►Go to step 16
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Note: Do not use the autopilot,
autothrottle, or flight directors.
12 Set pitch attitude and thrust from the Flight With
Unreliable Airspeed table in the Performance
Inflight chapter for the airplane configuration and
phase of flight, as needed.
▼ Continued on next page ▼
10.12
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
10.13
737 Flight Crew Operations Manual
▼Airspeed Unreliable (Stick Shaker Deactivation by Pulling Circuit
Breaker) continued▼
13 Check the Non-Normal Configuration Landing
Distance table in the Performance Inflight-QRH
chapter or other approved source.
or
pr
in
te
d
Note: Maintain visual conditions if possible.
Establish landing configuration early.
Radio altitude reference is available below
2,500 feet.
ad
ed
Use electronic and visual glideslope
indicators, where available, for approach and
landing.
do
w
nl
o
Do not use the autopilot, autothrottle, or
flight directors.
►►Go to step 16
14 Autopilot
(reliable side, if needed) . . . . . . . . . . . . . Engage
on
tro
lle
d
if
Note: Autopilot may not engage or may disengage
automatically.
15 Do not use the autothrottle.
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▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
10.13
10.14
737 Flight Crew Operations Manual
▼Airspeed Unreliable (Stick Shaker Deactivation by Pulling Circuit
Breaker) continued▼
16 Choose one:
Captain’s or First Officer’s altitude indication is
reliable:
or
pr
in
te
d
Use the reliable altitude indication for the
remainder of the flight.
►►Go to step 17
ad
ed
Captain’s and First Officer’s altitude indications
are unreliable:
Note: Airplane does not meet RVSM
airspace requirements.
do
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►►Go to step 20
17 Airplane may not meet RVSM airspace
requirements.
if
18 Set transponder to provide reliable altitude
reporting.
on
tro
lle
d
ALT selector . . . . . . . . . . . . . .(1 or 2) Select
reliable side
19 Transponder mode selector . . . . . . . . . . . . . . TA
nc
►►Go to step 21
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20 Set transponder altitude reporting off.
Transponder mode
selector . . . . . . . . . . . . . . . . . . . . . . ALT OFF
▼ Continued on next page ▼
10.14
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
10.15
737 Flight Crew Operations Manual
▼Airspeed Unreliable (Stick Shaker Deactivation by Pulling Circuit
Breaker) continued▼
21 A nuisance stick shaker may be deactivated at
pilot’s discretion.
or
pr
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This improves recognition of a stall warning on
the opposite side.
Note: Elevator Feel Shift may be active, resulting in
increased control column forces.
22 Choose one:
Deactivating stick shaker is needed:
ad
ed
Only the active stick shaker should be
deactivated.
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►►Go to step 23
Deactivating stick shaker is not needed:
►►Go to step 25
on
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d
if
23 When the circuit breaker is pulled, increased
control column forces due to Elevator Feel Shift
activation are removed.
Note: The stick shaker on the opposite side is not
deactivated.
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▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
10.15
10.16
737 Flight Crew Operations Manual
▼Airspeed Unreliable (Stick Shaker Deactivation by Pulling Circuit
Breaker) continued▼
24 Choose one:
Stick shaker left needs to be deactivated:
or
pr
in
te
d
STICK SHAKER LEFT
circuit breaker (P18-2:E4) . . . . . . . . Pull
►►Go to step 25
Stick shaker right needs to be deactivated:
►►Go to step 25
ad
ed
STICK SHAKER RIGHT
circuit breaker (P6-1:B6) . . . . . . . . . Pull
do
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25 Checklist Complete Except Deferred Items
Deferred Items
Review Before Descent
on
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if
For approach, only set the BARO minimums on the
reliable PFD. Remove the BARO minimums from the
unreliable PFD.
▼ Continued on next page ▼
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Note: If BARO minimums are set only on the First
Officer’s PFD, DA/MDA aural callouts are not
provided.
10.16
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
10.17
737 Flight Crew Operations Manual
▼Airspeed Unreliable (Stick Shaker Deactivation by Pulling Circuit
Breaker) continued▼
Go-Around Procedure Review
or
pr
in
te
d
Refer to the Performance Inflight chapter to
determine the go-around pitch attitude and thrust
setting:
For pitch attitude, refer to the Flight with
Unreliable Airspeed Go-Around table.
ad
ed
For thrust setting, refer to the Go-Around
%N1 table.
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on
tro
lle
d
if
do
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▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
10.17
10.18
737 Flight Crew Operations Manual
▼Airspeed Unreliable (Stick Shaker Deactivation by Pulling Circuit
Breaker) continued▼
Choose one:
Captain’s or First Officer’s airspeed indication
is reliable:
or
pr
in
te
d
When TO/GA is pushed, the flight director
pitch bar may automatically be removed.
An AFDS pitch mode change, such as LVL
CHG, restores the flight director pitch bar.
Note: Only use flight director guidance on
the reliable PFD.
ad
ed
■■■■
do
w
nl
o
Only the standby airspeed indication is
reliable:
Do not use TO/GA.
■■■■
d
if
Captain’s, First Officer’s, and standby
airspeed indications are unreliable:
■■■■
▼ Continued on next page ▼
U
nc
on
tro
lle
Do not use TO/GA.
10.18
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
10.19
737 Flight Crew Operations Manual
▼Airspeed Unreliable (Stick Shaker Deactivation by Pulling Circuit
Breaker) continued▼
Additional Information
One or more of the following may be associated with
unreliable airspeed or Mach indications:
on
tro
lle
d
if
do
w
nl
o
ad
ed
or
pr
in
te
d
•Difference between captain and first officer airspeed
indications
•Speed/altitude information not consistent with pitch
attitude and thrust setting
•Blank or fluctuating airspeed indication
•Continuous or intermittent stick shaker
•IAS DISAGREE alert
•ALT DISAGREE alert
•AOA DISAGREE alert
•SPD failure flag
•SPD LIM failure flag
•Erroneous minimum speed bars
•Erroneous maximum speed bars
•Airspeed low aural
•Airspeed low PFD indications on one side
•Overspeed warning
•Erroneous Flight Director (FD) pitch command
•EEC ALTN lights(s)
•Radome damage or loss
U
nc
If the AOA DISAGREE alert is shown, one or more of
the following flight deck effects can occur:
•Erroneous Pitch Limit Indicator (PLI)
•Windshear alerts
•Autoslat operation
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
10.19
10.20
737 Flight Crew Operations Manual
ALT DISAGREE
ALT DISAGREE
The ALT DISAGREE alert indicates the
captain’s and first officer’s altitude
indications disagree.
YR323 - YW351
1 Choose one:
IAS DISAGREE alert is shown:
or
pr
in
te
d
Condition:
►►Go to the Airspeed Unreliable
checklist on page 10.1
ad
ed
■■■■
IAS DISAGREE alert is not shown:
do
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►►Go to step 3
YK820, YL061
2 Choose one:
IAS DISAGREE alert is shown:
on
tro
lle
d
if
►►Go to the Airspeed Unreliable
(Stick Shaker Deactivation by
Pulling Circuit Breaker) checklist on
page 10.10
■■■■
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nc
IAS DISAGREE alert is not shown:
►►Go to step 3
3 Verify all altimeters are set to correct barometric
setting.
▼ Continued on next page ▼
10.20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
10.21
737 Flight Crew Operations Manual
▼ALT DISAGREE continued▼
4 Choose one:
ALT DISAGREE alert extinguishes:
■■■■
or
pr
in
te
d
Continue normal operation.
ALT DISAGREE alert stays illuminated:
Note: Airplane does not meet RVSM
airspace requirements.
ad
ed
►►Go to step 5
5 Standby altimeter is available.
do
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6 Do not use the flight path vector.
7 Maintain visual conditions if possible.
8 Choose one:
A reliable altitude can be determined:
d
if
►►Go to step 9
on
tro
lle
A reliable altitude cannot be determined:
►►Go to step 10
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nc
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
D6-27370-8AS-NOK
10.21
10.22
737 Flight Crew Operations Manual
▼ALT DISAGREE continued▼
9 Set transponder to provide reliable altitude
reporting
or
pr
in
te
d
YK820, YL061, YR591 - YS823
ALT selector . . . . . . . . . . . . . . .(1 or 2) Select
reliable side
YR323, YR339, YV081 - YW351
ALT SOURCE selector . . . . . . . .(1 or 2) Select
reliable side
►►Go to step 11
ad
ed
10 Set transponder altitude reporting off.
do
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nl
o
YK820 - YS823, YV084, YV098 - YW351
Transponder mode
selector . . . . . . . . . . . . . . . . . . . . . . ALT OFF
if
YV081, YV083, YV097
Transponder mode
selector . . . . . . . . . . . . . . . . . . ALT RPTG OFF
on
tro
lle
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11 Checklist Complete Except Deferred Items
Deferred Items
Review Before Descent:
U
nc
For approach, only set the BARO minimums on the
reliable PFD. Remove the BARO minimums from the
unreliable PFD.
Note: If BARO minimums are set only on the First
Officer’s PFD, DA/MDA aural callouts are not
provided.
Establish landing configuration early
▼ Continued on next page ▼
10.22
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737 Flight Crew Operations Manual
▼ALT DISAGREE continued▼
Radio altitude reference is available below 2,500 feet
■■■■
AOA DISAGREE
or
pr
in
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d
Use electronic and visual glideslope indicators, where
available, for approach and landing.
AOA DISAGREE
The AOA DISAGREE alert indicates the left
and right angle of attack vanes disagree.
ad
ed
Condition:
YR323 - YW351
do
w
nl
o
►►Go to the Airspeed Unreliable checklist on
page 10.1
YK820, YL061
on
tro
lle
CDS FAULT
CDS FAULT
The CDS FAULT annunciation indicates a
CDS fault occurs.
U
nc
Condition:
■■■■
d
if
►►Go to the Airspeed Unreliable (Stick Shaker
Deactivation by Pulling Circuit Breaker)
checklist on page 10.10
Note: CDS FAULT annunciates on the ground only,
before the second engine start.
1 Do not takeoff.
■■■■
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10.24
737 Flight Crew Operations Manual
Display Failure
Condition:
A display in the common display system is
failed.
1 Choose one:
or
pr
in
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A single display is not usable and automatic
switching has occurred:
Continue normal operation.
■■■■
do
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►►Go to step 2
ad
ed
A single display is not usable and automatic
switching has not occurred:
2 MAIN PANEL DUs selector . . . . . . . . . .As needed
3 LOWER DU selector. . . . . . . . . . . . . . .As needed
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■■■■
10.24
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737 Flight Crew Operations Manual
DISPLAYS CONTROL PANEL
DISPLAYS CONTROL PANEL
Condition:
The DISPLAYS CONTROL PANEL
annunciation indicates the EFIS control
panel is failed.
or
pr
in
te
d
Note: The altimeter blanks and an ALT flag
illuminates on the side corresponding to the
failed control panel.
1 CONTROL PANEL select
switch . . . . . . . . . . . . .BOTH ON 1 or BOTH ON 2
ad
ed
Select the operating control panel.
2 Verify that the DISPLAYS CONTROL PANEL
annunciation and ALT flag extinguish.
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10.26
737 Flight Crew Operations Manual
DSPLY SOURCE
DISPLAY SOURCE
The DSPLY SOURCE 1 or DSPLY SOURCE 2
annunciation indicates only one DEU is
supplying display information. Indications
may include:
•No hydraulic pressure indication on the
failed side
•Speed limit flag shown on the failed side
•Minimum maneuver speed and stick
shaker band removed on the failed side
•Both EEC ALTN lights illuminated.
or
pr
in
te
d
Condition:
ad
ed
Note: Flight director indications may be removed
and autoflight mode reversions may occur.
do
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Dual autopilot approach is not available.
1 Choose one:
DSPLY SOURCE 1 annunciation is shown:
on
tro
lle
d
if
Verify that the correct flight director
indications and flight mode annunciations
are shown on the first officer’s side.
Select Autopilot B.
►►Go to step 2
U
nc
DSPLY SOURCE 2 annunciation is shown:
Verify that the correct flight director
indications and flight mode annunciations
are shown on the captain’s side.
Select Autopilot A.
►►Go to step 2
▼ Continued on next page ▼
10.26
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737 Flight Crew Operations Manual
▼DISPLAY SOURCE continued▼
2 Choose one:
EEC ALTN lights are illuminated:
►►Go to step 3
■■■■
3 Choose one:
or
pr
in
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d
EEC ALTN lights are not illuminated:
EEC ALTERNATE MODE checklist has been
completed:
ad
ed
■■■■
do
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EEC ALTERNATE MODE checklist has not been
completed:
OFF - Flight Recorder
on
tro
lle
OFF
Condition:
■■■■
d
if
►►Go to the EEC ALTERNATE MODE
checklist on page 7.14
FLIGHT RECORDER OFF
The flight recorder is off.
■■■■
U
nc
1 Continue normal operation.
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10.28
737 Flight Crew Operations Manual
IAS DISAGREE
IAS DISAGREE
Condition:
The IAS DISAGREE alert indicates the
captain’s and first officer’s airspeed
indications disagree.
YR323 - YW351
or
pr
in
te
d
►►Go to the Airspeed Unreliable checklist on
page 10.1
YK820, YL061
►►Go to the Airspeed Unreliable (Stick Shaker
Deactivation by Pulling Circuit Breaker)
checklist on page 10.10
U
nc
on
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if
do
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ad
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■■■■
10.28
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11 Flight Management,
NNC.11-Flight
Management,
Navigation
Navigation
(tab)
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Flight Management, Navigation
Section 11
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Table of Contents
ADS-B Out Failure .......................................... 11.1
FMC DISAGREE .............................................. 11.2
FMC DISAGREE - VERTICAL ............................. 11.3
FMC FAIL ...................................................... 11.4
FMC FAIL ...................................................... 11.6
FMC/CDU ALERTING MESSAGE......................... 11.9
GLS.............................................................. 11.9
GPS............................................................ 11.10
ILS............................................................. 11.10
IRS DC FAIL ................................................ 11.11
IRS FAULT................................................... 11.12
IRS ON DC .................................................. 11.14
UNABLE REQD NAV PERF - RNP...................... 11.16
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2
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11.TOC.1
Non-Normal Checklists Flight Management, Navigation
737 Flight Crew Operations Manual
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Table of Contents
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11.TOC.2
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September 2, 2021
11.1
737 Flight Crew Operations Manual
Flight
File
Highlight
Management, Navigation
ADS-B Out Failure
One or more of these occur:
•ATC reports ADS-B Out is lost or degraded
•GPS-L or GPS-R INVALID message is in
the FMC scratchpad and the transponder
is selected to the related side.
•Transponder is failed
or
pr
in
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Condition:
1 Transponder selector. . . . . . . . . . Select opposite
transponder
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■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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11.1
11.2
737 Flight Crew Operations Manual
MSG DISAGREE
FMC
-and
FMC
MSG
FMC
DISAGREE
- FMC DISAGREE
FMC DISAGREE
M
S
G
YL061 - YW351
FMC
Condition:
or
pr
in
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d
P/RST
Data needed for dual FMC operation
disagree.
1 Choose one:
ad
ed
Flying an approach with an RNP alerting
requirement:
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Go-around unless suitable visual references
can be established and maintained.
■■■■
if
Flying an approach without an RNP alerting
requirement:
■■■■
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on
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Verify position.
11.2
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737 Flight Crew Operations Manual
MSG -and
FMC
DISAGREE
FMC
MSG
FMC
DISAGREE
- FMC
- VERTICAL
DISAGREE
- VERTICAL
- VERTICAL
FMC DISAGREE - VERTICAL
M
S
G
YL061 - YW351
FMC
One of the following occur:
•Left FMC and right FMC target airspeeds
disagree during descent
•Left FMC and right FMC vertical paths
disagree during descent.
ad
ed
Condition:
or
pr
in
te
d
P/RST
1 Do not move the FMC source select switch.
do
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The FMC will attempt to correct the difference
without crew action.
2 Monitor crossing altitudes to ensure compliance.
■■■■
if
Additional Information
on
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The disagreement will most likely be corrected when
crossing a waypoint with an altitude constraint.
U
nc
If the disagreement remains when entering the
approach phase, the FMC DISAGREE - VERTICAL
message will be replaced with the FMC DISAGREE
message. An approach with an RNP alerting
requirement is not authorized when the FMC
DISAGREE message is shown.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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11.3
11.4
737 Flight Crew Operations Manual
FMC - FMC FAIL (With Single FMC Option)
FMC
FMC FAIL
P/RST
YK820
One or more of these occur:
•Loss of FMC data on a CDU
•Loss of FMC data on a navigation display
map mode
•Illumination of the FMC alert light.
or
pr
in
te
d
Condition:
1 Resume conventional navigation. Without an
operating FMC, LNAV and VNAV are not available.
ad
ed
2 Verify position relative to terrain using conventional
navigation.
do
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Note: EGPWS may use inaccurate GPS position
data or an inappropriate value of RNP. This
could result in a VSD terrain display that is
incorrectly positioned relative to the airplane
track.
if
3 When preparing for approach:
on
tro
lle
d
Use the SPD REF selector to set the current
gross weight.
Use the SPD REF selector to set the reference
airspeed bugs.
U
nc
Use the N1 SET selector to set the N1 bugs.
11.4
▼ Continued on next page ▼
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11.5
737 Flight Crew Operations Manual
▼FMC FAIL continued▼
Note: For additional information on using the N1
SET and SPD REF selectors refer to:
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■■■■
or
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•Setting N1 Bugs with No Operative FMC
Supplementary Procedure (SP 7).
•Setting Airspeed Bugs with No Operative FMC
Supplementary Procedure (SP 10).
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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11.5
11.6
737 Flight Crew Operations Manual
FMC - FMC FAIL (With Dual FMC Option)
FMC
FMC FAIL
P/RST
YL061 - YW351
Display of VTK followed by MAP failure flags
on one or both navigation displays.
Objective:
To restore dual FMC operation, configure for
single FMC operation or resume conventional navigation.
Note: LNAV/VNAV may disengage.
or
pr
in
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Condition:
ad
ed
1 Check both navigation display MAP modes and FMC
CDUs.
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if
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▼ Continued on next page ▼
11.6
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11.7
737 Flight Crew Operations Manual
▼FMC FAIL continued▼
2 Choose one:
Both FMCs are failed.
►►Go to step 7
or
pr
in
te
d
No FMC data on the captain’s and first officer’s
navigation display MAP modes and no FMC data
on both CDUs:
No FMC data on the captain’s navigation display
MAP mode and no FMC data on both CDUs:
ad
ed
Left FMC is failed.
►►Go to step 3
do
w
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o
No FMC data on the first officer’s navigation
display MAP mode, MSG light is illuminated and
SINGLE FMC OPERATION scratchpad message is
shown:
if
Right FMC is failed.
on
tro
lle
d
►►Go to step 3
3 FMC source
select switch . . . . . . . .BOTH ON L or BOTH ON R
Select the operating FMC.
nc
4 Wait 1 minute.
U
5 Check for FMC-L and FMC-R bearing/distance
information on POS SHIFT page 3/3.
▼ Continued on next page ▼
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11.7
11.8
737 Flight Crew Operations Manual
▼FMC FAIL continued▼
6 Choose one:
Bearing/distance information for both FMCs are
displayed:
■■■■
or
pr
in
te
d
FMC source select switch . . . . . . NORMAL
Bearing/distance information for only a single
FMC is displayed:
Continue with single FMC operation.
ad
ed
■■■■
do
w
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7 Resume conventional navigation. Without an
operating FMC, LNAV and VNAV are not available.
YR323 - YW351
8 Verify position relative to terrain using conventional
navigation.
on
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lle
d
if
Note: EGPWS may use inaccurate GPS position
data or an inappropriate value of RNP. This
could result in a VSD terrain display that is
incorrectly positioned relative to the airplane
track.
9 When preparing for the approach:
U
nc
Use the SPD REF selector to set the current
gross weight.
Use the SPD REF selector to set the reference
airspeed bugs.
Use the N1 SET selector to set the N1 bugs.
▼ Continued on next page ▼
11.8
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11.9
737 Flight Crew Operations Manual
▼FMC FAIL continued▼
Note: For additional information on using the N1
SET and SPD REF selectors refer to:
■■■■
MSG -and
FMC
CDU
MSG
FMC
Alerting
- CDU Alerting
or
pr
in
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d
•Setting N1 Bugs with No Operative FMC
Supplementary Procedure (SP 7).
•Setting Airspeed Bugs with No Operative FMC
Supplementary Procedure (SP 10).
ad
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FMC/CDU ALERTING MESSAGE
M
S
G
FMC
Condition:
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P/RST
An alert message is in the FMC scratchpad.
GLS
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GLS
d
if
1 Take action as needed by the message.
GLS
YR323, YR339
A GLS failure occurs.
nc
Condition:
■■■■
U
1 Do not fly a GLS approach.
2 ILS and non-ILS approaches may be flown.
■■■■
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11.9
11.10
737 Flight Crew Operations Manual
GPS
GPS
GPS
Condition:
Both GPS receivers are failed.
Note: The FMC uses only IRS or radio inputs.
ADS-B is inoperative.
or
pr
in
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d
Look-ahead terrain alerting and display are
unavailable due to position uncertainty.
1 Continue normal operation if ANP meets the
requirements for the phase of flight.
ad
ed
■■■■
ILS
ILS
ILS
Condition:
do
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YR323, YR339
An ILS failure occurs.
if
1 Do not fly an ILS approach.
■■■■
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2 GLS and non-ILS approaches may be flown.
11.10
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11.11
737 Flight Crew Operations Manual
DC FAIL
IRS DC FAIL
DC FAIL
Condition:
IRS backup DC power is failed.
1 Choose one:
or
pr
in
te
d
One IRS DC FAIL light is illuminated and all other
IRS lights are extinguished:
Continue normal operation. The IRS is
operating normally on AC power.
■■■■
ad
ed
Both IRS DC FAIL lights are illuminated:
The IRS is operating normally on AC power.
do
w
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The battery is nearly discharged or the
switched hot battery bus is not powered.
The following systems may be inoperative:
Engine and APU fire extinguishing
■■■■
U
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on
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lle
d
if
APU start.
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11.11
11.12
737 Flight Crew Operations Manual
ALIGN and
FAULT
-and
IRS
FAULT
ALIGN - IRS
IRS FAULT
FAULT
One or more of these occur:
•An IRS fault occurs
•On the ground, if the ALIGN light is also
illuminated, the present position entry is
possibly incorrect.
or
pr
in
te
d
Condition:
1 Choose one:
On the ground:
In flight:
do
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►►Go to step 6
ad
ed
►►Go to step 2
On the ground
2 Choose one:
ALIGN light is extinguished:
on
tro
lle
d
if
Do not takeoff.
■■■■
U
nc
ALIGN light is also illuminated:
IRS mode selector
(failed side) . . . . . . . . . . . . . . . . . OFF
The FAULT light extinguishes
immediately and the ALIGN light
extinguishes after approximately 30
seconds.
►►Go to step 3
▼ Continued on next page ▼
11.12
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11.13
737 Flight Crew Operations Manual
▼IRS FAULT continued▼
3 After the ALIGN light extinguishes:
IRS mode selector
(failed side) . . . . . . . . . . . . . . . . . . . . NAV
4 Choose one:
ALIGN light is flashing:
or
pr
in
te
d
Enter present position.
Re-enter present position using the most
accurate latitude and longitude.
ad
ed
►►Go to step 5
do
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ALIGN light is not flashing:
►►Go to step 5
5 Choose one:
if
FAULT light illuminates again:
on
tro
lle
d
Do not takeoff.
■■■■
FAULT light does not illuminate again:
■■■■
U
nc
Verify IRS alignment is complete
In flight
6 Autopilot (if engaged) . . . . . . . . . . . . .Disengage
▼ Continued on next page ▼
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11.13
11.14
737 Flight Crew Operations Manual
▼IRS FAULT continued▼
7 IRS transfer switch . . . .BOTH ON L or BOTH ON R
Select the operating IRS.
or
pr
in
te
d
Note: The selected IRS is the source of:
•Attitude and heading for both PFDs and NDs
•AFDS guidance
•Weather radar information
•GPWS and Windshear alerts
ad
ed
Note: Autopilot(s) cannot be engaged.
8 Autothrottle (if engaged) . . . . . . . . . . .Disengage
do
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■■■■
ON DC
IRS ON DC
ON DC
IRS AC power is failed.
1 Choose one:
if
Condition:
on
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Left IRS ON DC light is illuminated:
The left IRS continues to operate as long as
DC power is available.
■■■■
U
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Right IRS ON DC light is illuminated:
Power to the right IRS is removed after 5
minutes.
■■■■
11.14
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11.15
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11.15
11.16
737 Flight Crew Operations Manual
UNABLE REQD NAV PERF - RNP (FMC Update U10.7 and Later)
UNABLE REQD NAV PERF - RNP
Condition:
UNABLE REQD NAV PERF-RNP is shown. The
actual navigation performance is not
sufficient.
or
pr
in
te
d
1 Choose one:
On a procedure or airway with an RNP alerting
requirement:
►►Go to step 2
►►Go to step 3
ad
ed
On a procedure or airway without an RNP
alerting requirement:
do
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2 Select an alternate procedure or airway. During an
approach, go-around unless suitable visual
references can be established and maintained.
if
Note: The FMC uses inertial inputs only, unless
radio updating is enabled.
on
tro
lle
d
If radio updating is allowed, consider doing
the following steps:
U
nc
•Select the FMC NAV OPTIONS page
•Select VOR UPDATE ON
11.16
■■■■
▼ Continued on next page ▼
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11.17
737 Flight Crew Operations Manual
▼UNABLE REQD NAV PERF - RNP continued▼
3 Verify position.
Note: The FMC uses inertial inputs only, unless
radio updating is enabled.
or
pr
in
te
d
If radio updating is allowed, consider doing
the following steps:
•Select the FMC NAV OPTIONS page
•Select VOR UPDATE ON
U
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Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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11.17
11.18
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11.18
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NNC.12-Fuel
12
Fuel (tab)
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Fuel
Section 12
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Table of Contents
CONFIG ........................................................ 12.1
CROSSFEED SELECTOR INOPERATIVE............... 12.2
FUEL FILTER BYPASS ...................................... 12.5
Fuel Leak Engine ............................................ 12.6
FUEL PUMP LOW PRESSURE........................... 12.12
Fuel Quantity Indication Inoperative ............... 12.13
Fuel Temperature Low .................................. 12.14
IMBAL ........................................................ 12.15
LOW ........................................................... 12.18
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Non-Normal Checklists Fuel
737 Flight Crew Operations Manual
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12.TOC.2
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12.1
737 Flight Crew Operations Manual
File Highlight
Fuel
CONFIG
(Airplanes with Center Tank Auto Shutoff)
CONFIG
All of these occur:
•Both center tank fuel pump switches are
off
•There is more than 726 kgs of fuel in the
center tank
•An engine is running.
or
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Condition:
1 Do not accomplish this procedure until established
in a level flight attitude.
ad
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2 CTR FUEL PUMP switches (both). . . . . . . . . . . ON
Verify that the LOW PRESSURE lights
extinguish.
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3 Resume normal fuel management.
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Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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D6-27370-8AS-NOK
12.1
12.2
737 Flight Crew Operations Manual
VALVE OPEN - Crossfeed
CROSSFEED SELECTOR
INOPERATIVE
VALVE
OPEN
One of the following occurs:
•The crossfeed VALVE OPEN light stays
illuminated bright blue
•The CROSSFEED selector is in the open
position and the crossfeed VALVE OPEN
light is extinguished
•When the CROSSFEED selector is rotated
to a new position, the crossfeed VALVE
OPEN light does not illuminate bright blue.
ad
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Condition:
May or may not be illuminated
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1 Check the FUEL CROSSFEED VALVE circuit breaker
(P6-3:B7).
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▼ Continued on next page ▼
12.2
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12.3
737 Flight Crew Operations Manual
▼CROSSFEED SELECTOR INOPERATIVE continued▼
2 Choose one:
FUEL CROSSFEED VALVE circuit breaker is
tripped:
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It is not possible to determine the position
of the fuel crossfeed valve.
Note: Verify that sufficient fuel is available
to both engines to complete the
flight.
IMBAL
ad
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Do not accomplish the following checklist:
■■■■
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FUEL CROSSFEED VALVE circuit breaker is not
tripped:
if
►►Go to step 3
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D6-27370-8AS-NOK
12.3
12.4
737 Flight Crew Operations Manual
▼CROSSFEED SELECTOR INOPERATIVE continued▼
3 Choose one:
CROSSFEED selector is in the closed position:
Crossfeed valve is failed open.
■■■■
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Note: Maintain fuel balance with selective
use of fuel pumps.
CROSSFEED selector is in the open position:
Crossfeed valve is failed closed.
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Note: As conditions allow, vary engine
thrust as needed to maintain fuel
balance.
Verify that sufficient fuel is available
to both engines to complete the
flight.
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■■■■
12.4
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12.5
737 Flight Crew Operations Manual
FILTER BYPASS
FILTER
BYPASS
Condition:
FUEL FILTER BYPASS
Fuel contamination can cause fuel to bypass
the engine fuel filter.
1 Choose one:
or
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Only one FILTER BYPASS light, ENG 1 or ENG 2,
has illuminated during the flight:
Note: Erratic engine operation and
flameout may occur on the affected
engine due to fuel contamination.
ad
ed
■■■■
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FILTER BYPASS lights for both engines illuminate
or have illuminated at any time during the flight
(either separately or at the same time):
►►Go to step 2
2 Plan to land at the nearest suitable airport.
■■■■
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Note: Erratic engine operation and flameout may
occur on either or both engines due to fuel
contamination.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 21, 2019
D6-27370-8AS-NOK
12.5
12.6
737 Flight Crew Operations Manual
Fuel Leak Engine
An engine fuel leak is suspected for the
reasons listed in the Additional Information
section of this checklist.
Objective:
To confirm there is an engine fuel leak and
shut down the affected engine if needed.
This checklist does not address the unlikely
possibility of a tank leak.
1 A diversion may be needed.
or
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Condition:
ad
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2 Main tank FUEL PUMPS switches (all) . . . . . . . ON
3 CROSSFEED selector . . . . . . . . . . . . . . . . . Close
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4 CTR FUEL PUMPS switches (both) . . . . . . . . . OFF
The fuel CONFIG alert may show with fuel in the
center tank.
if
The following steps check for an engine fuel leak
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5 Record the main tank fuel quantities and the
current time.
6 An engine fuel leak is confirmed if one or both of
the following are true:
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Fuel spray is observed from an engine or strut
A change in fuel imbalance of 230 kgs within 30
minutes or less
▼ Continued on next page ▼
12.6
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12.7
737 Flight Crew Operations Manual
▼Fuel Leak Engine continued▼
7 Choose one:
Engine fuel leak is confirmed:
►►Go to step 11
►►Go to step 8
8 Choose one:
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Engine fuel leak is not confirmed:
The center tank contains usable fuel:
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►►Go to step 9
The center tank does not contain usable fuel:
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►►Go to step 10
9 CTR FUEL PUMPS switches (both) . . . . . . . . . . ON
■■■■
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10 Resume normal fuel management.
An engine fuel leak is confirmed
11 The following steps shut down the engine to stop
an engine fuel leak.
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12 The engine to be shut down is the engine on the
side where the fuel quantity decreased faster.
13 Autothrottle . . . . . . . . . . . . . . . . . . . .Disengage
14 Thrust lever
(affected engine) . . . . . . Confirm . . . . . . . Close
▼ Continued on next page ▼
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D6-27370-8AS-NOK
12.7
12.8
737 Flight Crew Operations Manual
▼Fuel Leak Engine continued▼
15 When the affected engine is at idle thrust:
Engine start lever
(affected engine) . . . . Confirm . . . . . CUTOFF
or
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This closes the spar valve and stops an
engine fuel leak.
16 PACK switch (affected side) . . . . . . . . . . . . . OFF
YK820, YL061, YR591 - YS823
17 Choose one:
ad
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This causes the operating pack to regulate to
high flow in flight with the flaps up.
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APU is available for start:
APU . . . . . . . . . . . . . . . . . . . . . . START
When APU is running:
d
if
APU GEN switch
(affected side) . . . . . . . . . . . . . ON
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►►Go to step 18
APU is not available:
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►►Go to step 18
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YK820, YL061, YR591 - YS823
18 Transponder mode selector . . . . . . . . . . . . . . TA
This prevents climb commands which can
exceed single engine performance capability.
▼ Continued on next page ▼
12.8
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September 30, 2022
12.9
737 Flight Crew Operations Manual
▼Fuel Leak Engine continued▼
YR323, YR339, YV081 - YW351
19 Choose one:
APU is available for start:
When APU is running:
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APU . . . . . . . . . . . . . . . . . . . . . . START
APU GEN switch
(affected side) . . . . . . . . . . . . . ON
APU is not available:
ad
ed
►►Go to step 20
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►►Go to step 20
YR323, YR339, YV081 - YW351
20 Transponder mode selector . . . . . . . . . . TA ONLY
if
This prevents climb commands which can
exceed single engine performance capability.
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21 ISOLATION VALVE switch . . . . . . . . .Verify AUTO
This ensures bleed air is available to both wings
if wing anti-ice is needed.
22 Choose one:
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Fuel LOW alert is shown:
►►Go to step 23
Fuel LOW alert is not shown:
►►Go to step 25
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 21, 2019
D6-27370-8AS-NOK
12.9
12.10
737 Flight Crew Operations Manual
▼Fuel Leak Engine continued▼
23 CROSSFEED selector . . . . . . . . . . . . . . . . . Open
This ensures that all fuel is available to the
running engine.
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24 FUEL PUMPS switches (all). . . . . . . . . . . . . . . ON
This ensures that all fuel is available for use.
25 Plan to land at the nearest suitable airport.
Note: Balance fuel as needed. All remaining fuel
can be used for the running engine.
YK820, YL061, YR339 - YW351
ad
ed
Note: Do not use FMC performance predictions.
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►►Go to the One Engine Inoperative
Landing checklist on page 7.34
■■■■
YR323
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►►Go to the One Engine Inoperative
Landing checklist on page 7.38
■■■■
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▼ Continued on next page ▼
12.10
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D6-27370-8AS-NOK
September 30, 2022
12.11
737 Flight Crew Operations Manual
▼Fuel Leak Engine continued▼
Additional Information
Reasons that an engine fuel leak should be
suspected:
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•A visual observation of fuel spray
•The total fuel quantity is decreasing at an abnormal
rate
•An engine has excessive fuel flow
•The fuel IMBAL alert shows
•The fuel LOW alert shows
•The USING RSV FUEL message shows on the FMC
CDU
•The INSUFFICIENT FUEL message shows on the
FMC CDU
•The CHECK FMC FUEL QUANTITY message shows on
the FMC CDU.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 21, 2019
D6-27370-8AS-NOK
12.11
12.12
737 Flight Crew Operations Manual
LOW PRESSURE - Fuel Pump
LOW
PRESSURE
Condition:
FUEL PUMP LOW PRESSURE
The fuel pump pressure is low.
or
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Note: Fuel pump LOW PRESSURE lights may flicker
when tank quantity is low and the airplane is
in turbulent air or during climb or descent.
1 Choose one:
One main tank fuel pump LOW PRESSURE light
is illuminated:
ad
ed
Main tank FUEL PUMP switch
(affected pump). . . . . . . . . . . . . . . . OFF
Sufficient fuel pressure is available
for normal operation.
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■■■■
Both main tank fuel pump LOW PRESSURE lights
are illuminated:
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Note: At high altitude, thrust deterioration
or engine flameout may occur.
■■■■
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One CTR tank fuel pump LOW PRESSURE light is
illuminated:
►►Go to step 2
Both CTR tank fuel pump LOW PRESSURE lights
are illuminated:
►►Go to step 5
▼ Continued on next page ▼
12.12
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D6-27370-8AS-NOK
March 21, 2019
12.13
737 Flight Crew Operations Manual
▼FUEL PUMP LOW PRESSURE continued▼
2 CROSSFEED selector. . . . . . . . . . . . . . . . . Open
This prevents fuel imbalance.
3 CTR FUEL PUMP switch (affected side) . . . . . OFF
or
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4 When the other CTR tank fuel pump LOW
PRESSURE light illuminates:
CROSSFEED selector . . . . . . . . . . . . . . Close
Remaining CTR FUEL PUMP switch . . . . . . OFF
ad
ed
■■■■
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Both CTR tank fuel pump LOW PRESSURE lights
are illuminated
5 CTR FUEL PUMP switches (both). . . . . . . . . . OFF
6 Fuel CONFIG alert may show with fuel in the center
tank.
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7 Center tank fuel is unusable. Main tank fuel may
not be sufficient for the planned flight.
■■■■
Fuel Quantity Indication Inoperative
nc
Condition:
The fuel quantity indication is blank.
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1 Enter and periodically update the manually
calculated FUEL weight on the FMC PERF INIT page.
■■■■
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12.13
12.14
737 Flight Crew Operations Manual
Fuel Temperature Low
Condition:
Fuel temperature is near the minimum.
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1 When fuel temperature is approaching the fuel
temperature limit (3° C /5° F above the fuel freeze
point or - 43° C /- 45° F whichever is higher):
Increase speed, change altitude and/or deviate
to a warmer air mass to achieve a TAT equal to
or higher than the fuel temperature limit.
ad
ed
TAT will increase approximately 0.5 to 0.7° C for
each 0.01 Mach increase in speed. In extreme
conditions, it may be necessary to descend as
low as FL250.
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12.14
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12.15
737 Flight Crew Operations Manual
IMBAL
IMBAL
There is a fuel imbalance between the main
tanks.
Objective:
To decide if a fuel leak is suspected. To balance fuel if a fuel leak is not suspected.
or
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Condition:
1 If an engine has low fuel flow and unusual engine
indications, the IMBAL alert may show due to an
engine malfunction instead of a fuel leak.
ad
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2 The IMBAL alert may be caused by a fuel leak, an
inoperative crossfeed valve or a fuel imbalance.
3 A fuel leak should be suspected if one or more of
the following are true:
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The total fuel remaining is less than the planned
fuel remaining
An engine has excessive fuel flow.
if
4 Choose one:
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A fuel leak is suspected:
►►Go to the Fuel Leak Engine checklist
on page 12.6
nc
■■■■
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A fuel leak is not suspected:
►►Go to step 5
▼ Continued on next page ▼
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D6-27370-8AS-NOK
12.15
12.16
737 Flight Crew Operations Manual
▼IMBAL continued▼
5 CROSSFEED selector . . . . . . . . . . . . . . . . . Open
Verify that the VALVE OPEN light illuminates
bright, then dim. This indicates that the
crossfeed valve is operating correctly.
or
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6 Choose one:
Crossfeed valve is operating correctly:
►►Go to step 7
Crossfeed valve is not operating correctly:
ad
ed
►►Go to the CROSSFEED SELECTOR
INOPERATIVE checklist on page
12.2
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■■■■
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▼ Continued on next page ▼
12.16
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March 21, 2019
12.17
737 Flight Crew Operations Manual
▼IMBAL continued▼
7 Choose one:
Main tank 1 quantity is low:
or
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Main tank 1 FUEL PUMPS
switches (both) . . . . . . . . . . . . . . . . OFF
This allows fuel from the higher
quantity tank to feed both engines.
►►Go to step 8
Main tank 2 quantity is low:
ad
ed
Main tank 2 FUEL PUMPS
switches (both) . . . . . . . . . . . . . . . . OFF
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This allows fuel from the higher
quantity tank to feed both engines.
►►Go to step 8
if
8 When fuel balancing is complete:
d
Main tank FUEL PUMPS switches (all) . . . . . ON
■■■■
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CROSSFEED selector . . . . . . . . . . . . . . Close
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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D6-27370-8AS-NOK
12.17
12.18
737 Flight Crew Operations Manual
LOW
LOW
The fuel quantity is low in a main tank.
Objective:
To decide if a fuel leak is suspected. To
ensure that all fuel is available for use.
or
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Condition:
Note: Avoid high nose up attitude. Make thrust
changes slowly and smoothly. This reduces
the possibility of uncovering fuel pumps.
1 The fuel LOW alert may be caused by a fuel leak or
low fuel.
ad
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2 A fuel leak should be suspected if one or more of
the following are true:
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The total fuel remaining is less than the planned
fuel remaining.
An engine has excessive fuel flow.
on
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if
One main tank is abnormally low compared to
the other main tank and to the expected fuel
remaining in the tanks.
3 Choose one:
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A fuel leak is suspected:
►►Go to the Fuel Leak Engine checklist
on page 12.6
■■■■
A fuel leak is not suspected:
►►Go to step 4
▼ Continued on next page ▼
12.18
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12.19
737 Flight Crew Operations Manual
▼LOW continued▼
4 CROSSFEED selector. . . . . . . . . . . . . . . . . Open
This ensures that fuel is available to both
engines if the low tank empties.
or
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5 FUEL PUMPS switches (all). . . . . . . . . . . . . . . ON
This ensures that all fuel is available for use.
6 Plan to land at the nearest suitable airport.
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Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 21, 2019
D6-27370-8AS-NOK
12.19
12.20
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12.20
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D6-27370-8AS-NOK
March 21, 2019
NNC.13-Hydraulics
13
Hydraulics (tab)
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Hydraulics
Section 13
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Table of Contents
HYDRAULIC PUMP LOW PRESSURE ................... 13.1
HYDRAULIC PUMP OVERHEAT ..........................13.2
LOSS OF SYSTEM A ........................................ 13.3
LOSS OF SYSTEM B ........................................ 13.6
MANUAL REVERSION or LOSS OF SYSTEM A AND
SYSTEM B ................................................ 13.12
STANDBY HYDRAULIC LOW PRESSURE............ 13.18
STANDBY HYDRAULIC LOW QUANTITY ............ 13.18
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 15, 2016
2
D6-27370-8AS-NOK
13.TOC.1
Non-Normal Checklists Hydraulics
737 Flight Crew Operations Manual
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Table of Contents
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13.TOC.2
D6-27370-8AS-NOK
September 15, 2016
13.1
737 Flight Crew Operations Manual
File Highlight
Hydraulics
LOW
PRESSURE - Hydraulic Pump (single)
HYDRAULIC PUMP LOW
PRESSURE
LOW
PRESSURE
Condition:
The hydraulic pump pressure is low.
1 HYD PUMP switch (affected side) . . . . . . . . . OFF
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■■■■
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Note: Loss of an engine-driven hydraulic pump and
a high demand on the system may result in
an intermittent illumination of the LOW
PRESSURE light for the remaining electric
motor-driven hydraulic pump.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 15, 2016
D6-27370-8AS-NOK
13.1
13.2
737 Flight Crew Operations Manual
OVERHEAT - Hydraulic Pump
OVERHEAT
Condition:
HYDRAULIC PUMP OVERHEAT
The hydraulic pump temperature is high.
1 ELEC HYD PUMP switch (affected side) . . . . . OFF
or
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Note: One pump supplies sufficient pressure for
normal system operation.
2 MFD SYS switch . . . . . . . . . . . . . . . . . . . . Push
3 Choose one:
ad
ed
Affected side hydraulic pressure is 3300 psi or
less:
■■■■
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Affected side hydraulic pressure is greater than
3300 psi:
ENG HYD PUMP switch
(affected side) . . . . . . . . . . . . . . . . . OFF
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►►Go to step 4
4 Choose one:
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System A HYD PUMPS switches are OFF:
►►Go to the LOSS OF SYSTEM A
checklist on page 13.3
■■■■
System B HYD PUMPS switches are OFF:
►►Go to the LOSS OF SYSTEM B
checklist on page 13.6
■■■■
13.2
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13.3
737 Flight Crew Operations Manual
LOW PRESSURE - Hydraulic Pump - System A (both)
LOSS OF SYSTEM A
FLT CONTROL
A HYD PUMPS
A
ENG 1
LOW
PRESSURE
LOW
PRESSURE
LOW
PRESSURE
Hydraulic system A pressure is low.
or
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Condition:
ELEC 2
1 System A
FLT CONTROL switch. . . . Confirm . . . . STBY RUD
ad
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2 System A
HYD PUMP switches (both) . . . . . . . . . . . . . OFF
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3 Check the Non–Normal Configuration Landing
Distance tables in the Performance Inflight-QRH
chapter or other approved source.
4 NOSE WHEEL STEERING switch . . . . . . . . . . ALT
5 Plan for manual gear extension.
▼ Continued on next page ▼
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Note: When the gear has been lowered manually, it
cannot be retracted. The drag penalty with
gear extended may make it impossible to
reach an alternate field.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 15, 2016
D6-27370-8AS-NOK
13.3
13.4
737 Flight Crew Operations Manual
▼LOSS OF SYSTEM A continued▼
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Note: Inoperative Items
Autopilot A inop
Autopilot B is available.
Flight spoilers (two on each wing) inop
Roll rate and speedbrake effectiveness may be
reduced in flight.
Normal landing gear extension and retraction
inop
Manual gear extension is needed.
Ground spoilers inop
Landing distance will be increased.
Alternate brakes inop
Normal brakes are available.
Engine 1 thrust reverser normal hydraulic
pressure inop
Thrust reverser will deploy and retract at a slower
rate and some thrust asymmetry can be
anticipated during thrust reverser deployment.
Normal nose wheel steering inop
Alternate nose wheel steering is available.
6 Checklist Complete Except Deferred Items
Deferred Items
nc
Descent Checklist
U
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing data . . . . . . . . . VREF ___, Minimums ___
▼ Continued on next page ▼
13.4
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13.5
737 Flight Crew Operations Manual
▼LOSS OF SYSTEM A continued▼
Approach briefing . . . . . . . . . . . . . . . . Completed
Approach Checklist
or
pr
in
te
d
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Manual Gear Extension
LANDING GEAR lever. . . . . . . . . . . . . . . . . . . OFF
Manual gear extension handles. . . . . . . . . . . . Pull
ad
ed
The uplock is released when the handle is pulled
to its limit.
do
w
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o
The related red landing gear indicator light
illuminates, indicating uplock release.
Wait 15 seconds after the last manual gear
extension handle is pulled:
on
tro
lle
d
if
LANDING GEAR lever . . . . . . . . . . . . . . . . DN
Landing Checklist
ENGINE START switches . . . . . . . . . . . . . . . CONT
nc
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
U
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps . . . . . . . . . . . . . . . . . . . . . ___, Green light
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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13.5
13.6
737 Flight Crew Operations Manual
LOW PRESSURE - Hydraulic Pump - System B (both)
LOSS OF SYSTEM B
FLT CONTROL
B HYD PUMPS
B
ELEC 1
LOW
PRESSURE
LOW
PRESSURE
LOW
PRESSURE
Hydraulic system B pressure is low.
or
pr
in
te
d
Condition:
ENG 2
1 System B
FLT CONTROL switch . . . . Confirm . . . .STBY RUD
3 Plan a flaps 15 landing.
4 Set VREF 15 or VREF ICE.
ad
ed
2 System B
HYD PUMP switches (both). . . . . . . . . . . . . . OFF
do
w
nl
o
Note: If any of the following conditions apply,
set VREF ICE = VREF 15 + 10 knots:
on
tro
lle
d
if
•Engine anti–ice will be used during
landing
•Wing anti–ice has been used any
time during the flight
•Icing conditions were encountered
during the flight and the landing
temperature is below 10° C.
U
nc
Note: When VREF ICE is needed, the wind
additive should not exceed 5 knots.
5 Plan to extend flaps to 15 using alternate flap
extension.
Note: The drag penalty with the leading edge
devices extended may make it impossible to
reach an alternate field.
▼ Continued on next page ▼
13.6
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September 20, 2018
13.7
737 Flight Crew Operations Manual
▼LOSS OF SYSTEM B continued▼
6 Check the Non–Normal Configuration Landing
Distance tables in the Performance Inflight-QRH
chapter or other approved source.
or
pr
in
te
d
7 Do not arm the autobrake for landing. Use manual
braking.
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on
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if
do
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ad
ed
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 15, 2016
D6-27370-8AS-NOK
13.7
13.8
737 Flight Crew Operations Manual
▼LOSS OF SYSTEM B continued▼
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if
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ad
ed
or
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Note: Inoperative Items
Autopilot B inop
Autopilot A is available.
Flight spoilers (two on each wing) inop
Roll rate and speedbrake effectiveness may be
reduced in flight.
Yaw damper inop
Trailing edge flaps normal hydraulic system
inop
The trailing edge flaps can be operated with the
alternate electrical system. Alternate flap
extension time to flaps 15 is approximately 2
minutes.
Leading edge flaps and slats normal hydraulic
system inop
The leading edge flaps and slats can be extended
with standby pressure. Once extended, they can
not be retracted.
Autobrake inop
Use manual braking.
Normal brakes inop
Alternate brakes are available.
Engine 2 thrust reverser normal hydraulic
pressure inop
Thrust reverser will deploy and retract at a slower
rate and some thrust asymmetry can be
anticipated during thrust reverser deployment.
Alternate nose wheel steering inop
Normal nose wheel steering is available.
8 Checklist Complete Except Deferred Items
▼ Continued on next page ▼
13.8
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13.9
737 Flight Crew Operations Manual
▼LOSS OF SYSTEM B continued▼
Deferred Items
Descent Checklist
Pressurization. . . . . . . . . . . . . . . . . LAND ALT ___
or
pr
in
te
d
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Landing data . . . . . . . VREF 15 or VREF ICE ___,
Minimums ___
Approach Checklist
ad
ed
Approach briefing . . . . . . . . . . . . . . . . Completed
do
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Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
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▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 15, 2016
D6-27370-8AS-NOK
13.9
13.10
737 Flight Crew Operations Manual
▼LOSS OF SYSTEM B continued▼
Alternate Flap Extension
During flap extension, set the flap lever to the
desired flap position.
or
pr
in
te
d
230K maximum during alternate flap extension.
ALTERNATE FLAPS master switch . . . . . . . ARM
Note: The landing gear configuration warning
may sound if the flaps are between 10 and
15 and the landing gear are retracted.
ad
ed
YL061 - YW351
do
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Note: The amber LE FLAPS TRANSIT light stays
illuminated until the flaps approach the
flaps 15 position.
YK820
d
if
Note: The amber LE FLAPS TRANSIT light stays
illuminated until the flaps approach the
flaps 10 position.
on
tro
lle
Note: Operation within the lower amber airspeed
band may be needed until the LE FLAPS
TRANSIT light extinguishes.
U
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▼ Continued on next page ▼
13.10
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September 30, 2022
13.11
737 Flight Crew Operations Manual
▼LOSS OF SYSTEM B continued▼
ad
ed
Additional Deferred Item
or
pr
in
te
d
If flap asymmetry occurs, release the switch
immediately. There is no asymmetry protection.
ALTERNATE FLAPS
position switch . . . . . . . . . . . . . . . Hold DOWN
to extend flaps
to 15 on schedule
As flaps are extending, slow to respective
maneuvering speed.
do
w
nl
o
GROUND PROXIMITY FLAP
INHIBIT switch . . . . . . . . . . . . . . . . FLAP INHIBIT
Landing Checklist
ENGINE START switches . . . . . . . . . . . . . . . CONT
if
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
on
tro
lle
d
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps. . . . . . . . . . . . . . . . . . . . . . 15, Green light
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■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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13.11
13.12
737 Flight Crew Operations Manual
LOW PRESSURE - Hydraulic Pump - System A and B
MANUAL REVERSION
or
LOSS OF SYSTEM A AND SYSTEM B
MANUAL REVERSION or LOSS OF SYSTEM A AND SYSTEM B
FLT CONTROL
HYD PUMPS
B
LOW
PRESSURE
LOW
PRESSURE
Condition:
ENG 1 ELEC 2
ELEC 1 ENG 2
LOW
PRESSURE
LOW
PRESSURE
or
pr
in
te
d
A
Hydraulic system A and B pressures are low.
ad
ed
1 System A and B FLT CONTROL
switches (both) . . . . . Confirm. . . . . .STBY RUD
2 YAW DAMPER switch . . . . . . . . . . . . . . . . . . . ON
do
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3 System A and B
HYD PUMPS switches (all) . . . . . . . . . . . . . . OFF
4 Plan to land at the nearest suitable airport.
5 Plan a flaps 15 landing.
if
6 Set VREF 15 or VREF ICE.
U
nc
on
tro
lle
d
Note: If any of the following conditions apply,
set VREF ICE = VREF 15 + 10 knots:
•Engine anti–ice will be used during
landing
•Wing anti–ice has been used any
time during the flight
•Icing conditions were encountered
during the flight and the landing
temperature is below 10° C.
Note: When VREF ICE is needed, the wind
additive should not exceed 5 knots.
▼ Continued on next page ▼
13.12
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D6-27370-8AS-NOK
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13.13
737 Flight Crew Operations Manual
▼MANUAL REVERSION or LOSS OF SYSTEM A AND SYSTEM B
continued▼
7 Plan to extend flaps to 15 using alternate flap
extension.
8 Plan for manual gear extension.
or
pr
in
te
d
Note: The drag penalty with the leading edge
devices extended may make it impossible to
reach an alternate field.
ad
ed
Note: When the gear has been lowered manually, it
cannot be retracted. The drag penalty with
gear extended may make it impossible to
reach an alternate field.
do
w
nl
o
9 Check the Non–Normal Configuration Landing
Distance tables in the Performance Inflight-QRH
chapter or other approved source.
Note: The crosswind capability of the airplane is
greatly reduced.
if
10 Do not arm the autobrake for landing.
d
11 Do not arm the speedbrakes for landing.
on
tro
lle
12 On touchdown, apply steady brake pressure
without modulating the brakes.
nc
13 Do not attempt to taxi the airplane after stopping.
U
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 15, 2016
D6-27370-8AS-NOK
13.13
13.14
737 Flight Crew Operations Manual
▼MANUAL REVERSION or LOSS OF SYSTEM A AND SYSTEM B
continued▼
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ad
ed
or
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in
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Note: Inoperative Items
Autopilots A and B inop
All flight spoilers inop
Roll rate will be reduced and speedbrakes will not
be available in flight.
Trailing edge flaps normal hydraulic system
inop
The trailing edge flaps can be operated with the
alternate electrical system. Alternate flap
extension time to flaps 15 is approximately 2
minutes.
Leading edge flaps and slats normal hydraulic
system inop
The leading edge flaps and slats can be extended
with standby hydraulic pressure. Once extended,
they can not be retracted.
Normal landing gear extension and retraction
inop
Manual gear extension is needed.
Autobrake inop
Ground spoilers inop
Landing distance will be increased.
Normal and alternate brakes inop
Inboard and outboard brakes have accumulator
pressure only. On landing, apply steady brake
pressure without modulating the brakes.
Both thrust reversers normal pressure inop
Thrust reversers will deploy and retract at a
slower rate.
Nose wheel steering inop
Do not attempt to taxi the airplane after stopping.
▼ Continued on next page ▼
13.14
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 31, 2023
13.15
737 Flight Crew Operations Manual
▼MANUAL REVERSION or LOSS OF SYSTEM A AND SYSTEM B
continued▼
14 Checklist Complete Except Deferred Items
Deferred Items
or
pr
in
te
d
Descent Checklist
Pressurization. . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
ad
ed
Landing data . . . . . . . VREF 15 or VREF ICE ___,
Minimums ___
do
w
nl
o
Approach briefing . . . . . . . . . . . . . . . . Completed
Go-Around Procedure Review
Do the normal go-around procedure except:
d
if
Advance thrust to go-around smoothly and
slowly to avoid excessive pitch-up.
on
tro
lle
Be prepared to trim.
Limit bank angle to 15° when airspeed is less
than the minimum maneuver speed.
U
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Approach Checklist
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 15, 2016
D6-27370-8AS-NOK
13.15
13.16
737 Flight Crew Operations Manual
▼MANUAL REVERSION or LOSS OF SYSTEM A AND SYSTEM B
continued▼
Alternate Flap Extension
or
pr
in
te
d
During flap extension, set the flap lever to the
desired flap position.
230K maximum during alternate flap extension.
ALTERNATE FLAPS master switch . . . . . . . ARM
ad
ed
Note: The landing gear configuration warning
may sound if the flaps are between 10 and
15 and the landing gear are retracted.
YL061 - YW351
do
w
nl
o
Note: The amber LE FLAPS TRANSIT light stays
illuminated until the flaps approach the
flaps 15 position.
YK820
on
tro
lle
d
if
Note: The amber LE FLAPS TRANSIT light stays
illuminated until the flaps approach the
flaps 10 position.
▼ Continued on next page ▼
U
nc
Note: Operation within the lower amber airspeed
band may be needed until the LE FLAPS
TRANSIT light extinguishes.
13.16
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
September 30, 2022
13.17
737 Flight Crew Operations Manual
▼MANUAL REVERSION or LOSS OF SYSTEM A AND SYSTEM B
continued▼
ad
ed
Manual Gear Extension
or
pr
in
te
d
If flap asymmetry occurs, release the switch
immediately. There is no asymmetry protection.
ALTERNATE FLAPS
position switch . . . . . . . . . . . . . . . Hold DOWN
to extend flaps
to 15 on schedule
As flaps are extending, slow to respective
maneuvering speed.
LANDING GEAR lever. . . . . . . . . . . . . . . . . . . OFF
do
w
nl
o
Manual gear extension handles. . . . . . . . . . . . Pull
The uplock is released when the handle is pulled
to its limit.
if
The related red landing gear indicator light
illuminates, indicating uplock release.
on
tro
lle
d
Wait 15 seconds after the last manual gear
extension handle is pulled:
LANDING GEAR lever . . . . . . . . . . . . . . . . DN
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Additional Deferred Item
GROUND PROXIMITY FLAP
INHIBIT switch . . . . . . . . . . . . . . . . FLAP INHIBIT
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 15, 2016
D6-27370-8AS-NOK
13.17
13.18
737 Flight Crew Operations Manual
▼MANUAL REVERSION or LOSS OF SYSTEM A AND SYSTEM B
continued▼
Landing Checklist
ENGINE START switches. . . . . . . . . . . . . . . . CONT
or
pr
in
te
d
Speedbrake . . . . . . . . . . . . . . . . . . DOWN detent
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps . . . . . . . . . . . . . . . . . . . . . . 15, Green light
■■■■
LOW PRESSURE - Hydraulic Pump - Standby
The standby hydraulic pump pressure is low.
do
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o
Condition:
STANDBY HYDRAULIC LOW
PRESSURE
ad
ed
LOW
PRESSURE
if
Note: With a loss of hydraulic system A or B, the
thrust reverser on the affected side is
inoperative.
LOW QUANTITY
on
tro
lle
d
Note: With a loss of hydraulic system A and B, the
rudder is inoperative.
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LOW
QUANTITY
Condition:
■■■■
STANDBY HYDRAULIC LOW
QUANTITY
The standby hydraulic quantity is low.
1 Continue normal operation.
■■■■
13.18
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 3, 2022
14 Landing Gear (tab)
NNC.14-Landing
Gear
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Landing Gear
Section 14
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Table of Contents
ANTISKID INOPERATIVE ................................. 14.1
AUTO BRAKE DISARM ..................................... 14.3
Brake Pressure Indicator Zero PSI .................... 14.5
GEAR DISAGREE ............................................ 14.6
Landing Gear Lever Jammed in the Up Position 14.10
Landing Gear Lever Will Not Move Up After Takeoff...
14.14
Manual Gear Extension ................................. 14.18
Partial or All Gear Up Landing ........................ 14.20
WHEEL WELL FIRE.............................................. ►►8.26
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March 31, 2023
2
D6-27370-8AS-NOK
14.TOC.1
Non-Normal Checklists Landing Gear
737 Flight Crew Operations Manual
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Table of Contents
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Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
14.TOC.2
D6-27370-8AS-NOK
March 31, 2023
14.1
737 Flight Crew Operations Manual
Landing
File
ANTISKID
Highlight
Gear
INOP
ANTISKID
INOP
Condition:
ANTISKID INOPERATIVE
An antiskid system fault occurs.
or
pr
in
te
d
Caution! Locked wheel protection is not
available.
1 AUTO BRAKE select switch. . . . . . . . . . . . . . OFF
The autobrake system is inoperative.
2 Do not arm the speedbrakes for landing. Manually
deploy the speedbrakes immediately upon landing.
ad
ed
Automatic speedbrake extension may be
inoperative.
do
w
nl
o
3 Check the Non–Normal Configuration Landing
Distance tables in the Performance Inflight-QRH
chapter or other approved source.
4 Checklist Complete Except Deferred Items
if
Deferred Items
on
tro
lle
d
Landing Procedure Review
Use minimum braking consistent with runway length
and conditions to reduce the possibility of a tire
blowout.
U
nc
Do not apply the brakes until the nose wheel is on
the ground and the speedbrakes have been manually
deployed.
Brake initially using light steady pedal pressure.
Increase pressure as ground speed decreases. Do
not pump the brakes.
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 15, 2016
D6-27370-8AS-NOK
14.1
14.2
737 Flight Crew Operations Manual
▼ANTISKID INOPERATIVE continued▼
Descent Checklist
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
or
pr
in
te
d
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
Landing data . . . . . . . . . VREF ___, Minimums ___
Approach briefing . . . . . . . . . . . . . . . . Completed
ad
ed
Approach Checklist
do
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Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing Checklist
ENGINE START switches. . . . . . . . . . . . . . . . CONT
if
Speedbrake . . . . . . . . . . . . . . . . . . DOWN detent
d
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
■■■■
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Flaps . . . . . . . . . . . . . . . . . . . . . ___, Green light
14.2
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 26, 2015
14.3
737 Flight Crew Operations Manual
AUTO BRAKE DISARM
AUTO BRAKE
DISARM
Condition:
AUTO BRAKE DISARM
The autobrake system disarms after being
set.
On the ground:
or
pr
in
te
d
1 Choose one:
AUTO BRAKE select switch . . . . . . . . OFF
►►Go to step 2
In flight:
ad
ed
►►Go to step 3
2 Choose one:
do
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AUTO BRAKE DISARM light extinguishes:
■■■■
AUTO BRAKE DISARM light stays illuminated:
on
tro
lle
d
if
Do not takeoff.
■■■■
3 AUTO BRAKE select switch. . . . OFF, then reselect
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▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 26, 2015
D6-27370-8AS-NOK
14.3
14.4
737 Flight Crew Operations Manual
▼AUTO BRAKE DISARM continued▼
4 Choose one:
AUTO BRAKE DISARM light stays extinguished:
■■■■
or
pr
in
te
d
AUTO BRAKE DISARM light illuminates again:
AUTO BRAKE select switch . . . . . . . . OFF
Use manual brakes for landing.
►►Go to step 5
ad
ed
5 Checklist Complete Except Deferred Items
Deferred Items
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Descent Checklist
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
if
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
on
tro
lle
d
Landing data . . . . . . . . . VREF ___, Minimums ___
Approach briefing . . . . . . . . . . . . . . . . Completed
nc
Approach Checklist
U
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Landing Checklist
ENGINE START switches. . . . . . . . . . . . . . . . CONT
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
▼ Continued on next page ▼
14.4
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 26, 2015
14.5
737 Flight Crew Operations Manual
▼AUTO BRAKE DISARM continued▼
Landing gear . . . . . . . . . . . . . . . . . . . . . . . Down
Flaps . . . . . . . . . . . . . . . . . . . . . ___, Green light
or
pr
in
te
d
■■■■
Brake Pressure Indicator Zero PSI
Condition:
The brake accumulator has no nitrogen
precharge.
1 Accumulator braking is not available.
ad
ed
Note: If hydraulic systems indications are normal,
brake operation is unaffected.
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lle
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if
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■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 26, 2015
D6-27370-8AS-NOK
14.5
14.6
737 Flight Crew Operations Manual
LEFT GEAR
NOSE
RIGHT
GEAR
GEAR
GEAR DISAGREE
NOSE
GEAR
Condition:
RIGHT
GEAR
The landing gear position disagrees with the
LANDING GEAR lever position.
or
pr
in
te
d
LEFT
GEAR
Note: Do not exceed the gear EXTEND limit speed
(270K/.82M).
1 Choose one:
ad
ed
Do not use FMC performance predictions with
gear extended.
LANDING GEAR lever is UP:
do
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►►Go to step 5
LANDING GEAR lever is OFF:
►►Go to step 2
if
LANDING GEAR lever is DN:
on
tro
lle
d
►►Go to step 9
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▼ Continued on next page ▼
14.6
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
September 20, 2018
14.7
737 Flight Crew Operations Manual
▼GEAR DISAGREE continued▼
2 Choose one:
LANDING GEAR lever moved to the UP position
after takeoff:
or
pr
in
te
d
►►Go to step 3
LANDING GEAR lever did not move to the UP
position after takeoff:
►►Go to the Landing Gear Lever Will
Not Move Up After Takeoff checklist
on page 14.14
3
do
w
nl
o
235K maximum
ad
ed
■■■■
LANDING GEAR lever. . . . . . . . . . . . . . . . . UP
4 Choose one:
d
if
All red and green landing gear indicator lights
are extinguished:
■■■■
U
nc
on
tro
lle
The landing gear lever should be kept in the
UP position to keep the landing gear
retracted.
Any red landing gear indicator light is
illuminated:
►►Go to step 8
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 21, 2019
D6-27370-8AS-NOK
14.7
14.8
737 Flight Crew Operations Manual
▼GEAR DISAGREE continued▼
5 Choose one:
All red and green landing gear indicator lights
are illuminated:
or
pr
in
te
d
Open and close the manual gear extension
access door. Verify the door is fully closed.
►►Go to step 6
►►Go to step 8
6
do
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o
235K maximum
ad
ed
Any other combination of landing gear
indicator lights is illuminated:
LANDING GEAR lever . . . . . . . . . . DN, then UP
7 Choose one:
All landing gear indicator lights extinguish:
on
tro
lle
d
if
LANDING GEAR lever . . . . . . . . . . . . OFF
■■■■
Any red landing gear indicator light is
illuminated:
nc
►►Go to step 8
U
8 Flight with gear down increases fuel consumption
and decreases climb performance. Refer to the
Gear Down performance tables in the Performance
Inflight section.
■■■■
▼ Continued on next page ▼
14.8
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September 15, 2016
14.9
737 Flight Crew Operations Manual
▼GEAR DISAGREE continued▼
9 Check landing gear indicator lights.
10 Choose one:
or
pr
in
te
d
Note: If a green landing gear indicator light is
illuminated on either the center main panel
or the overhead panel, the related landing
gear is down and locked.
All landing gear indicate down and locked and
one or more red landing gear indicator lights are
also illuminated:
ad
ed
►►Go to step 11
Any landing gear is not down and locked:
do
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►►Go to the Manual Gear Extension
checklist on page 14.18
■■■■
d
if
11 Verify landing gear lever is pushed in and fully in
the DN detent.
on
tro
lle
12 Choose one:
All red landing gear indicator lights extinguish:
■■■■
U
nc
One or more red landing gear indicator lights
stay illuminated:
GROUND PROXIMITY GEAR
INHIBIT switch . . . . . . . . . GEAR INHIBIT
Land normally.
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
May 16, 2019
D6-27370-8AS-NOK
14.9
14.10
737 Flight Crew Operations Manual
Landing Gear Lever Jammed
in the Up Position
Condition:
The LANDING GEAR lever will not move from
the UP position.
or
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in
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Note: Start this checklist only when ready to
extend the gear for landing.
Once the gear is extended, do not retract.
270K/.82M maximum.
1
ad
ed
LANDING GEAR override trigger . . . . . . . . Pull
2 LANDING GEAR lever . . . . . . . . . . . . . . . . . . DN
do
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3 Choose one:
LANDING GEAR lever moves to the DN position:
►►Go to step 4
d
if
LANDING GEAR lever does not move to the DN
position:
on
tro
lle
►►Go to step 6
4 Check landing gear indicator lights.
U
nc
Note: If a green landing gear indicator light is
illuminated on either the center main panel
or the overhead panel, the related landing
gear is down and locked.
▼ Continued on next page ▼
14.10
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 21, 2019
14.11
737 Flight Crew Operations Manual
▼Landing Gear Lever Jammed in the Up Position continued▼
5 Choose one:
All landing gear indicate down and locked:
■■■■
or
pr
in
te
d
Plan to land at the nearest suitable airport.
One or more landing gear do not indicate down
and locked:
►►Go to the Manual Gear Extension
checklist on page 14.18
ad
ed
■■■■
do
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6 NOSE WHEEL
STEERING switch . . . . . . . . . . . . . . Verify NORM
Nose wheel steering is not available.
on
tro
lle
d
if
Warning! Do not use alternate nose wheel
steering because the landing gear may
retract on the ground.
U
nc
7
270K/.82M maximum.
Manual gear
extension handles (all) . . . . . . . . . . . . . . Pull
The uplock is released when the handle is pulled
to its limit. The related red landing gear
indicator light illuminates, indicating uplock
released.
Note: With the LANDING GEAR lever in the UP or
OFF position, the red landing gear indicator
lights will stay illuminated.
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 21, 2019
D6-27370-8AS-NOK
14.11
14.12
737 Flight Crew Operations Manual
▼Landing Gear Lever Jammed in the Up Position continued▼
8 Check landing gear indicator lights.
or
pr
in
te
d
Note: If a green landing gear indicator light is
illuminated on either the center main panel
or the overhead panel, the related landing
gear is down and locked.
9 Choose one:
All landing gear indicate down and locked:
►►Go to step 10
ad
ed
One or more landing gear do not indicate down
and locked:
do
w
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►►Go to the Partial or All Gear Up
Landing checklist on page 14.20
■■■■
10 Checklist Complete Except Deferred Items
d
if
Deferred Items
on
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Descent Checklist
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
nc
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . ___
U
Landing data . . . . . . . . . VREF ___, Minimums ___
Approach briefing . . . . . . . . . . . . . . . . Completed
▼ Continued on next page ▼
14.12
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14.13
737 Flight Crew Operations Manual
▼Landing Gear Lever Jammed in the Up Position continued▼
Approach Checklist
Additional Deferred Item
or
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Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
GROUND PROXIMITY GEAR
INHIBIT switch . . . . . . . . . . . . . . . . GEAR INHIBIT
ad
ed
Landing Checklist
ENGINE START switches . . . . . . . . . . . . . . . CONT
do
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Speedbrake . . . . . . . . . . . . . . . . . . . . . . . ARMED
Landing gear . . . . . . . . . . . . Down, Three green
Flaps . . . . . . . . . . . . . . . . . . . . . ___, Green light
if
Note: Nose wheel steering is not available.
■■■■
U
nc
on
tro
lle
d
Warning! Do not use alternate nose wheel
steering because the landing gear may
retract on the ground.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 21, 2019
D6-27370-8AS-NOK
14.13
14.14
737 Flight Crew Operations Manual
Landing Gear Lever Will Not
Move Up After Takeoff
The LANDING GEAR lever cannot be moved
to the UP position due to one of the
following:
•Failure of the landing gear lever lock
solenoid
•Failure of the air/ground system
•Failure of the ground spoiler interlock
valve to close.
or
pr
in
te
d
Condition:
ad
ed
Note: Do not use FMC performance predictions.
1 LANDING GEAR lever . . . . . . . . . . . . . . . . . . DN
do
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o
2 Retract the flaps on schedule.
U
nc
on
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lle
d
if
▼ Continued on next page ▼
14.14
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 21, 2019
14.15
737 Flight Crew Operations Manual
▼Landing Gear Lever Will Not Move Up After Takeoff continued▼
3 Choose one:
or
pr
in
te
d
Intermittent cabin altitude/configuration warning
horn stays silent and the TAKEOFF CONFIG
lights (if installed and operative) do not
illuminate after the flaps are fully retracted and
the thrust levers are advanced beyond the
vertical position:
Note: This indicates a failure of the landing
gear lever lock solenoid.
ad
ed
►►Go to step 4
do
w
nl
o
Intermittent cabin altitude/configuration warning
horn sounds or the TAKEOFF CONFIG lights (if
installed and operative) illuminate when the
flaps are fully retracted:
on
tro
lle
d
if
Note: This indicates either a failure of the
air/ground system or a failure of the
ground spoiler interlock valve to
close.
Do not retract the gear.
nc
►►Go to step 7
U
4
235K maximum.
LANDING GEAR override trigger . . . . . . . . Pull
5 LANDING GEAR lever . . . . . . . . . . . . . . . . . . UP
After landing gear retraction is complete:
LANDING GEAR lever . . . . . . . . . . . OFF
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 21, 2019
D6-27370-8AS-NOK
14.15
14.16
737 Flight Crew Operations Manual
▼Landing Gear Lever Will Not Move Up After Takeoff continued▼
6 Continue normal operation.
■■■■
or
pr
in
te
d
7 LANDING GEAR
TAKEOFF WARNING CUTOFF
circuit breaker (P6–3:C18) . . . . . . . . . . . . . Pull
ad
ed
Note: The intermittent cabin altitude/configuration
warning horn may still sound and the
TAKEOFF CONFIG lights (if installed and
operative) may still illuminate depending on
thrust lever and flap position.
do
w
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o
Caution! Do not use the speedbrakes in flight.
8 Plan to land at the nearest suitable airport.
9 Do not arm the autobrake for landing. Use manual
braking.
d
if
10 Do not arm the speedbrakes for landing. Manually
deploy the speedbrakes immediately upon landing.
on
tro
lle
11 Checklist Complete Except Deferred Items
Deferred Items
nc
Descent Checklist
U
Pressurization . . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
Landing data . . . . . . . . . VREF ___, Minimums ___
Approach briefing . . . . . . . . . . . . . . . . Completed
▼ Continued on next page ▼
14.16
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
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14.17
737 Flight Crew Operations Manual
▼Landing Gear Lever Will Not Move Up After Takeoff continued▼
Approach Checklist
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
or
pr
in
te
d
Gear Down Verification
LANDING GEAR lever. . . . . . . . . . . . . . . Verify DN
Landing Checklist
ad
ed
ENGINE START switches . . . . . . . . . . . . . . . CONT
Speedbrake . . . . . . . . . . . . . . . . . . DOWN detent
do
w
nl
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Landing gear . . . . . . Down (previously verified)
Flaps . . . . . . . . . . . . . . . . . . . . . ___, Green light
■■■■
U
nc
on
tro
lle
d
if
Note: Manually deploy the speedbrakes
immediately upon touchdown. Use manual
braking.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 21, 2019
D6-27370-8AS-NOK
14.17
14.18
737 Flight Crew Operations Manual
Manual Gear Extension
One of these occurs:
•Any landing gear is not down and locked
when the LANDING GEAR lever is down
•The LANDING GEAR lever is jammed in the
OFF position.
or
pr
in
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d
Condition:
Note: If a green landing gear indicator light is
illuminated on either the center main panel
or the overhead panel, the related landing
gear is down and locked.
ad
ed
1 LANDING GEAR lever . . . . . . . . OFF (if possible)
270K/.82M maximum.
Manual gear
extension handles (affected gear) . . . . . . . Pull
The uplock is released when the handle is pulled
to its limit. The related red landing gear
indicator light illuminates, indicating uplock
released.
if
do
w
nl
o
2
on
tro
lle
d
3 Wait 15 seconds after the last manual gear
extension handle is pulled:
LANDING GEAR lever . . . . . . . DN (if possible)
nc
4 Check landing gear indicator lights.
U
Note: If the LANDING GEAR lever is in the OFF
position, the red landing gear indicator lights
will also be illuminated.
▼ Continued on next page ▼
14.18
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14.19
737 Flight Crew Operations Manual
▼Manual Gear Extension continued▼
5 Choose one:
All landing gear indicate down and locked:
►►Go to step 6
or
pr
in
te
d
One or more landing gear do not indicate down
and locked:
►►Go to the Partial or All Gear Up
Landing checklist on page 14.20
6 Choose one:
ad
ed
■■■■
LANDING GEAR lever is in the DN position:
do
w
nl
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Land normally.
■■■■
LANDING GEAR lever is in the OFF position:
on
tro
lle
d
if
GROUND PROXIMITY GEAR
INHIBIT switch . . . . . . . . . GEAR INHIBIT
Land normally.
Note: Nose wheel steering is not available.
U
nc
■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 21, 2019
D6-27370-8AS-NOK
14.19
14.20
737 Flight Crew Operations Manual
Partial or All Gear Up Landing
Condition:
All landing gear are not down and locked
after attempting manual gear extension.
1 Choose one:
or
pr
in
te
d
Manual gear extension has been attempted:
►►Go to step 2
Manual gear extension has not been attempted:
►►Go to the Manual Gear Extension
checklist on page 14.18
ad
ed
■■■■
do
w
nl
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2 Brief the crew and passengers on emergency
landing and evacuation procedures.
3 Consider burning off fuel to reduce touchdown
speed.
if
4 Plan a flaps 40 landing.
on
tro
lle
d
5 Set VREF 40.
6 LANDING GEAR
AURAL WARN circuit breaker (P6-3:D18) . . . . Pull
U
nc
This prevents the landing gear warning horn
with gear retracted and landing flaps selected.
The flight deck chime for an incoming call from
the cabin crew is unavailable.
▼ Continued on next page ▼
14.20
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14.21
737 Flight Crew Operations Manual
▼Partial or All Gear Up Landing continued▼
7 FLIGHT CONTROL
AUTO SPEED BRAKE
circuit breaker (P6-2:B9). . . . . . . . . . . . . . . Pull
or
pr
in
te
d
This prevents inadvertent deployment of ground
spoilers after landing.
8 Do not arm the autobrake for landing. Use manual
braking.
9 Do not arm the speedbrakes for landing.
ad
ed
10 Checklist Complete Except Deferred Items
Deferred Items
do
w
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o
Descent Checklist
Pressurization. . . . . . . . . . . . . . . . . LAND ALT ___
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
d
if
Landing data . . . . . VREF 40___, Minimums ___
on
tro
lle
Approach briefing . . . . . . . . . . . . . . . . Completed
Approach Checklist
U
nc
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . ___
▼ Continued on next page ▼
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 21, 2019
D6-27370-8AS-NOK
14.21
14.22
737 Flight Crew Operations Manual
▼Partial or All Gear Up Landing continued▼
Landing Procedure Review
or
pr
in
te
d
Do not extend the speedbrakes unless stopping
distance is critical. When stopping distance is critical,
extend the speedbrakes after all landing gear, the
nose or the engine nacelle have contacted the
runway.
Do not use the thrust reversers unless stopping
distance is critical.
ad
ed
Turn all fuel pump switches OFF just before the flare.
do
w
nl
o
After stopping, do the Evacuation checklist, if
needed.
Additional Deferred Items
APU switch . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
d
if
GROUND PROXIMITY GEAR
INHIBIT switch . . . . . . . . . . . . . . . . GEAR INHIBIT
on
tro
lle
When on approach:
This ensures the airplane is depressurized
at touchdown.
U
nc
Engine BLEED air switches. . . . . . . . . . . . OFF
Landing Checklist
ENGINE START switches. . . . . . . . . . . . . . . . CONT
Speedbrake . . . . . . . . . . . . . . . . . . DOWN detent
Landing gear . . . . . . . . . . . . . . . . . . . ___ Down
▼ Continued on next page ▼
14.22
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D6-27370-8AS-NOK
March 21, 2019
14.23
737 Flight Crew Operations Manual
▼Partial or All Gear Up Landing continued▼
Flaps. . . . . . . . . . . . . . . . . . . . . . 40, Green light
■■■■
U
nc
on
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d
if
do
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ad
ed
or
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WHEEL WELL FIRE ►►8.26
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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D6-27370-8AS-NOK
14.23
14.24
do
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ad
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737 Flight Crew Operations Manual
U
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on
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Intentionally
Blank
14.24
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
D6-27370-8AS-NOK
March 21, 2019
15 Warning Systems
NNC.15-Warning
Systems
(tab)
Table Of Contents
737 Flight Crew Operations Manual
Non-Normal Checklists
Chapter NNC
Warning Systems
Section 15
or
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Table of Contents
LANDING CONFIGURATION......................... 15.1
TAKEOFF CONFIGURATION ......................... 15.1
WARNING HORN (INTERMITTENT) ............. 15.2
WARNING LIGHT - CABIN ALTITUDE OR
TAKEOFF CONFIGURATION ...................... 15.2
NNC. 3
U
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on
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do
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ad
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GROUND PROXIMITY GPWS INOPERATIVE .........15.3
LANDING CONFIGURATION......................... 15.1
Overspeed .................................................... 15.3
PSEU ............................................................15.4
Tail Strike ..................................................... 15.5
TAKEOFF CONFIGURATION ......................... 15.1
WARNING HORN (INTERMITTENT) ............. 15.2
WARNING LIGHT - CABIN ALTITUDE OR
TAKEOFF CONFIGURATION ...................... 15.2
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 31, 2023
2
D6-27370-8AS-NOK
15.TOC.1
Non-Normal Checklists Warning Systems
737 Flight Crew Operations Manual
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Table of Contents
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Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
15.TOC.2
D6-27370-8AS-NOK
March 31, 2023
15.1
737 Flight Crew Operations Manual
Warning
File
Highlight
Systems
LANDING CONFIGURATION
Condition:
In flight, the steady warning horn sounds.
1 Assure correct airplane landing configuration.
TAKEOFF CONFIG
or
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in
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----------------------■■■■
TAKEOFF CONFIGURATION
On the ground, the intermittent cabin
altitude/configuration warning horn sounds
or a TAKEOFF CONFIG light (if installed and
operative) illuminates when advancing the
thrust levers to takeoff thrust.
do
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o
Condition:
(If installed and operative)
ad
ed
TAKEOFF
CONFIG
1 Assure correct airplane takeoff configuration.
U
nc
on
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if
----------------------■■■■
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
March 26, 2015
D6-27370-8AS-NOK
15.1
15.2
737 Flight Crew Operations Manual
WARNING HORN (INTERMITTENT)
or
WARNING LIGHT - CABIN ALTITUDE
OR TAKEOFF CONFIGURATION
Left Forward Panel
TAKEOFF
CONFIG
Right Forward Panel
CABIN
ALTITUDE
CABIN
ALTITUDE
TAKEOFF
CONFIG
One of these occurs:
•In flight, at an airplane flight altitude
above 10,000 feet MSL, the intermittent
warning horn sounds or a CABIN
ALTITUDE light (if installed and operative)
illuminates
•On the ground, the intermittent warning
horn sounds or a TAKEOFF CONFIG light
(if installed and operative) illuminates
when advancing the thrust levers to
takeoff thrust.
if
do
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ad
ed
Condition:
or
pr
in
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(If installed and operative)
on
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d
1 If the intermittent warning horn sounds or a CABIN
ALTITUDE light (if installed and operative)
illuminates in flight at an airplane flight altitude
above 10,000 feet MSL:
U
nc
Don the oxygen masks and set the regulators to
100%.
Establish crew communications.
►►Go to the CABIN ALTITUDE WARNING
or Rapid Depressurization checklist on
page 2.1
■■■■
▼ Continued on next page ▼
15.2
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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15.3
737 Flight Crew Operations Manual
▼WARNING HORN (INTERMITTENT) continued▼
2 If the intermittent warning horn sounds or a
TAKEOFF CONFIG light (if installed and operative)
illuminates on the ground when advancing the
thrust levers to takeoff thrust:
or
pr
in
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Assure correct airplane takeoff configuration.
----------------------■■■■
INOP - Ground Proximity
GROUND PROXIMITY
GPWS INOPERATIVE
A ground proximity warning system (GPWS)
fault occurs.
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Condition:
ad
ed
INOP
Note: Some or all GPWS alerts are not available.
GPWS alerts which occur are valid.
on
tro
lle
d
if
■■■■
Airspeed is more than Vmo/Mmo.
■■■■
U
nc
Condition:
Overspeed
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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D6-27370-8AS-NOK
15.3
15.4
737 Flight Crew Operations Manual
PSEU
PSEU
PSEU
Condition:
A proximity switch electronics unit fault
occurs.
or
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in
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Note: The PSEU light illuminates on the ground
only.
1 Choose one:
PSEU light stays illuminated when the Master
Caution system is reset:
ad
ed
►►Go to step 2
PSEU light extinguishes when the Master
Caution system is reset:
do
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■■■■
2 Choose one:
if
PSEU light stays illuminated when the parking
brake is set or when both engines are shut down:
on
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d
Do not takeoff.
■■■■
■■■■
U
nc
PSEU light extinguishes when the parking brake
is set or when both engines are shut down:
15.4
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September 20, 2018
15.5
737 Flight Crew Operations Manual
Tail Strike
Condition:
A tail strike is suspected or confirmed.
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Caution! Continued pressurization of the
airplane can cause further structural
damage.
1 Pressurization mode selector . . . . . . . . . . . . MAN
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Use momentary actuation of the outflow valve
switch to avoid large and rapid pressurization
changes.
Outflow
VALVE switch . . . . . Move to OPEN until
2
the outflow VALVE
indication shows fully open
to depressurize the airplane
3 Plan to land at the nearest suitable airport.
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15.6
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15.6
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Operational Information (tab)
Table Of Contents
Operational Information
737 Flight Crew Operations Manual
Operational Information
Chapter OI
Table of Contents
Section TOC
Ops Info . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OI.1
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Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OI.1.1
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OI.TOC.1
Operational Information Table of Contents
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OI.TOC.2
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737 Flight Crew Operations Manual
Operational Information
Chapter OI
Ops Info
Section 1
Ops Highlight
File
Info
Introduction
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Note: This section is reserved for operator-developed information.
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OI.1.1
Operational Information Ops Info
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OI.1.2
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Section TableInflight
Performance
of Contents
- QRH (tab)
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Table of Contents
Section TOC
737-800W CFM56-7B24 KG JAA
CATC/N TALPA - - - - - - - - - - - - - - - - - - - - - PI-QRH.10.1
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737-800WSFP1 CFM56-7B24 C KG M FAA CATC/N TALPA
(FMC Model 737-800W.1) - - - - - - - - - - - - - - PI-QRH.20.1
737-800WSFP1 CFM56-7B26 C M KG FAA CATC/N TALPA
(FMC Model 737-800W.1) - - - - - - - - - - - - - - PI-QRH.30.1
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737-800WSFP1 CFM56-7B26 C M KG JAA CATC/N TALPA
(FMC Model 737-800W.1) - - - - - - - - - - - - - - PI-QRH.40.1
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Performance Inflight - QRH Table of Contents
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737-800W
Section
737-800W
CFM56-7B24
CFM56-7B24
KG JAAKG
CATC/N
JAA CATC/N
TALPA TALPA
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Table of Contents
Section 10
737-800W CFM56-7B24 KG JAA CATC/N TALPA
Pkg Model Identification . . . . . . . . . . . . . . . . . . . PI-QRH.ModID.10.1
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General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.10.1
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Flight With Unreliable Airspeed/
Turbulent Air Penetration . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.10.1
CLIMB (280/.76) . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.10.1
CRUISE (.76/280) . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.10.1
DESCENT (.76/280) . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.10.2
HOLDING (VREF40 + 70). . . . . . . . . . . . . . . . . . . PI-QRH.10.2
TERMINAL AREA (5000 FT) . . . . . . . . . . . . . . . . PI-QRH.10.3
Airport Altitude = -2000 FT . . . . . . . . . . . . . . . . PI-QRH.10.3
Airport Altitude = -1000 FT . . . . . . . . . . . . . . . . PI-QRH.10.4
Airport Altitude = SEA LEVEL . . . . . . . . . . . . . PI-QRH.10.5
Airport Altitude = 1000 FT . . . . . . . . . . . . . . . . PI-QRH.10.6
Airport Altitude = 2000 FT . . . . . . . . . . . . . . . . PI-QRH.10.7
Airport Altitude = 3000 FT . . . . . . . . . . . . . . . . PI-QRH.10.8
Airport Altitude = 4000 FT . . . . . . . . . . . . . . . . PI-QRH.10.9
Airport Altitude = 5000 FT . . . . . . . . . . . . . . . PI-QRH.10.10
Airport Altitude = 6000 FT . . . . . . . . . . . . . . . .PI-QRH.10.11
Airport Altitude = 7000 FT . . . . . . . . . . . . . . . PI-QRH.10.12
Airport Altitude = 8000 FT . . . . . . . . . . . . . . . PI-QRH.10.13
Airport Altitude = 9000 FT . . . . . . . . . . . . . . . PI-QRH.10.14
Airport Altitude = 10000 FT . . . . . . . . . . . . . . PI-QRH.10.15
Airport Altitude = 11000 FT. . . . . . . . . . . . . . . PI-QRH.10.16
Airport Altitude = 12000 FT . . . . . . . . . . . . . . PI-QRH.10.17
Airport Altitude = 13000 FT . . . . . . . . . . . . . . PI-QRH.10.18
Airport Altitude = 14000 FT . . . . . . . . . . . . . . PI-QRH.10.19
Airport Altitude = 14500 FT . . . . . . . . . . . . . . PI-QRH.10.20
FINAL APPROACH (1500 FT) . . . . . . . . . . . . . . PI-QRH.10.21
Airport Altitude = -2000 FT . . . . . . . . . . . . . . . PI-QRH.10.21
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Performance Inflight - QRH Table of Contents
737 Flight Crew Operations Manual
PI-QRH.10.21
PI-QRH.10.22
PI-QRH.10.22
PI-QRH.10.23
PI-QRH.10.23
PI-QRH.10.24
PI-QRH.10.24
PI-QRH.10.25
PI-QRH.10.25
PI-QRH.10.26
PI-QRH.10.26
PI-QRH.10.27
PI-QRH.10.27
PI-QRH.10.28
PI-QRH.10.28
PI-QRH.10.29
PI-QRH.10.29
PI-QRH.10.30
PI-QRH.10.31
PI-QRH.10.32
PI-QRH.10.33
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Airport Altitude = -1000 FT . . . . . . . . . . . . . . .
Airport Altitude = SEA LEVEL . . . . . . . . . . . .
Airport Altitude = 1000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 2000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 3000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 4000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 5000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 6000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 7000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 8000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 9000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 10000 FT. . . . . . . . . . . . . . .
Airport Altitude = 11000 FT. . . . . . . . . . . . . . .
Airport Altitude = 12000 FT. . . . . . . . . . . . . . .
Airport Altitude = 13000 FT. . . . . . . . . . . . . . .
Airport Altitude = 14000 FT. . . . . . . . . . . . . . .
Airport Altitude = 14500 FT. . . . . . . . . . . . . . .
GO-AROUND . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Max Climb %N1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Go-around %N1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
VREF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Advisory Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.11.1
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Runway Surface Condition Correlation . . . . . . . . . . . . PI-QRH.11.1
Normal Configuration Landing Distance . . . . . . . . . . . PI-QRH.11.2
Non-Normal Configuration Landing Distance . . . . . . . PI-QRH.11.6
Airspeed Unreliable (Flaps 15) . . . . . . . . . . . . . . . . PI-QRH.11.6
Airspeed Unreliable (Flaps 30) . . . . . . . . . . . . . . . . PI-QRH.11.7
Airspeed Unreliable (Flaps 40) . . . . . . . . . . . . . . . . PI-QRH.11.8
All Flaps Up Landing. . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.11.9
ANTISKID INOPERATIVE (Flaps 15) . . . . . . . . PI-QRH.11.10
ANTISKID INOPERATIVE (Flaps 30) . . . . . . . . PI-QRH.11.11
ANTISKID INOPERATIVE (Flaps 40) . . . . . . . . PI-QRH.11.12
Jammed or Restricted Flight Controls (Flaps 15) . PI-QRH.11.13
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LEADING EDGE FLAPS TRANSIT (Flaps 15) . .PI-QRH.11.14
LOSS OF SYSTEM A (Flaps 15) . . . . . . . . . . . . . .PI-QRH.11.15
LOSS OF SYSTEM A (Flaps 30) . . . . . . . . . . . . . .PI-QRH.11.16
LOSS OF SYSTEM A (Flaps 40) . . . . . . . . . . . . . .PI-QRH.11.17
LOSS OF SYSTEM A AND SYSTEM B
(Flaps 15). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.11.18
LOSS OF SYSTEM B (Flaps 15) . . . . . . . . . . . . . .PI-QRH.11.19
MANUAL REVERSION (Flaps 15). . . . . . . . . . . .PI-QRH.11.20
One Engine Inoperative Landing (Flaps 15) . . . . . .PI-QRH.11.21
One Engine Inoperative Landing (Flaps 30) . . . . . .PI-QRH.11.22
Stabilizer Trim Inoperative (Flaps 15) . . . . . . . . . .PI-QRH.11.23
Trailing Edge Flap Asymmetry (1 ≤ Flap
Lever <15) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.11.24
Trailing Edge Flap Asymmetry (Flap Lever
15 or 25) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.11.25
Trailing Edge Flap Asymmetry (Flap Lever 30) . . .PI-QRH.11.26
Trailing Edge Flap Disagree (1 ≤ Indicated
Flaps <15) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.11.27
Trailing Edge Flap Disagree (15 ≤ Indicated
Flaps <30) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.11.28
Trailing Edge Flap Disagree (30 ≤ Indicated
Flaps <40) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.11.29
Trailing Edge Flaps Up Landing . . . . . . . . . . . . . . .PI-QRH.11.30
Recommended Brake Cooling Schedule . . . . . . . . . . .PI-QRH.11.31
Engine Inoperative . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.12.1
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Initial Max Continuous %N1 . . . . . . . . . . . . . . . . . . . . PI-QRH.12.1
Max Continuous %N1 . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.12.2
Driftdown Speed/Level Off Altitude . . . . . . . . . . . . . . PI-QRH.12.6
Driftdown/LRC Cruise Range Capability . . . . . . . . . . PI-QRH.12.7
Long Range Cruise Altitude Capability . . . . . . . . . . . . PI-QRH.12.8
Long Range Cruise Control . . . . . . . . . . . . . . . . . . . . . PI-QRH.12.9
Long Range Cruise Diversion Fuel and Time . . . . . . PI-QRH.12.10
Holding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.12.11
Gear Down Landing Rate of Climb Available . . . . . . PI-QRH.12.12
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PI-QRH.TOC.10.3
Performance Inflight - QRH Table of Contents
737 Flight Crew Operations Manual
Gear Down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.13.1
PI-QRH.13.1
PI-QRH.13.2
PI-QRH.13.3
PI-QRH.13.4
PI-QRH.13.5
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Long Range Cruise Altitude Capability . . . . . . . . . . . .
Long Range Cruise Control . . . . . . . . . . . . . . . . . . . . .
Long Range Cruise Enroute Fuel and Time . . . . . . . . .
Descent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Holding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Gear Down, Engine Inoperative . . . . . . . . . . . . . . . . . . . .PI-QRH.14.1
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Driftdown Speed/Level Off Altitude. . . . . . . . . . . . . . .
Long Range Cruise Altitude Capability . . . . . . . . . . . .
Long Range Cruise Control . . . . . . . . . . . . . . . . . . . . .
Long Range Cruise Diversion Fuel and Time. . . . . . . .
Holding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
PI-QRH.14.1
PI-QRH.14.1
PI-QRH.14.2
PI-QRH.14.3
PI-QRH.14.4
Text. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.15.1
PI-QRH.15.1
PI-QRH.15.1
PI-QRH.15.2
PI-QRH.15.4
PI-QRH.15.6
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Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Advisory Information . . . . . . . . . . . . . . . . . . . . . . . . . .
Engine Inoperative . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Gear Down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
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PI-QRH.TOC.10.4
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737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Pkg Model Identification
Section 10
Pkg Model Identification
File Model
Pkg
highlight
Identification
General
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The table below shows the airplanes that have been identified with the following
performance package. Note, some airplanes may be identified with more than one
performance package. This configuration table information reflects the Boeing
delivered configuration updated for service bulletin incorporations in
conformance with the policy stated in the introduction section of the FCOM. The
performance data is prepared for the owner/operator named on the title page. The
intent of this information is to assist flight crews and airlines in knowing which
performance package is applicable to a given airplane. The performance package
model identification information is based on Boeing's knowledge of the airline's
fleet at a point in time approximately three months prior to the page date. Notice
of Errata (NOE) will not be provided to airlines to identify airplanes that are
moved between performance packages within this manual or airplanes added to
the airline's fleet whose performance packages are already represented in this
manual. These types of changes will be updated in the next block revision.
Owners/operators are responsible for ensuring the operational documentation they
are using is complete and matches the current configuration of their airplanes, and
the accuracy and validity of all information furnished by the owner/operator or
any other party. Owners/operators receiving active revision service are
responsible to ensure that any modifications to the listed airplanes are properly
reflected in this manual.
d
Serial and tabulation number are supplied by Boeing.
Serial Number
Tabulation
Number
HS-DBO
33621
YK820
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Registry Number
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PI-QRH.ModID.10.1
Performance Inflight - QRH Pkg Model Identification
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PI-QRH.ModID.10.2
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737-800W/CFM56-7B24
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
General
Section 10
General
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
file Highlight
General
40
2.0
82.9
1.0
81.2
1.0
80.7
1.0
77.2
1.0
73.6
1.0
69.8
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CRUISE (.76/280)
Flaps Up, %N1 for Level Flight
PRESSURE
ALTITUDE (FT)
PITCH ATT
40000
%N1
PITCH ATT
35000
%N1
PITCH ATT
30000
%N1
PITCH ATT
25000
%N1
PITCH ATT
20000
%N1
PITCH ATT
15000
%N1
WEIGHT (1000 KG)
50
60
70
4.0
4.0
1100
600
4.0
3.5
4.0
1900
1500
1100
6.5
6.0
6.0
3300
2600
2100
9.5
8.5
8.0
4400
3600
3000
12.5
11.0
10.0
5300
4400
3700
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40
4.0
1700
4.0
2500
7.0
4200
11.0
5600
14.5
6700
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CLIMB (280/.76)
Flaps Up, Set Max Climb Thrust
PRESSURE
ALTITUDE (FT)
PITCH ATT
40000
V/S (FT/MIN)
PITCH ATT
30000
V/S (FT/MIN)
PITCH ATT
20000
V/S (FT/MIN)
PITCH ATT
10000
V/S (FT/MIN)
SEA
PITCH ATT
V/S (FT/MIN)
LEVEL
WEIGHT (1000 KG)
50
60
70
2.5
3.5
85.4
88.9
2.0
2.5
3.0
82.6
84.4
86.8
1.5
2.0
2.5
81.5
82.7
84.2
1.5
2.0
2.5
77.9
79.0
80.5
1.5
2.0
2.5
74.2
75.3
76.6
1.5
2.0
3.0
70.6
71.6
72.9
80
4.0
800
6.0
1700
8.0
2500
9.5
3100
80
3.5
90.4
3.0
86.1
3.0
82.3
3.5
78.2
3.5
74.4
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PI-QRH.10.1
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
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HOLDING (VREF40 + 70)
Flaps Up, %N1 for Level Flight
PRESSURE ALTITUDE (FT)
PITCH ATT
%N1
KIAS
PITCH ATT
%N1
KIAS
PITCH ATT
%N1
KIAS
40
5.0
56.1
178
5.0
52.5
178
5.0
48.9
178
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15000
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10000
80
1.5
-2700
0.5
-2000
0.5
-1700
0.5
-1500
0.5
-1400
WEIGHT (1000 KG)
50
60
70
5.0
5.0
5.0
61.7
65.9
69.8
193
212
229
5.0
5.0
5.0
57.5
62.1
65.9
192
211
228
5.5
5.0
5.0
53.9
58.1
62.0
192
210
227
80
5.0
73.2
246
5.0
69.1
244
5.0
65.5
243
U
nc
5000
WEIGHT (1000 KG)
50
60
70
-0.5
0.5
1.0
-2400
-2300
-2500
-2.0
-1.0
-0.5
-2600
-2300
-2100
-2.0
-1.0
0.0
-2300
-2000
-1900
-2.0
-1.0
0.0
-2100
-1800
-1700
-2.5
-1.0
-0.5
-1900
-1700
-1500
or
pr
in
te
d
40
-1.5
-2700
-3.5
-3100
-3.5
-2800
-3.5
-2500
-3.5
-2300
ad
ed
DESCENT (.76/280)
Flaps Up, Set Idle Thrust
PRESSURE
ALTITUDE (FT)
PITCH ATT
40000
V/S (FT/MIN)
PITCH ATT
30000
V/S (FT/MIN)
PITCH ATT
20000
V/S (FT/MIN)
PITCH ATT
10000
V/S (FT/MIN)
SEA
PITCH ATT
V/S (FT/MIN)
LEVEL
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.2
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = -2000 FT
if
d
or
pr
in
te
d
80
6.5
63.6
225
6.0
65.8
205
6.5
66.7
185
6.0
71.1
185
6.5
71.6
175
7.0
72.9
165
6.5
76.3
175
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
52.3 56.3 60.0
192
204
215
5.0
5.5
6.0
54.5 58.6 62.4
172
184
195
6.0
6.0
6.5
54.5 59.0 63.1
152
164
175
5.0
5.5
5.5
58.6 63.4 67.5
152
164
175
5.5
6.0
6.0
58.7 63.7 67.9
142
154
165
6.5
6.5
7.0
59.7 64.8 69.0
132
144
155
6.0
6.0
6.0
63.3 68.2 72.6
142
154
165
ad
ed
40
4.5
47.6
178
5.0
49.7
158
5.5
49.4
138
5.0
53.2
138
5.5
53.3
128
6.5
54.0
118
5.5
57.5
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.10.3
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = -1000 FT
if
d
U
nc
on
tro
lle
80
6.5
64.5
225
6.0
66.6
205
6.5
67.6
185
6.0
72.0
185
6.5
72.5
175
7.0
73.7
165
6.5
77.1
175
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
52.9 57.0 60.8
192
204
215
5.0
5.5
6.0
55.2 59.4 63.3
172
184
195
6.0
6.0
6.5
55.2 59.8 64.0
152
164
175
5.5
5.5
5.5
59.4 64.2 68.3
152
164
175
5.5
6.0
6.0
59.5 64.5 68.7
142
154
165
6.5
6.5
7.0
60.6 65.6 69.8
132
144
155
6.0
6.0
6.0
64.1 69.0 73.4
142
154
165
ad
ed
40
4.5
48.3
178
5.0
50.4
158
5.5
50.0
138
5.0
53.9
138
5.5
54.0
128
6.5
54.7
118
5.5
58.3
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.4
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = SEA LEVEL
if
d
or
pr
in
te
d
80
6.5
65.2
225
6.0
67.3
205
6.5
68.3
185
6.0
72.9
185
6.5
73.4
175
7.0
74.6
165
6.5
77.9
175
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
53.6 57.7 61.6
192
204
215
5.0
5.5
6.0
55.9 60.2 64.1
172
184
195
6.0
6.0
6.5
56.0 60.6 64.7
152
164
175
5.5
5.5
5.5
60.2 65.0 69.1
152
164
175
5.5
6.0
6.0
60.4 65.3 69.5
142
154
165
6.5
6.5
7.0
61.4 66.3 70.6
132
144
155
6.0
6.0
6.0
65.0 69.9 74.3
142
154
165
ad
ed
40
4.5
49.0
178
5.0
51.1
158
5.5
50.7
138
5.0
54.7
138
5.5
54.7
128
6.5
55.5
118
5.5
59.1
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.10.5
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 1000 FT
if
d
U
nc
on
tro
lle
80
6.5
66.0
225
6.0
68.1
205
6.5
69.1
185
6.0
73.7
185
6.5
74.2
175
7.0
75.4
165
6.5
78.8
175
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
54.3 58.4 62.5
192
204
215
5.0
5.5
6.0
56.7 61.0 64.8
172
184
195
6.0
6.0
6.5
56.7 61.4 65.5
152
164
175
5.5
5.5
5.5
61.0 65.8 69.9
152
164
175
5.5
6.0
6.0
61.2 66.1 70.3
142
154
165
6.5
6.5
7.0
62.2 67.1 71.5
132
144
155
6.0
6.0
6.0
65.8 70.7 75.1
142
154
165
ad
ed
40
4.5
49.8
178
5.0
51.8
158
5.5
51.4
138
5.0
55.4
138
5.5
55.4
128
6.5
56.3
118
5.5
59.9
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.6
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 2000 FT
if
d
or
pr
in
te
d
80
6.5
66.7
225
6.0
68.9
205
6.5
69.9
185
6.0
74.5
185
6.5
75.1
175
7.0
76.2
165
6.5
79.7
175
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
55.1 59.2 63.3
192
204
215
5.0
5.5
6.0
57.4 61.8 65.6
172
184
195
6.0
6.0
6.5
57.5 62.3 66.3
152
164
175
5.5
5.5
5.5
61.8 66.6 70.8
152
164
175
5.5
6.0
6.0
62.0 66.9 71.2
142
154
165
6.5
6.5
7.0
63.0 67.9 72.4
132
144
155
6.0
6.0
6.0
66.5 71.6 75.9
142
154
165
ad
ed
40
4.5
50.4
178
5.0
52.5
158
5.5
52.2
138
5.0
56.1
138
5.5
56.2
128
6.5
57.0
118
5.5
60.7
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.10.7
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 3000 FT
if
d
U
nc
on
tro
lle
80
6.5
67.4
225
6.0
69.7
205
6.5
70.7
185
6.0
75.3
185
6.5
75.9
175
7.0
77.0
165
6.5
80.5
175
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
55.8 60.0 64.1
192
205
216
5.0
5.5
6.0
58.1 62.6 66.3
172
185
196
6.0
6.0
6.5
58.2 63.1 67.1
152
165
176
5.5
5.5
5.5
62.6 67.4 71.6
152
165
176
5.5
6.0
6.0
62.8 67.7 72.1
142
155
166
6.5
6.5
7.0
63.8 68.7 73.2
132
145
156
6.0
6.0
6.0
67.3 72.5 76.7
142
155
166
ad
ed
40
4.5
51.1
178
5.0
53.3
158
5.5
52.9
138
5.0
56.9
138
5.5
56.9
128
6.5
57.8
118
5.5
61.5
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.8
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 4000 FT
if
d
or
pr
in
te
d
80
6.5
68.2
225
6.0
70.5
205
6.5
71.6
185
6.0
76.1
185
6.5
76.6
175
7.0
77.9
165
6.5
81.4
175
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
56.5 60.8 64.9
192
205
216
5.0
5.5
6.0
58.9 63.4 67.1
172
185
196
6.0
6.0
6.5
59.0 63.9 67.9
152
165
176
5.5
5.5
5.5
63.4 68.2 72.5
152
165
176
5.5
6.0
6.0
63.6 68.5 73.0
142
155
166
6.5
6.5
7.0
64.6 69.6 74.1
132
145
156
6.0
6.0
6.0
68.1 73.3 77.6
142
155
166
ad
ed
40
4.5
51.7
178
5.0
54.0
158
5.5
53.6
138
5.0
57.7
138
5.5
57.7
128
6.5
58.6
118
5.5
62.3
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.10.9
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 5000 FT
if
d
U
nc
on
tro
lle
80
6.5
69.0
225
6.0
71.4
205
6.5
72.5
185
6.0
76.9
185
6.5
77.5
175
7.0
78.8
165
6.5
82.3
175
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
57.3 61.6 65.7
192
205
216
5.0
5.5
6.0
59.7 64.2 67.9
172
185
196
6.0
6.0
6.5
59.9 64.7 68.7
152
165
176
5.5
5.5
5.5
64.2 69.1 73.3
152
165
176
5.5
6.0
6.0
64.4 69.4 73.8
142
155
166
6.5
6.5
7.0
65.4 70.5 74.9
132
145
156
6.0
6.0
6.0
69.0 74.2 78.5
142
155
166
ad
ed
40
4.5
52.4
178
5.0
54.7
158
5.5
54.4
138
5.0
58.5
138
5.5
58.5
128
6.5
59.4
118
5.5
63.1
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.10
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 6000 FT
if
d
or
pr
in
te
d
80
6.5
69.8
225
6.0
72.3
205
6.5
73.3
185
6.0
77.7
185
6.5
78.3
175
7.0
79.6
165
6.5
83.2
175
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
58.0 62.5 66.4
192
205
216
5.0
5.5
6.0
60.5 64.9 68.7
172
185
196
6.0
6.0
6.5
60.7 65.5 69.5
152
165
176
5.5
5.5
5.5
65.1 69.9 74.1
152
165
176
5.5
6.0
6.0
65.2 70.3 74.7
142
155
166
6.5
6.5
7.0
66.2 71.4 75.7
132
145
156
6.0
6.0
6.0
69.9 75.0 79.3
142
155
166
ad
ed
40
4.5
53.1
178
5.0
55.5
158
5.5
55.1
138
5.0
59.3
138
5.5
59.4
128
6.5
60.3
118
5.5
64.0
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.10.11
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 7000 FT
if
d
U
nc
on
tro
lle
80
6.5
70.6
226
6.0
73.1
206
6.5
74.1
186
6.0
78.6
186
6.5
79.2
176
7.0
80.5
166
6.5
84.1
176
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
58.8 63.4 67.1
192
205
216
5.0
5.5
6.0
61.4 65.7 69.5
172
185
196
6.0
6.0
6.5
61.6 66.3 70.4
152
165
176
5.5
5.5
5.5
65.9 70.8 75.0
152
165
176
5.5
6.0
6.0
66.0 71.2 75.4
142
155
166
6.5
6.5
7.0
67.0 72.2 76.6
132
145
156
6.0
6.0
6.0
70.8 75.8 80.2
142
155
166
ad
ed
40
4.5
53.9
178
5.0
56.3
158
5.5
55.9
138
5.0
60.1
138
5.5
60.2
128
6.5
61.1
118
5.5
64.8
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.12
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 8000 FT
if
d
or
pr
in
te
d
80
6.5
71.4
226
6.0
74.0
206
6.5
74.9
186
6.0
79.6
186
6.0
80.1
176
7.0
81.4
166
6.5
85.0
176
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
59.6 64.1 67.9
192
205
216
5.0
5.5
6.0
62.2 66.5 70.4
172
185
196
6.0
6.0
6.5
62.4 67.0 71.2
152
165
176
5.5
5.5
5.5
66.7 71.7 75.8
152
165
176
5.5
6.0
6.0
66.9 72.1 76.2
142
155
166
6.5
6.5
7.0
67.9 73.1 77.5
132
145
156
6.0
6.0
6.0
71.6 76.7 81.1
142
155
166
ad
ed
40
4.5
54.6
178
5.0
57.0
158
5.5
56.7
138
5.0
61.0
138
5.5
61.0
128
6.5
61.9
118
5.5
65.6
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.10.13
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 9000 FT
if
d
U
nc
on
tro
lle
80
6.5
72.3
226
6.0
74.8
206
6.5
75.8
186
6.0
80.4
186
6.0
81.0
176
7.0
82.3
166
6.5
85.9
176
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.5
5.5
6.0
60.5 64.9 68.6
192
205
216
5.0
5.5
6.0
63.0 67.3 71.3
172
185
196
6.0
6.0
6.5
63.2 67.9 72.1
152
165
176
5.5
5.5
5.5
67.5 72.5 76.6
152
165
176
5.5
6.0
6.0
67.7 72.9 77.1
142
155
166
6.5
6.5
7.0
68.7 73.9 78.4
132
145
156
6.0
6.0
6.0
72.5 77.6 82.0
142
155
166
ad
ed
40
4.5
55.4
178
5.0
57.7
158
5.5
57.5
138
5.0
61.8
138
5.5
61.8
128
6.5
62.8
118
5.5
66.4
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.14
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 10000 FT
if
d
or
pr
in
te
d
80
6.5
73.0
227
6.0
75.6
207
6.5
76.6
187
6.0
81.4
187
6.0
81.9
177
7.0
83.2
167
6.5
86.9
177
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.5
5.5
6.0
61.3 65.6 69.5
192
205
216
5.0
5.5
6.0
63.8 68.1 72.2
172
185
196
6.0
6.0
6.0
64.0 68.7 72.9
152
165
176
5.5
5.5
5.5
68.4 73.3 77.5
152
165
176
5.5
6.0
6.0
68.6 73.7 78.0
142
155
166
6.5
6.5
7.0
69.7 74.8 79.3
132
145
156
6.0
6.0
6.0
73.4 78.5 82.9
142
155
166
ad
ed
40
4.5
56.1
178
5.0
58.5
158
5.5
58.3
138
5.0
62.6
138
5.5
62.7
128
6.5
63.6
118
5.5
67.2
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.10.15
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 11000 FT
if
d
U
nc
on
tro
lle
80
6.5
73.9
227
6.0
76.4
207
6.5
77.5
187
6.0
82.3
187
6.0
82.9
177
7.0
84.2
167
6.5
88.0
177
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.5
5.5
6.0
62.3 66.3 70.3
192
205
217
5.0
5.5
6.0
64.6 69.1 73.1
172
185
197
6.0
6.0
6.0
64.9 69.7 73.8
152
165
177
5.5
5.5
5.5
69.4 74.2 78.5
152
165
177
5.5
6.0
6.0
69.7 74.6 79.0
142
155
167
6.5
6.5
6.5
70.8 75.8 80.3
132
145
157
6.0
6.0
6.0
74.3 79.5 84.0
142
155
167
ad
ed
40
4.5
56.9
178
5.0
59.5
158
5.5
59.4
138
5.0
63.6
138
5.5
63.8
128
6.5
64.7
118
5.5
68.4
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.16
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 12000 FT
if
d
or
pr
in
te
d
80
6.5
74.6
228
6.0
77.3
208
6.5
78.5
188
6.0
83.3
188
6.0
83.9
178
6.5
85.2
168
6.0
89.1
178
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.5
5.5
6.0
63.0 67.1 71.2
192
205
217
5.5
5.5
6.0
65.4 70.0 73.8
172
185
197
6.0
6.0
6.0
65.8 70.7 74.7
152
165
177
5.5
5.5
5.5
70.4 75.1 79.5
152
165
177
5.5
6.0
6.0
70.8 75.6 80.0
142
155
167
6.5
6.5
6.5
71.8 76.9 81.3
132
145
157
6.0
6.0
6.0
75.3 80.5 85.0
142
155
167
ad
ed
40
5.0
57.7
178
5.0
60.6
158
5.5
60.5
138
5.0
64.6
138
5.5
64.7
128
6.5
65.8
118
5.5
69.6
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.10.17
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 13000 FT
if
d
U
nc
on
tro
lle
80
6.5
75.5
228
6.0
78.2
208
6.5
79.4
188
6.0
84.2
188
6.0
84.8
178
6.5
86.2
168
6.0
90.2
178
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.5
5.5
6.0
63.7 67.9 72.0
192
205
217
5.5
5.5
6.0
66.3 70.9 74.6
172
185
197
6.0
6.0
6.0
66.8 71.7 75.6
152
165
177
5.5
5.5
5.5
71.4 76.0 80.4
152
165
177
5.5
6.0
6.0
71.7 76.5 81.0
142
155
167
6.5
6.5
6.5
72.8 77.9 82.3
132
145
157
6.0
6.0
6.0
76.4 81.5 86.0
142
155
167
ad
ed
40
5.0
58.5
178
5.0
61.4
158
5.5
61.5
138
5.0
65.6
138
5.5
65.8
128
6.5
66.9
118
5.5
70.6
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.18
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 14000 FT
if
d
or
pr
in
te
d
80
6.5
76.3
228
6.0
79.0
208
6.5
80.3
188
6.0
85.1
188
6.0
85.8
178
6.5
87.3
168
6.0
91.5
178
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.5
5.5
6.0
64.4 68.7 72.8
192
205
217
5.5
5.5
6.0
67.1 71.7 75.4
172
185
197
6.0
6.0
6.0
67.8 72.5 76.5
152
165
177
5.5
5.5
5.5
72.3 77.0 81.3
152
165
177
5.5
6.0
6.0
72.6 77.6 81.9
142
155
167
6.5
6.5
6.5
73.8 78.9 83.3
132
145
157
6.0
6.0
6.0
77.5 82.5 87.1
142
155
167
ad
ed
40
5.0
59.4
179
5.0
62.3
159
5.5
62.3
139
5.0
66.5
139
5.5
66.9
129
6.5
68.1
119
5.5
71.6
129
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.10.19
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 14500 FT
if
d
U
nc
on
tro
lle
80
6.5
76.7
229
6.0
79.5
209
6.5
80.7
189
6.0
85.5
189
6.0
86.3
179
6.5
87.8
169
6.0
92.3
179
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.5
5.5
6.0
64.8 69.2 73.2
192
206
218
5.5
5.5
6.0
67.6 72.1 75.9
172
186
198
6.0
6.0
6.0
68.3 72.9 76.9
152
166
178
5.5
5.5
5.5
72.7 77.5 81.8
152
166
178
5.5
6.0
6.0
73.1 78.1 82.4
142
156
168
6.5
6.5
6.5
74.2 79.4 83.7
132
146
158
6.0
6.0
6.0
78.0 83.0 87.6
142
156
168
ad
ed
40
5.0
59.9
179
5.0
62.7
159
5.5
62.8
139
5.0
67.1
139
5.5
67.4
129
6.5
68.6
119
5.5
72.1
129
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.20
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = -2000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = -1000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
46.7 50.6
54.1
145
159
171
0.5
1.0
1.0
51.0 55.3
59.0
139
152
163
-0.5
-0.5
-0.5
56.2 60.9
64.9
132
144
155
80
2.5
57.0
181
1.0
62.3
173
0.0
68.3
164
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
47.3 51.2
54.8
145
159
171
0.5
1.0
1.0
51.7 56.0
59.8
139
152
163
-0.5
-0.5
-0.5
56.9 61.7
65.7
132
144
155
80
2.5
57.8
181
1.0
63.1
173
0.0
69.0
165
or
pr
in
te
d
40
2.0
42.2
130
0.5
46.3
125
-0.5
50.8
118
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
42.7
130
0.5
46.9
125
-0.5
51.5
118
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.10.21
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = SEA LEVEL
Flap placard speed exceeded in shaded area.
Airport Altitude = 1000 FT
80
2.5
58.4
181
1.0
63.9
173
0.0
69.8
165
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
48.6
52.6
56.2
145
159
171
0.5
1.0
1.0
53.2
57.5
61.3
139
152
163
-0.5
-0.5
-0.5
58.4 63.2
67.3
132
144
155
80
2.5
59.2
181
1.0
64.6
173
0.0
70.6
165
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
48.0 51.9
55.5
145
159
171
0.5
1.0
1.0
52.5
56.7
60.5
139
152
163
-0.5
-0.5
-0.5
57.6 62.4
66.5
132
144
155
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
43.3
130
0.5
47.5
125
-0.5
52.2
118
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
43.9
130
0.5
48.1
125
-0.5
52.9
118
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.22
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 2000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 3000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
49.2 53.3
56.9
145
159
171
0.5
1.0
1.0
53.8 58.2
62.1
139
152
163
-0.5
-0.5
-0.5
59.2 64.0
68.0
132
144
155
80
2.5
59.9
181
1.0
65.4
173
0.0
71.5
165
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
49.8 54.1
57.6
145
159
171
0.5
1.0
1.0
54.5 59.0
63.0
139
152
163
-0.5
-0.5
-0.5
59.9 64.9
68.8
132
144
155
80
2.5
60.7
181
1.0
66.2
173
0.0
72.3
165
or
pr
in
te
d
40
2.0
44.5
130
0.5
48.8
125
-0.5
53.6
118
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
45.1
131
0.5
49.4
125
-0.5
54.4
118
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.10.23
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 4000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 5000 FT
80
2.5
61.5
181
1.0
67.0
173
0.0
73.2
165
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
51.2
55.4
59.0
145
159
171
0.5
1.0
1.0
56.0
60.6
64.5
139
152
163
-0.5
-0.5
-0.5
61.5 66.4
70.4
132
144
155
80
2.5
62.3
181
1.0
67.7
173
0.0
74.0
165
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
50.5 54.7
58.3
145
159
171
0.5
1.0
1.0
55.3
59.8
63.7
139
152
163
-0.5
-0.5
-0.5
60.7 65.6
69.6
132
144
155
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
45.8
131
0.5
50.1
125
-0.5
55.1
118
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
46.5
131
0.5
50.8
125
-0.5
55.8
118
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.24
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 6000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 7000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
51.9 56.1
59.8
145
159
171
0.5
1.0
1.0
56.7 61.4
65.2
139
152
163
-0.5
-0.5
-0.5
62.3 67.1
71.3
132
144
155
80
2.5
63.0
182
1.0
68.5
173
0.0
74.8
165
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
52.6 56.8
60.6
146
159
171
0.5
1.0
1.0
57.4 62.2
66.0
139
152
163
-0.5
-0.5
-0.5
63.1 67.9
72.2
132
144
156
80
2.5
63.8
182
1.0
69.3
173
0.0
75.6
165
or
pr
in
te
d
40
2.0
47.1
131
0.5
51.6
125
-0.5
56.6
118
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
47.7
131
0.5
52.3
125
-0.5
57.3
118
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.10.25
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 8000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 9000 FT
80
2.5
64.5
182
1.0
70.1
173
0.0
76.4
165
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
54.0
58.3
62.2
146
159
171
0.5
1.0
1.0
59.0
63.7
67.6
139
152
163
-0.5
-0.5
-0.5
64.7 69.6
73.8
132
145
156
80
2.5
65.2
182
1.0
70.9
173
0.0
77.2
165
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
53.3 57.6
61.4
146
159
171
0.5
1.0
1.0
58.2
62.9
66.8
139
152
163
-0.5
-0.5
-0.5
64.0 68.7
73.0
132
145
156
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
48.4
131
0.5
52.9
125
-0.5
58.1
118
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
49.0
131
0.5
53.7
125
-0.5
58.9
118
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.26
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 10000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 11000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
54.7 59.1
62.9
146
159
171
0.5
1.0
1.0
59.8 64.5
68.3
139
152
163
-0.5
-0.5
-0.5
65.5 70.5
74.6
132
145
156
80
2.5
65.9
182
1.0
71.7
173
0.0
78.1
165
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
55.5 59.9
63.6
146
159
171
0.5
1.0
1.0
60.7 65.3
69.1
139
152
163
-0.5
-0.5
-0.5
66.3 71.3
75.4
132
145
156
80
2.5
66.6
182
1.0
72.5
173
-0.5
79.0
165
or
pr
in
te
d
40
2.0
49.7
131
0.5
54.4
125
-0.5
59.8
118
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
50.4
131
0.5
55.1
125
-0.5
60.5
118
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.10.27
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 12000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 13000 FT
80
2.5
67.4
182
1.0
73.3
173
-0.5
79.8
166
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
56.9
61.5
65.1
146
160
172
0.5
1.0
1.0
62.2
66.8
70.8
139
152
164
-0.5
-0.5
-0.5
67.9 73.0
77.1
132
145
156
80
2.5
68.1
182
1.0
74.1
173
-0.5
80.7
166
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
56.2 60.7
64.3
146
159
172
0.5
1.0
1.0
61.5
66.1
70.0
139
152
164
-0.5
-0.5
-0.5
67.1 72.2
76.2
132
145
156
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
51.1
131
0.5
55.9
125
-0.5
61.3
118
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
51.9
131
0.5
56.6
125
-0.5
62.2
118
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.28
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 14000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 14500 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
57.8 62.4
65.8
146
160
172
0.5
1.0
1.0
63.1 67.7
71.7
139
152
164
-0.5
-0.5
-0.5
68.9 73.9
78.0
132
145
156
80
2.5
69.0
182
1.0
74.9
174
-0.5
81.7
166
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
58.3 62.8
66.3
146
160
172
0.5
1.0
1.0
63.6 68.2
72.1
139
152
164
-0.5
-0.5
-0.5
69.5 74.4
78.5
132
145
156
80
2.5
69.4
182
1.0
75.3
174
-0.5
82.2
167
or
pr
in
te
d
40
2.0
52.7
131
0.5
57.6
125
-0.5
63.2
118
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
53.1
131
0.5
58.2
125
-0.5
63.7
118
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.10.29
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
GO-AROUND
Flaps 15, Gear Up, Set Go-Around Thrust
5000
SEA
LEVEL
U
nc
on
tro
lle
d
if
-2000
80
9.0
1100
177
10.5
1500
175
11.5
1800
175
13.0
2000
175
13.0
2000
174
or
pr
in
te
d
10000
WEIGHT (1000 KG)
50
60
70
13.5
11.5
10.0
2500
1900
1400
142
155
166
16.0
13.5
11.5
3000
2400
1900
142
155
166
18.0
15.0
13.0
3400
2700
2200
142
154
165
20.0
16.5
14.5
3700
3000
2500
142
154
165
20.5
17.0
14.5
3600
3000
2500
142
154
165
ad
ed
14500
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
40
17.0
3200
128
19.5
3800
128
22.5
4200
128
25.0
4500
128
25.5
4500
128
do
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PRESSURE ALTITUDE (FT)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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D6-27370-8AS-NOK
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737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
Max Climb %N1
file Highlight
Based on engine bleed for packs on or off and anti-ice off
PRESSURE ALTITUDE (FT)/SPEED (KIAS/MACH)
10000
15000
20000
25000
30000
35000
280
280
280
280
280
.78
89.7
89.8
89.6
91.4
93.0
94.4
90.5
90.7
90.0
90.8
92.4
93.7
91.3
91.5
91.0
90.8
91.7
93.0
92.1
92.3
91.9
91.7
91.7
92.3
92.9
93.1
92.7
92.5
92.5
91.6
93.6
93.8
93.6
93.3
93.3
92.4
94.3
94.6
94.4
94.1
94.0
93.2
95.0
95.2
95.2
94.8
94.7
94.0
95.8
96.0
95.9
95.6
95.4
94.7
95.2
96.8
96.7
96.3
96.1
95.5
94.4
97.1
97.6
97.0
96.7
96.2
93.6
96.3
98.5
97.9
97.4
97.0
92.8
95.5
97.9
99.0
98.4
97.8
92.0
94.7
97.2
98.9
99.4
98.6
91.2
93.9
96.4
98.1
99.7
99.5
90.3
93.1
95.6
97.4
98.9
100.5
89.5
92.3
94.8
96.6
98.1
100.2
88.7
91.4
94.1
95.8
97.3
99.3
87.8
90.6
93.3
95.0
96.5
98.5
87.0
89.8
92.4
94.1
95.6
97.6
86.1
88.9
91.6
93.3
94.8
96.8
37000
.78
94.5
93.8
93.1
92.4
91.7
91.7
92.6
93.4
94.2
95.0
95.8
96.6
97.5
98.3
99.2
100.1
100.7
99.9
99.0
98.2
97.3
41000
.78
92.8
92.1
91.4
90.7
90.0
90.1
91.1
92.1
93.0
94.0
94.9
95.8
96.7
97.7
98.7
99.7
100.3
99.5
98.7
97.8
96.9
or
pr
in
te
d
5000
280
89.7
90.5
91.2
91.9
92.6
93.3
94.1
94.1
93.3
92.5
91.8
91.0
90.2
89.4
88.6
87.8
87.0
86.1
85.3
84.5
83.6
ad
ed
60
55
50
45
40
35
30
25
20
15
10
5
0
-5
-10
-15
-20
-25
-30
-35
-40
0
280
89.4
90.2
90.9
91.6
92.4
92.9
92.2
91.5
90.7
90.0
89.2
88.4
87.7
86.9
86.1
85.3
84.5
83.7
82.9
82.0
81.2
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TAT (°C)
%N1 Adjustments for Engine Bleeds
BLEED CONFIGURATION
ENGINE ANTI-ICE
ENGINE & WING ANTI-ICE*
PRESSURE ALTITUDE (1000 FT)
10
20
30
35
-0.8
-0.9
-0.9
-0.8
-2.1
-2.5
-2.7
-3.0
41
-0.8
-3.0
U
nc
on
tro
lle
d
if
*Dual bleed sources
0
-0.6
-1.8
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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Performance Inflight - QRH
General
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Go-around %N1
Based on engine bleed for packs on, engine and wing anti-ice on or off
0
91.8
92.6
93.3
94.1
94.9
95.8
95.7
94.9
94.2
93.4
92.6
91.8
91.0
90.2
89.4
88.6
87.8
86.9
86.1
85.2
84.4
83.5
82.6
1000
91.8
92.6
93.3
94.1
94.9
95.8
96.3
95.5
94.7
94.0
93.2
92.4
91.6
90.8
90.0
89.2
88.3
87.5
86.7
85.8
84.9
84.1
83.2
2000
3000
4000
5000
6000
7000
8000
9000 10000
92.5
93.3
94.1
94.8
95.7
96.5
96.1
95.3
94.5
93.8
93.0
92.2
91.4
90.6
89.7
88.9
88.1
87.2
86.3
85.5
84.6
83.7
92.5
93.3
94.0
94.8
95.7
96.5
96.7
95.9
95.1
94.4
93.6
92.8
92.0
91.1
90.3
89.5
88.6
87.8
86.9
86.1
85.2
84.3
93.3
94.0
94.7
95.6
96.4
97.3
96.5
95.8
95.0
94.2
93.4
92.6
91.8
90.9
90.1
89.3
88.4
87.6
86.7
85.8
84.9
93.2
94.0
94.7
95.5
96.4
97.3
97.2
96.5
95.7
94.9
94.1
93.3
92.5
91.7
90.8
90.0
89.2
88.3
87.4
86.6
85.7
93.2
93.9
94.6
95.5
96.3
97.2
97.9
97.2
96.4
95.6
94.8
94.0
93.2
92.4
91.6
90.7
89.9
89.0
88.2
87.3
86.4
93.9
94.6
95.4
96.2
97.1
98.3
97.9
97.1
96.4
95.6
94.8
94.0
93.2
92.3
91.5
90.7
89.8
89.0
88.1
87.2
93.8
94.6
95.3
96.2
97.0
98.2
98.7
97.9
97.1
96.4
95.6
94.8
94.0
93.2
92.3
91.5
90.7
89.8
89.0
88.1
94.5
95.3
96.1
97.0
98.1
99.4
98.7
98.0
97.2
96.4
95.7
94.9
94.1
93.3
92.5
91.6
90.8
90.0
89.1
PRESSURE ALTITUDE (FT)
3000 4000 5000 6000 7000
0.8
0.8
0.8
0.9
0.9
-0.1 -0.1 -0.1 -0.1 -0.1
8000
0.9
-0.1
9000 10000
1.0
0.9
-0.1 -0.1
94.4
95.2
96.0
96.9
98.0
99.4
99.5
98.8
98.1
97.3
96.5
95.8
95.0
94.2
93.4
92.6
91.8
90.9
90.1
or
pr
in
te
d
60
55
50
45
40
35
30
25
20
15
10
5
0
-5
-10
-15
-20
-25
-30
-35
-40
-45
-50
AIRPORT PRESSURE ALTITUDE (FT)
-2000
91.0
91.7
92.5
93.3
94.1
94.3
93.5
92.8
92.0
91.3
90.5
89.7
89.0
88.2
87.4
86.6
85.8
84.9
84.1
83.3
82.4
81.6
80.7
ad
ed
TAT
(°C)
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AIRPORT
OAT
°C
°F
57
134
52
125
47
116
42
108
37
99
32
90
27
81
22
72
17
63
12
54
7
45
2
36
-3
27
-8
18
-13
9
-17
1
-22
-8
-27
-17
-32
-26
-37
-35
-42
-44
-47
-53
-52
-62
%N1 Adjustments for Engine Bleeds
0
0.8
-0.1
1000
0.8
-0.1
2000
0.8
-0.1
if
-2000
0.6
-0.1
U
nc
on
tro
lle
d
BLEED
CONFIGURATION
PACKS OFF
A/C HIGH
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
General
737 Flight Crew Operations Manual
VREF
file Highlight
40
160
155
151
146
141
135
128
122
115
108
15
177
172
167
161
156
149
143
136
128
121
U
nc
on
tro
lle
d
if
do
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ad
ed
85
80
75
70
65
60
55
50
45
40
FLAPS
30
168
163
158
153
148
142
136
129
122
115
or
pr
in
te
d
WEIGHT (1000 KG)
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PI-QRH.10.33
Performance Inflight - QRH
General
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o
ad
ed
or
pr
in
te
d
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
U
nc
on
tro
lle
d
if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.10.34
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September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Advisory Information
Section 11
Advisory
file
Highlight
Information
ADVISORY INFORMATION
Runway Surface Condition Correlation
Advisory Information
Advisory Information
5
4
3
Dry
Wet (Smooth, Grooved or PFC) or Frost
3 mm (0.12 inches) or less of: Water, Slush, Dry Snow or Wet Snow
Compacted Snow at or below -15°C OAT
Wet (Slippery), Dry Snow or Wet Snow (any depth) over Compacted Snow
Greater than 3 mm (0.12 inches) of : Dry Snow or Wet Snow
Compacted Snow at OAT warmer than -15°C
Greater than 3 mm (0.12 inches) of: Water or Slush
Ice
Wet Ice, Water on top of Compacted Snow, Dry Snow or Wet Snow over Ice
Good
Good to Medium
Medium
Medium to Poor
Poor
Nil
U
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2
1
0
REPORTED
BRAKING
ACTION
Dry
RUNWAY SURFACE CONDITION DESCRIPTION
or
pr
in
te
d
RUNWAY
CONDITION
CODE
6
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PI-QRH.11.1
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
1280
1575
2160
2695
2955
65/-65
70/-75
110/-125
160/-175
190/-205
25/35
35/40
50/70
75/105
90/120
-40/140
-50/175
-85/290
-115/395
-140/465
40/50
45/60
50/70
75/105
90/120
-70/235
-70/240
-85/290
-115/395
-140/465
40/-35
35/-30
5/0
35/-45
75/-85
-90/310
-90/315
-100/340
-120/425
-140/475
-110/385
-110/390
-110/395
-125/450
-140/485
Good Reported Braking Action
1705
1805
2160
2695
2955
85/-90
90/-100
110/-125
160/-175
190/-205
40
65
110
110
100
25
0
0
70
225
45
5
0
70
335
40/-40
40/-40
60/-60
75/-75
80/-80
60
70
110
110
100
80
85
5
70
225
180
195
15
70
335
70/-55
65/-50
40/-25
55/-60
85/-90
50/-50
50/-50
60/-60
75/-75
80/-85
65
80
110
110
100
150
150
85
95
235
350
360
245
165
370
100/-75
90/-70
75/-50
75/-70
100/-90
60/-60
60/-60
65/-65
75/-75
80/-85
75
85
110
110
100
220
220
160
120
240
520
525
470
260
405
do
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MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
10/-10
0/0
0/0
35/-45
75/-85
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF30
25/-25
35/-35
60/-60
75/-75
80/-80
ad
ed
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
1985
2055
2275
2725
2960
110/-115
115/-120
125/-135
160/-175
190/-205
50/70
55/70
60/80
80/105
90/120
if
Medium Reported Braking Action
130/-140
140/-145
140/-145
160/-180
190/-205
d
2265
2305
2390
2755
2970
65/85
65/85
65/85
80/105
90/120
U
nc
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
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PI-QRH.11.2
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September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
APP
SPD
ADJ
REVERSE
THRUST
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
165/-115
165/-110
150/-100
145/-105
160/-125
65/-70
65/-70
70/-70
80/-80
85/-90
80
90
105
105
100
340
340
310
255
340
860
865
840
660
735
75/-80
75/-80
75/-80
80/-85
85/-90
85
90
100
105
100
460
460
460
385
435
1200
1210
1215
1065
1070
Medium To Poor Reported Braking Action
2580
2600
2655
2920
3085
160/-165
165/-170
165/-170
180/-195
200/-215
80/105
80/105
80/105
90/120
95/130
Poor Reported Braking Action
2895
2900
2920
3080
3200
190/-195
190/-195
195/-195
200/-205
215/-220
90/125
90/125
90/125
100/130
100/140
-160/610
-160/610
-160/615
-165/635
-175/650
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MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
-135/495
-135/500
-135/505
-145/540
-155/565
ad
ed
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
PER
5 KTS ONE NO
ABOVE REV REV
VREF30
or
pr
in
te
d
REF
DIST
235/-155
235/-155
230/-145
220/-145
225/-155
if
Reference distance is based on sea level, standard day, no wind or slope, VREF30, two-engine detent No. 2
reverse thrust, and auto speedbrakes.
For max manual braking and manual speedbrakes, increase reference landing distance by 70 m.
For autobrake and manual speedbrakes, increase reference landing distance by 65 m.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
All reference distances and adjustments shown have been increased by 15%.
U
nc
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d
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.3
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
1230
1480
2005
2510
2775
65/-60
65/-70
100/-115
145/-160
175/-190
25/30
30/40
45/65
70/90
85/110
-40/130
-45/160
-80/270
-110/380
-130/450
40/50
40/50
45/65
70/90
85/110
-65/230
-70/235
-80/275
-110/380
-130/450
40/-35
35/-30
10/-5
25/-40
65/-75
-85/305
-85/310
-95/335
-115/405
-130/455
-105/380
-105/385
-110/390
-120/430
-130/465
Good Reported Braking Action
1635
1730
2015
2510
2775
80/-85
85/-90
100/-115
145/-160
175/-190
40
65
105
110
100
15
0
0
40
180
40
0
0
40
255
35/-35
40/-40
50/-50
70/-70
75/-75
60
70
110
110
100
75
80
5
40
180
160
175
15
40
255
70/-55
60/-50
45/-30
45/-50
80/-80
45/-45
45/-50
55/-55
70/-70
75/-75
65
80
105
110
100
135
140
90
65
185
315
320
235
130
285
100/-75
85/-70
80/-50
65/-65
90/-85
50/-50
50/-60
60/-60
70/-70
75/-75
75
85
105
110
100
195
195
175
85
195
465
465
450
220
315
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
10/-10
0/0
0/0
25/-40
65/-75
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF40
25/-25
30/-30
50/-50
70/-70
75/-75
ad
ed
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1900
1960
2130
2545
2785
100/-110
105/-115
110/-125
145/-165
175/-190
50/65
50/65
55/70
70/95
85/110
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
Medium Reported Braking Action
120/-130
125/-140
125/-140
150/-165
175/-190
d
2165
2190
2245
2580
2790
60/80
65/80
65/80
70/100
85/110
U
nc
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.4
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
APP
SPD
ADJ
REVERSE
THRUST
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
165/-110
160/-110
150/-100
140/-100
155/-120
60/-65
60/-65
65/-65
70/-75
80/-80
80
85
100
105
100
305
305
295
210
290
70/-75
70/-75
70/-75
75/-80
80/-85
85
85
100
105
100
415 1070
415 1070
415 1075
335 955
385 935
Medium To Poor Reported Braking Action
2460
2475
2510
2740
2905
150/-160
150/-160
150/-165
165/-180
185/-200
70/100
75/100
75/100
80/110
90/120
Poor Reported Braking Action
2755
2765
2775
2900
3015
180/-185
180/-185
180/-190
185/-190
195/-205
85/115
85/120
85/120
85/120
90/125
-160/600
-160/600
-160/605
-160/615
-165/635
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
-130/490
-130/490
-135/495
-140/525
-150/550
ad
ed
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
PER
5 KTS ONE NO
ABOVE REV REV
VREF40
or
pr
in
te
d
REF
DIST
230/-150
230/-150
225/-145
215/-140
220/-150
770
770
760
585
625
if
Reference distance is based on sea level, standard day, no wind or slope, VREF40, two-engine detent No. 2
reverse thrust, and auto speedbrakes.
For max manual braking and manual speedbrakes, increase reference landing distance by 65 m.
For autobrake and manual speedbrakes, increase reference landing distance by 50 m.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
All reference distances and adjustments shown have been increased by 15%.
U
nc
on
tro
lle
d
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.5
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
file Highlight
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Airspeed Unreliable (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1225
1585
2700
80/-65
70/-80
165/-180
25/35
35/45
85/110
-40/130
-50/165
-110/370
15/-10
5/-5
50/-55
80/-85
85/-95
165/-180
40/55
45/60
85/110
-60/215
-65/225
-110/370
35/-30
30/-25
55/-55
30
0
165
60
5
180
40/-40
40/-40
75/-75
N/A
N/A
N/A
90
100
165
205
230
180
55/70
55/75
85/110
-80/285
-85/290
-115/395
65/-50
60/-45
70/-65
50/-50
50/-50
75/-80
N/A
N/A
N/A
165
175
185
400
420
270
65/85
65/90
70/90
-100/350
-100/355
-105/370
90/-70
85/-65
60/-45
55/-55
55/-60
65/-65
N/A
N/A
N/A
240
245
145
595
605
460
80/105
80/110
80/110
-125/450
-125/455
-130/465
150/-105
150/-100
130/-85
65/-70
65/-70
70/-75
N/A
N/A
N/A
375
375
315
990
995
920
90/125
90/125
90/125
-145/550
-145/550
-150/555
210/-140
210/-135
195/-125
75/-80
75/-80
75/-80
N/A
N/A
N/A
505 1385
500 1380
485 1375
Good To Medium Reported Braking Action
1900
1990
2730
105/-110
110/-120
170/-185
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
25/-25
35/-35
75/-75
ad
ed
1625
1750
2700
REVERSE
THRUST
ADJ
N/A
N/A
N/A
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2175
2230
2405
130/-135
130/-140
135/-145
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
160/-165
160/-165
160/-170
d
2480
2510
2620
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2785
2785
2835
185/-190
185/-190
185/-190
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.6
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Airspeed Unreliable (Flaps 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1175
1485
2495
60/-60
60/-70
150/-160
75/-80
80/-90
150/-160
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/125
-45/155
-105/355
15/-10
5/-5
45/-50
25/-25
30/-35
70/-70
N/A
N/A
N/A
25
0
140
55
5
160
40/50
40/55
75/95
-60/210
-65/220
-105/355
35/-30
30/-30
45/-50
35/-35
40/-40
70/-70
N/A
N/A
N/A
80
90
140
185
205
160
-80/275
-80/285
-110/380
60/-50
55/-50
65/-60
45/-45
50/-50
70/-70
N/A
N/A
N/A
150
155
160
355
370
245
-95/340
-95/345
-100/360
85/-70
80/-65
60/-50
50/-55
55/-55
60/-60
N/A
N/A
N/A
215
215
135
520
530
420
75/100
75/100
75/100
-120/440
-120/440
-125/450
145/-100
140/-95
125/-90
60/-65
65/-65
65/-70
N/A
N/A
N/A
325
325
280
845
845
795
85/115
85/115
85/115
-140/535
-140/535
-145/540
200/-130
200/-125
190/-125
65/-70
70/-75
70/-75
N/A
N/A
N/A
435 1165
430 1160
425 1165
ad
ed
1565
1675
2495
REVERSE
THRUST
ADJ
25/30
30/40
75/95
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1815
1895
2525
100/-105
100/-110
150/-165
50/65
50/70
75/100
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2065
2115
2250
120/-125
120/-130
120/-135
60/80
60/80
60/85
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
145/-150
145/-155
145/-155
d
2340
2370
2455
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2610
2620
2660
170/-170
170/-175
170/-175
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.7
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Airspeed Unreliable (Flaps 40)
VREF40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1135
1395
2345
55/-55
55/-65
135/-150
20/30
30/35
70/90
-35/120
-45/150
-100/340
15/-10
5/0
40/-45
70/-80
75/-85
135/-150
35/50
40/50
70/90
-60/205
-60/215
-100/340
N/A
N/A
N/A
20
0
105
45
0
110
35/-30
30/-25
40/-45
35/-35
35/-35
65/-65
N/A
N/A
N/A
75
85
105
170
185
110
45/65
50/65
70/90
-80/270
-80/280
-105/365
60/-50
55/-45
55/-55
45/-45
45/-45
65/-65
N/A
N/A
N/A
135
140
125
320
330
195
55/75
60/80
60/80
-95/335
-95/340
-100/350
85/-65
80/-60
60/-50
50/-50
50/-50
55/-55
N/A
N/A
N/A
195
195
135
465
475
405
70/95
70/95
70/95
-120/430
-120/435
-120/440
140/-100
140/-95
125/-90
60/-60
60/-60
60/-65
N/A
N/A
N/A
295
295
265
750
755
725
80/110
80/110
80/110
-140/525
-140/525
-140/530
195/-130
195/-125
190/-125
65/-70
65/-70
65/-70
N/A
N/A
N/A
395 1035
390 1035
395 1045
Good To Medium Reported Braking Action
1745
1815
2375
90/-100
95/-105
140/-155
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1510
1605
2345
REVERSE
THRUST
ADJ
20/-20
30/-30
65/-65
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
1980
2020
2115
110/-120
115/-125
115/-125
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
135/-145
140/-145
140/-145
d
2240
2265
2325
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2495
2505
2530
160/-165
160/-165
160/-165
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.8
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
All Flaps Up Landing
VREF40 + 55
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1480
2005
3510
185/-85
85/-90
195/-225
85/-95
90/-100
195/-225
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-45/205
-60/195
-130/430
20/-15
5/-5
75/-85
35/-35
50/-50
105/-105
45
75
100
45
5
280
95
20
330
50/65
55/75
115/150
-65/230
-75/245
-130/430
40/-35
30/-25
75/-85
45/-50
55/-55
105/-105
45
70
100
110
85
280
255
225
330
-90/310
-95/320
-135/455
75/-60
65/-55
90/-95
60/-65
65/-65
105/-105
55
75
100
215
205
305
515
515
435
-110/385
-110/390
-120/420
105/-85
100/-80
65/-60
70/-75
75/-75
90/-90
65
75
110
315
325
165
775
800
510
100/140
105/140
105/145
-140/495
-140/500
-145/520
180/-130
175/-120
145/-105
85/-90
90/-90
95/-100
75
85
110
505 1345
505 1355
385 1175
120/165
120/165
120/165
-165/605
-165/605
-170/615
250/-170
245/-160
220/-150
95/-100
100/-100
100/-105
80
90
110
690 1915
685 1905
600 1840
ad
ed
1905
2150
3510
REVERSE
THRUST
ADJ
50/105
45/70
115/150
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
2275
2440
3540
115/-125
120/-130
200/-225
65/90
70/95
115/150
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2645
2730
3100
145/-155
150/-160
145/-170
80/110
85/115
90/120
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
185/-190
185/-195
180/-200
d
3060
3105
3350
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3470
3475
3595
220/-225
215/-225
210/-225
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.9
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
ANTISKID INOPERATIVE (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1945
105/-110
50/65
-80/290
55/-45
Autobrake Inoperative
Autobrake Inoperative
60/80
-100/350
85/-65
Autobrake Inoperative
Autobrake Inoperative
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
2165
125/-130
Good To Medium Reported Braking Action
2450
155/-155
45/-45
60
145
345
50/-55
70
215
530
905
75/100
-125/450 145/-100
Autobrake Inoperative
Autobrake Inoperative
60/-65
75
340
85/120
-145/545 200/-135
Autobrake Inoperative
Autobrake Inoperative
70/-75
80
460 1280
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
Good Reported Braking Action
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2735
180/-180
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
220/-220
d
3170
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
105/150
-195/775 415/-220
Autobrake Inoperative
Autobrake Inoperative
80/-90
90
780 2600
120/175
-245/1005 625/-305
Autobrake Inoperative
Autobrake Inoperative
85/-105
95
1100 3915
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3600
260/-260
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.10
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
ANTISKID INOPERATIVE (Flaps 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1845
95/-105
2045
115/-120
PER
5 KTS ONE NO
ABOVE REV REV
VREF
45/60
-80/280
55/-45
Autobrake Inoperative
Autobrake Inoperative
40/-45
60
125
300
55/75
-95/340
80/-65
Autobrake Inoperative
Autobrake Inoperative
50/-50
65
185
455
-120/435 135/-95
Autobrake Inoperative
Autobrake Inoperative
60/-60
75
290
765
-140/530 190/-125
Autobrake Inoperative
Autobrake Inoperative
65/-70
80
395 1075
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
REVERSE
THRUST
ADJ
ad
ed
Dry Runway
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
2305
140/-145
70/90
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2565
165/-165
80/105
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
200/-200
d
2960
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
95/130
-190/755 390/-205
Autobrake Inoperative
Autobrake Inoperative
70/-85
85
670 2145
110/155
-235/980 590/-285
Autobrake Inoperative
Autobrake Inoperative
75/-100
90
945 3215
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3355
235/-235
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.11
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
ANTISKID INOPERATIVE (Flaps 40)
VREF40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1765
90/-100
45/60
-80/275
55/-45
Autobrake Inoperative
Autobrake Inoperative
50/70
-95/335
80/-60
Autobrake Inoperative
Autobrake Inoperative
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1955
105/-115
Good To Medium Reported Braking Action
2200
130/-135
40/-40
60
115
265
45/-45
65
170
405
60/85
-120/430 135/-90
Autobrake Inoperative
Autobrake Inoperative
55/-55
75
265
680
70/100
-140/520 185/-120
Autobrake Inoperative
Autobrake Inoperative
60/-65
80
355
950
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
Good Reported Braking Action
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2440
150/-155
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
185/-190
d
2815
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
85/125
-185/740 380/-200
Autobrake Inoperative
Autobrake Inoperative
65/-80
85
610 1905
100/145
-230/960 575/-275
Autobrake Inoperative
Autobrake Inoperative
70/-95
85
860 2860
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3190
220/-225
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.12
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Jammed or Restricted Flight Controls (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1155
1460
2510
70/-60
65/-75
155/-170
75/-80
85/-90
155/-170
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/125
-45/155
-105/355
10/-10
5/-5
35/-50
20/-25
30/-30
70/-70
35
65
95
25
0
100
50
5
100
35/50
40/55
75/100
-60/205
-60/215
-105/355
35/-30
30/-25
35/-50
35/-35
35/-35
70/-70
50
55
95
80
90
100
185
205
100
-80/275
-80/280
-110/380
60/-50
55/-45
50/-60
45/-45
45/-45
70/-70
60
65
95
155
160
120
370
380
190
-95/340
-95/345
-100/355
85/-65
80/-65
60/-40
50/-55
50/-55
55/-60
65
75
100
225
225
145
550
555
465
75/100
75/100
75/105
-120/440
-120/445
-125/450
145/-100
145/-100
130/-80
60/-65
60/-65
65/-70
70
80
100
350
350
310
930
930
890
85/120
85/120
85/120
-145/540
-145/540
-145/540
205/-135
205/-135
200/-120
70/-75
70/-75
70/-75
75
80
95
475 1310
475 1305
475 1310
ad
ed
1530
1635
2510
REVERSE
THRUST
ADJ
25/30
30/40
75/100
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1790
1860
2540
100/-105
105/-110
160/-175
50/65
50/70
75/100
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2050
2085
2205
125/-130
125/-130
125/-135
60/80
60/80
60/85
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
155/-155
155/-155
155/-160
d
2340
2360
2430
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2630
2630
2650
180/-180
180/-180
180/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.13
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LEADING EDGE FLAPS TRANSIT (Flaps 15)
VREF15 + 15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1280
1650
2875
80/-70
70/-80
175/-190
25/35
35/45
90/115
-40/135
-50/170
-115/385
15/-15
5/-5
50/-60
85/-95
90/-100
175/-190
45/60
45/60
90/115
-65/220
-65/230
-115/385
35
65
100
30
0
155
70
5
160
40/-35
35/-30
50/-60
40/-40
45/-45
85/-85
50
60
100
105
115
160
240
260
160
60/80
60/80
90/120
-85/295
-85/300
-120/410
70/-55
65/-50
65/-70
50/-50
55/-55
85/-85
60
70
100
190
200
185
470
480
270
70/95
70/95
75/100
-100/365
-105/365
-110/380
95/-75
90/-70
65/-45
60/-60
60/-65
70/-70
70
75
110
275
280
175
695
700
570
85/120
85/120
90/120
-130/470
-130/470
-135/475
160/-115
160/-115
140/-90
70/-75
70/-75
75/-80
75
80
105
430 1160
430 1160
370 1095
100/140
100/140
100/140
-155/570
-155/570
-155/570
225/-150
230/-155
215/-130
80/-85
80/-85
80/-85
80
85
100
580 1620
575 1615
565 1615
Good To Medium Reported Braking Action
2020
2100
2910
115/-120
115/-125
180/-195
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1720
1840
2880
REVERSE
THRUST
ADJ
25/-25
40/-40
85/-85
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2320
2360
2525
140/-145
140/-150
140/-150
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
170/-175
170/-180
170/-175
d
2650
2670
2765
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2975
2975
3005
200/-205
200/-205
200/-200
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.14
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM A (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1270
1450
2615
70/-65
65/-75
150/-175
95/-100
95/-105
150/-175
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-40/135
-45/155
-110/365
15/-15
0/0
0/-10
25/-25
30/-30
75/-75
45
60
140
35
0
0
60
10
0
45/60
45/65
75/95
-70/235
-70/235
-110/365
50/-40
40/-35
0/-10
40/-45
45/-45
75/-75
70
75
140
135
135
0
275
275
0
-90/310
-90/310
-115/390
85/-65
80/-65
30/-25
50/-55
55/-55
75/-75
80
85
140
245
240
55
560
555
270
-110/380
-105/380
-105/380
115/-90
120/-95
120/-85
60/-65
60/-65
60/-65
90
90
90
350
345
345
840
830
830
90/125
90/125
90/125
-135/485
-135/485
-135/485
190/-135
195/-140
195/-135
70/-75
70/-75
70/-75
100
100
100
530 1435
530 1430
530 1430
105/145
105/150
105/150
-160/590
-160/590
-160/590
265/-175
265/-180
265/-180
80/-85
80/-85
80/-85
105
105
105
710 2025
710 2025
710 2025
ad
ed
1770
1780
2615
REVERSE
THRUST
ADJ
25/35
30/40
75/95
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
2080
2075
2655
125/-130
125/-130
155/-175
60/80
60/85
75/100
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2385
2370
2370
150/-155
150/-155
150/-155
75/100
75/100
75/100
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
185/-185
185/-185
185/-185
d
2720
2710
2710
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3055
3050
3050
215/-215
215/-215
215/-215
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.15
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM A (Flaps 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1210
1365
2410
65/-55
60/-65
135/-155
25/35
30/35
65/85
-40/130
-45/145
-105/350
15/-15
0/0
0/-10
85/-95
90/-95
135/-155
45/60
45/60
65/85
-65/225
-65/230
-105/350
45
55
135
30
10
0
50
15
0
45/-40
40/-35
0/-10
40/-40
40/-40
70/-70
70
75
135
120
120
0
240
240
0
55/75
60/75
70/90
-85/300
-85/300
-110/375
80/-65
80/-65
30/-25
50/-50
50/-50
70/-70
80
85
135
215
210
55
475
475
235
65/90
70/90
70/90
-105/370
-105/370
-105/370
110/-85
115/-90
115/-80
55/-60
55/-60
55/-60
85
90
90
305
300
300
710
705
705
80/110
85/115
85/115
-130/470
-130/470
-130/470
180/-125
185/-130
185/-125
65/-70
65/-70
65/-70
95
95
95
455 1180
455 1180
455 1180
95/130
95/135
95/135
-155/570
-155/570
-155/570
250/-165
250/-165
250/-165
75/-80
75/-80
75/-80
100
100
100
605 1650
605 1650
605 1650
Good To Medium Reported Braking Action
1965
1970
2450
110/-120
115/-120
140/-155
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1685
1700
2410
REVERSE
THRUST
ADJ
25/-25
30/-30
70/-70
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2240
2235
2235
135/-140
135/-140
135/-140
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
165/-170
165/-170
165/-170
d
2545
2540
2540
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2845
2845
2845
195/-195
195/-195
195/-195
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.16
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM A (Flaps 40)
VREF40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1165
1290
2225
60/-55
55/-60
125/-140
80/-90
85/-90
125/-140
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/125
-40/140
-100/335
15/-15
5/0
0/-5
25/-25
25/-25
60/-60
50
55
130
30
10
0
45
20
0
40/55
40/55
60/80
-65/225
-65/225
-100/335
45/-40
40/-35
0/-5
35/-40
40/-40
60/-60
70
75
130
105
105
0
210
210
0
-85/295
-85/295
-105/360
75/-65
75/-60
30/-20
45/-50
50/-50
60/-65
80
80
130
185
185
55
415
415
220
-100/360
-100/360
-100/360
105/-85
110/-85
110/-80
55/-55
55/-55
55/-55
85
85
90
265
265
265
615
615
615
75/105
75/105
75/105
-125/460
-125/460
-125/460
175/-120
180/-125
180/-120
65/-65
65/-65
65/-65
90
90
95
395 1010
400 1010
400 1010
85/120
90/125
90/125
-150/560
-150/560
-150/560
240/-155
245/-160
245/-160
70/-75
70/-75
70/-75
95
95
95
525 1400
530 1405
530 1405
ad
ed
1610
1620
2225
REVERSE
THRUST
ADJ
25/30
25/35
60/80
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1865
1870
2265
105/-115
105/-115
125/-145
50/70
50/70
60/85
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2120
2120
2120
125/-135
125/-135
125/-135
60/85
60/85
60/85
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
155/-160
155/-160
155/-160
d
2400
2400
2400
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2675
2680
2680
180/-185
180/-185
180/-185
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.17
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM A AND SYSTEM B (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1720
80/-90
40/50
-60/195
35/-35
Autobrake Inoperative
Autobrake Inoperative
65/90
-100/335 100/-80
Autobrake Inoperative
Autobrake Inoperative
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
2440
135/-145
Good To Medium Reported Braking Action
2815
170/-180
40/-40
75
-10
65
60/-60
105
95
440
930
85/115
-125/430 160/-120
Autobrake Inoperative
Autobrake Inoperative
70/-75
115
230
100/140
-150/525 215/-160
Autobrake Inoperative
Autobrake Inoperative
80/-85
120
365 1415
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
Good Reported Braking Action
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
3185
200/-210
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
240/-245
d
3555
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
120/165
-180/655 345/-215
Autobrake Inoperative
Autobrake Inoperative
90/-100
125
590 2400
135/190
-210/785 475/-270
Autobrake Inoperative
Autobrake Inoperative
100/-110
130
815 3380
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3920
275/-275
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.18
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM B (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1290
55/-60
95/-100
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-45/145
20/-15
Autobrake Inoperative
Autobrake Inoperative
25/-25
40
40
70
45/65
-75/255
50/-45
Autobrake Inoperative
Autobrake Inoperative
45/-45
60
140
285
-95/335
90/-70
Autobrake Inoperative
Autobrake Inoperative
55/-55
70
240
550
-115/410 125/-95
Autobrake Inoperative
Autobrake Inoperative
60/-65
75
340
815
ad
ed
1780
REVERSE
THRUST
ADJ
25/35
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
2075
125/-130
60/85
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2365
150/-155
70/100
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
180/-185
d
2675
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
85/120
-145/525 210/-140
Autobrake Inoperative
Autobrake Inoperative
70/-75
85
505 1345
100/140
-170/640 295/-180
Autobrake Inoperative
Autobrake Inoperative
75/-85
90
665 1870
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2985
210/-210
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.19
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
MANUAL REVERSION (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1720
80/-90
40/50
-60/195
35/-35
Autobrake Inoperative
Autobrake Inoperative
65/90
-100/335 100/-80
Autobrake Inoperative
Autobrake Inoperative
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
2440
135/-145
Good To Medium Reported Braking Action
2815
170/-180
40/-40
75
-10
65
60/-60
105
95
440
930
85/115
-125/430 160/-120
Autobrake Inoperative
Autobrake Inoperative
70/-75
115
230
100/140
-150/525 215/-160
Autobrake Inoperative
Autobrake Inoperative
80/-85
120
365 1415
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
Good Reported Braking Action
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
3185
200/-210
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
240/-245
d
3555
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
120/165
-180/655 345/-215
Autobrake Inoperative
Autobrake Inoperative
90/-100
125
590 2400
135/190
-210/785 475/-270
Autobrake Inoperative
Autobrake Inoperative
100/-110
130
815 3380
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3920
275/-275
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.20
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
One Engine Inoperative Landing (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1170
1450
2600
75/-65
70/-75
150/-170
80/-85
85/-95
150/-170
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/130
-45/155
-110/365
15/-10
0/0
10/-25
25/-25
30/-30
75/-75
35
60
120
0
0
0
25
0
0
40/50
40/55
75/95
-65/215
-65/225
-110/365
40/-35
35/-30
10/-25
40/-40
40/-40
75/-75
50
60
120
0
0
0
100
110
0
-85/295
-85/300
-115/395
75/-60
70/-55
35/-40
50/-50
50/-50
75/-75
60
70
120
0
0
0
205
215
65
-105/370
-105/375
-105/380
110/-85
105/-80
90/-65
60/-60
60/-60
60/-65
70
80
100
0
0
0
310
315
295
80/110
80/110
80/110
-135/490
-135/490
-135/495
200/-135
200/-135
185/-125
75/-75
75/-75
75/-75
80
90
100
0
0
0
540
540
535
95/130
95/130
95/130
-165/605
-165/605
-165/610
290/-185
290/-185
280/-180
85/-85
85/-85
85/-85
90
95
100
0
0
0
765
765
775
ad
ed
1590
1695
2600
REVERSE
THRUST
ADJ
25/30
30/40
75/95
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1910
1980
2640
110/-115
110/-120
155/-175
55/70
55/70
75/100
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2225
2265
2315
135/-140
135/-145
135/-150
65/85
65/85
65/85
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
170/-175
170/-180
170/-180
d
2615
2635
2670
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3000
3000
3025
200/-210
200/-210
205/-210
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.21
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
One Engine Inoperative Landing (Flaps 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1120
1365
2390
60/-55
60/-65
135/-150
20/30
30/35
65/85
-35/125
-45/150
-105/350
15/-10
0/0
10/-25
75/-80
80/-90
135/-150
35/50
40/50
65/85
-60/210
-65/220
-105/350
35
55
110
0
0
0
25
0
0
35/-30
35/-30
10/-25
35/-35
35/-40
65/-65
50
60
110
0
0
0
90
100
0
50/65
50/65
70/90
-80/285
-85/295
-110/375
70/-55
65/-55
35/-40
45/-45
45/-50
70/-70
60
70
110
0
0
0
180
185
55
60/80
60/80
60/80
-100/360
-100/365
-105/365
105/-80
95/-75
90/-65
55/-55
55/-55
55/-60
70
80
90
0
0
0
265
270
260
75/100
75/100
75/100
-130/475
-130/475
-135/475
185/-125
185/-120
175/-120
65/-70
65/-70
65/-70
80
85
90
0
0
0
450
455
450
85/115
85/115
90/120
-155/585
-155/585
-160/585
265/-170
270/-165
260/-170
75/-80
75/-80
75/-80
85
90
90
0
0
0
635
635
640
Good To Medium Reported Braking Action
1805
1870
2430
100/-105
105/-115
140/-155
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1520
1615
2390
REVERSE
THRUST
ADJ
20/-20
30/-30
65/-65
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2090
2125
2165
120/-130
125/-135
125/-135
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
150/-160
155/-165
155/-165
d
2435
2450
2485
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2775
2775
2805
180/-190
180/-190
185/-190
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.22
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Stabilizer Trim Inoperative (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1155
1460
2510
70/-60
65/-75
155/-170
75/-80
85/-90
155/-170
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/125
-45/155
-105/355
10/-10
5/-5
35/-50
20/-25
30/-30
70/-70
35
65
95
25
0
100
50
5
100
35/50
40/55
75/100
-60/205
-60/215
-105/355
35/-30
30/-25
35/-50
35/-35
35/-35
70/-70
50
55
95
80
90
100
185
205
100
-80/275
-80/280
-110/380
60/-50
55/-45
50/-60
45/-45
45/-45
70/-70
60
65
95
155
160
120
370
380
190
-95/340
-95/345
-100/355
85/-65
80/-65
60/-40
50/-55
50/-55
55/-60
65
75
100
225
225
145
550
555
465
75/100
75/100
75/105
-120/440
-120/445
-125/450
145/-100
145/-100
130/-80
60/-65
60/-65
65/-70
70
80
100
350
350
310
930
930
890
85/120
85/120
85/120
-145/540
-145/540
-145/540
205/-135
205/-135
200/-120
70/-75
70/-75
70/-75
75
80
95
475 1310
475 1305
475 1310
ad
ed
1530
1635
2510
REVERSE
THRUST
ADJ
25/30
30/40
75/100
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1790
1860
2540
100/-105
105/-110
160/-175
50/65
50/70
75/100
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2050
2085
2205
125/-130
125/-130
125/-135
60/80
60/80
60/85
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
155/-155
155/-155
155/-160
d
2340
2360
2430
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2630
2630
2650
180/-180
180/-180
180/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.23
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Asymmetry (1 ≤ Flap Lever <15)
VREF40 + 30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1260
1660
2880
90/-65
70/-75
165/-185
25/40
35/45
90/115
-40/135
-50/170
-115/385
15/-15
5/-5
55/-60
80/-85
80/-90
160/-185
40/55
45/60
90/115
-60/215
-65/225
-115/385
35
65
100
30
0
165
60
5
175
35/-30
30/-25
55/-65
40/-40
45/-45
85/-85
45
65
95
90
95
165
210
225
175
55/75
60/80
90/120
-80/290
-85/295
-120/410
65/-55
60/-50
70/-75
50/-50
55/-55
85/-85
55
70
95
175
180
190
420
435
270
70/90
70/95
70/95
-100/360
-100/360
-110/380
90/-75
85/-70
60/-45
60/-60
60/-60
70/-70
65
75
110
255
260
150
625
640
470
85/115
85/115
85/115
-125/465
-125/465
-135/475
155/-115
155/-110
135/-90
70/-75
70/-75
75/-80
75
80
110
400 1070
400 1070
340 985
100/135
100/135
100/135
-150/565
-150/565
-155/570
220/-150
220/-145
205/-130
80/-85
80/-85
80/-85
80
85
105
545 1510
540 1500
525 1495
Good To Medium Reported Braking Action
1975
2075
2915
105/-110
105/-115
165/-190
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1675
1815
2885
REVERSE
THRUST
ADJ
25/-25
40/-40
85/-85
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2275
2330
2535
125/-135
130/-140
125/-140
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
160/-165
160/-170
155/-165
d
2610
2635
2765
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2945
2940
2995
190/-195
185/-195
185/-190
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.24
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Asymmetry (Flap Lever 15 or 25)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1155
1460
2510
70/-60
65/-75
155/-170
75/-80
85/-90
155/-170
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/125
-45/155
-105/355
10/-10
5/-5
35/-50
20/-25
30/-30
70/-70
35
65
95
25
0
100
50
5
100
35/50
40/55
75/100
-60/205
-60/215
-105/355
35/-30
30/-25
35/-50
35/-35
35/-35
70/-70
50
55
95
80
90
100
185
205
100
-80/275
-80/280
-110/380
60/-50
55/-45
50/-60
45/-45
45/-45
70/-70
60
65
95
155
160
120
370
380
190
-95/340
-95/345
-100/355
85/-65
80/-65
60/-40
50/-55
50/-55
55/-60
65
75
100
225
225
145
550
555
465
75/100
75/100
75/105
-120/440
-120/445
-125/450
145/-100
145/-100
130/-80
60/-65
60/-65
65/-70
70
80
100
350
350
310
930
930
890
85/120
85/120
85/120
-145/540
-145/540
-145/540
205/-135
205/-135
200/-120
70/-75
70/-75
70/-75
75
80
95
475 1310
475 1305
475 1310
ad
ed
1530
1635
2510
REVERSE
THRUST
ADJ
25/30
30/40
75/100
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1790
1860
2540
100/-105
105/-110
160/-175
50/65
50/70
75/100
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2050
2085
2205
125/-130
125/-130
125/-135
60/80
60/80
60/85
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
155/-155
155/-155
155/-160
d
2340
2360
2430
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2630
2630
2650
180/-180
180/-180
180/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.25
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Asymmetry (Flap Lever 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1110
1365
2315
55/-55
60/-65
140/-150
20/30
30/35
65/90
-35/120
-45/150
-100/340
10/-10
5/0
30/-45
70/-75
75/-85
140/-150
35/45
35/50
65/90
-60/200
-60/210
-100/340
35
60
90
20
0
85
45
5
85
30/-30
30/-25
35/-45
35/-35
35/-35
65/-65
50
60
90
75
80
85
165
185
85
45/60
45/65
70/90
-75/265
-80/275
-105/365
55/-50
55/-45
50/-55
45/-45
45/-45
65/-65
60
65
90
135
140
105
325
335
170
55/75
55/75
55/75
-90/330
-95/335
-95/345
80/-65
75/-60
60/-40
50/-50
50/-50
50/-55
65
70
95
195
200
140
480
480
425
70/90
70/95
70/95
-115/430
-120/430
-120/435
140/-95
135/-95
125/-80
55/-60
60/-60
60/-65
70
75
95
305
305
275
790
790
770
80/105
80/110
80/110
-140/525
-140/525
-140/525
195/-125
195/-130
190/-115
60/-65
65/-70
65/-70
75
75
90
410 1100
410 1100
410 1110
Good To Medium Reported Braking Action
1705
1765
2345
95/-100
95/-105
140/-155
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1465
1560
2315
REVERSE
THRUST
ADJ
20/-20
30/-30
65/-65
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
1940
1970
2060
115/-120
115/-120
115/-125
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
140/-145
140/-145
140/-145
d
2205
2220
2275
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2465
2470
2485
160/-165
165/-165
165/-165
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.26
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Disagree (1 ≤ Indicated Flaps <15)
VREF40 + 30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1260
1660
2880
90/-65
70/-75
165/-185
80/-85
80/-90
160/-185
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-40/135
-50/170
-115/385
15/-15
5/-5
55/-60
25/-25
40/-40
85/-85
35
65
100
30
0
165
60
5
175
40/55
45/60
90/115
-60/215
-65/225
-115/385
35/-30
30/-25
55/-65
40/-40
45/-45
85/-85
45
65
95
90
95
165
210
225
175
-80/290
-85/295
-120/410
65/-55
60/-50
70/-75
50/-50
55/-55
85/-85
55
70
95
175
180
190
420
435
270
-100/360
-100/360
-110/380
90/-75
85/-70
60/-45
60/-60
60/-60
70/-70
65
75
110
255
260
150
625
640
470
85/115
85/115
85/115
-125/465
-125/465
-135/475
155/-115
155/-110
135/-90
70/-75
70/-75
75/-80
75
80
110
400 1070
400 1070
340 985
100/135
100/135
100/135
-150/565
-150/565
-155/570
220/-150
220/-145
205/-130
80/-85
80/-85
80/-85
80
85
105
545 1510
540 1500
525 1495
ad
ed
1675
1815
2885
REVERSE
THRUST
ADJ
25/40
35/45
90/115
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1975
2075
2915
105/-110
105/-115
165/-190
55/75
60/80
90/120
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2275
2330
2535
125/-135
130/-140
125/-140
70/90
70/95
70/95
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
160/-165
160/-170
155/-165
d
2610
2635
2765
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2945
2940
2995
190/-195
185/-195
185/-190
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.27
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Disagree (15 ≤ Indicated Flaps <30)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1155
1460
2510
70/-60
65/-75
155/-170
25/30
30/40
75/100
-35/125
-45/155
-105/355
10/-10
5/-5
35/-50
75/-80
85/-90
155/-170
35/50
40/55
75/100
-60/205
-60/215
-105/355
35
65
95
25
0
100
50
5
100
35/-30
30/-25
35/-50
35/-35
35/-35
70/-70
50
55
95
80
90
100
185
205
100
50/65
50/70
75/100
-80/275
-80/280
-110/380
60/-50
55/-45
50/-60
45/-45
45/-45
70/-70
60
65
95
155
160
120
370
380
190
60/80
60/80
60/85
-95/340
-95/345
-100/355
85/-65
80/-65
60/-40
50/-55
50/-55
55/-60
65
75
100
225
225
145
550
555
465
75/100
75/100
75/105
-120/440
-120/445
-125/450
145/-100
145/-100
130/-80
60/-65
60/-65
65/-70
70
80
100
350
350
310
930
930
890
85/120
85/120
85/120
-145/540
-145/540
-145/540
205/-135
205/-135
200/-120
70/-75
70/-75
70/-75
75
80
95
475 1310
475 1305
475 1310
Good To Medium Reported Braking Action
1790
1860
2540
100/-105
105/-110
160/-175
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1530
1635
2510
REVERSE
THRUST
ADJ
20/-25
30/-30
70/-70
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2050
2085
2205
125/-130
125/-130
125/-135
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
155/-155
155/-155
155/-160
d
2340
2360
2430
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2630
2630
2650
180/-180
180/-180
180/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.28
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Disagree (30 ≤ Indicated Flaps <40)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1110
1365
2315
55/-55
60/-65
140/-150
70/-75
75/-85
140/-150
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/120
-45/150
-100/340
10/-10
5/0
30/-45
20/-20
30/-30
65/-65
35
60
90
20
0
85
45
5
85
35/45
35/50
65/90
-60/200
-60/210
-100/340
30/-30
30/-25
35/-45
35/-35
35/-35
65/-65
50
60
90
75
80
85
165
185
85
-75/265
-80/275
-105/365
55/-50
55/-45
50/-55
45/-45
45/-45
65/-65
60
65
90
135
140
105
325
335
170
-90/330
-95/335
-95/345
80/-65
75/-60
60/-40
50/-50
50/-50
50/-55
65
70
95
195
200
140
480
480
425
70/90
70/95
70/95
-115/430
-120/430
-120/435
140/-95
135/-95
125/-80
55/-60
60/-60
60/-65
70
75
95
305
305
275
790
790
770
80/105
80/110
80/110
-140/525
-140/525
-140/525
195/-125
195/-130
190/-115
60/-65
65/-70
65/-70
75
75
90
410 1100
410 1100
410 1110
ad
ed
1465
1560
2315
REVERSE
THRUST
ADJ
20/30
30/35
65/90
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1705
1765
2345
95/-100
95/-105
140/-155
45/60
45/65
70/90
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
1940
1970
2060
115/-120
115/-120
115/-125
55/75
55/75
55/75
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
140/-145
140/-145
140/-145
d
2205
2220
2275
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2465
2470
2485
160/-165
165/-165
165/-165
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.29
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flaps Up Landing
VREF40 + 40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1335
1795
3120
110/-70
75/-80
175/-195
30/70
40/55
100/130
-40/140
-55/180
-120/400
15/-15
5/-5
65/-70
80/-90
85/-95
175/-195
45/60
50/65
100/130
-65/220
-70/235
-120/400
45
70
95
30
5
205
70
10
235
35/-30
25/-25
65/-70
40/-45
45/-50
90/-90
45
65
95
90
80
205
205
200
235
60/80
65/85
100/130
-85/295
-90/305
-125/425
65/-55
60/-50
80/-80
55/-55
55/-60
90/-90
55
70
95
175
175
225
415
425
325
70/95
75/100
80/105
-105/365
-105/370
-115/395
95/-75
90/-75
60/-55
65/-65
65/-65
75/-80
65
70
105
260
265
145
625
645
435
90/120
90/125
95/125
-130/475
-130/475
-140/490
165/-115
160/-115
135/-100
75/-80
75/-80
85/-90
75
80
105
415 1080
415 1085
335 965
105/145
105/145
105/145
-155/580
-155/580
-160/585
230/-155
230/-150
210/-140
85/-90
85/-90
90/-95
80
90
100
565 1530
560 1520
520 1495
Good To Medium Reported Braking Action
2080
2215
3145
110/-115
110/-120
180/-200
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1750
1945
3120
REVERSE
THRUST
ADJ
30/-30
40/-45
90/-90
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2405
2480
2755
135/-140
135/-145
135/-155
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
170/-175
165/-175
165/-180
d
2775
2815
2995
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3140
3145
3230
200/-205
195/-205
190/-205
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.30
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
Advisory
file
Highlight
Information
ADVISORY INFORMATION
Recommended Brake Cooling Schedule
Reference Brake Energy Per Brake (Millions of Foot Pounds)
180
10
67.3
69.5
70.5
71.4
73.2
74.8
76.3
59.7
61.6
62.5
63.4
64.9
66.2
67.4
51.8
53.6
54.4
55.1
56.5
57.5
58.3
44.1
45.5
46.2
46.8
48.0
48.8
49.3
36.4
37.6
38.2
38.7
39.7
40.2
40.6
0
60.8
62.8
63.7
64.6
66.2
67.5
68.7
54.9
56.7
57.5
58.3
59.8
60.9
61.8
48.1
49.7
50.4
51.1
52.3
53.2
53.9
40.9
42.2
42.8
43.4
44.5
45.2
45.7
33.7
34.8
35.3
35.8
36.7
37.2
37.5
5
69.6
71.9
72.9
73.9
75.7
77.4
79.0
62.7
64.8
65.7
66.5
68.2
69.6
70.9
54.8
56.6
57.4
58.2
59.6
60.7
61.7
46.4
48.0
48.7
49.3
50.6
51.4
52.1
38.2
39.5
40.0
40.6
41.6
42.2
42.6
10
81.2
83.9
85.1
86.2
88.4
90.5
92.9
72.9
75.4
76.4
77.4
79.4
81.2
83.0
63.5
65.6
66.5
67.4
69.1
70.5
71.9
53.6
55.4
56.2
56.9
58.4
59.4
60.3
43.9
45.4
46.0
46.6
47.8
48.6
49.1
or
pr
in
te
d
0
22.4
23.1
23.5
23.8
24.4
24.7
24.8
20.2
20.8
21.1
21.4
22.0
22.2
22.3
18.0
18.5
18.8
19.1
19.6
19.8
19.8
15.7
16.3
16.5
16.7
17.2
17.3
17.3
13.5
14.0
14.2
14.4
14.8
14.9
14.9
do
w
nl
o
10
19.3
20.0
20.2
20.5
21.1
21.3
21.3
17.5
18.1
18.4
18.6
19.1
19.3
19.3
15.7
16.3
16.5
16.7
17.2
17.3
17.3
14.0
14.4
14.7
14.9
15.2
15.4
15.4
12.3
12.7
12.9
13.1
13.4
13.5
13.5
if
5
17.0
17.6
17.8
18.1
18.5
18.7
18.7
15.4
15.9
16.2
16.4
16.8
17.0
17.0
13.9
14.3
14.6
14.8
15.1
15.3
15.3
12.3
12.7
12.9
13.1
13.4
13.6
13.6
10.8
11.2
11.4
11.5
11.8
11.9
11.9
d
0
15.1
15.6
15.8
16.0
16.4
16.6
16.6
13.7
14.2
14.4
14.6
14.9
15.1
15.1
12.3
12.7
12.9
13.1
13.4
13.6
13.5
11.0
11.3
11.5
11.6
11.9
12.1
12.0
9.6
10.0
10.1
10.2
10.5
10.6
10.6
nc
on
tro
lle
WEIGHT OAT
(1000 KG) (°C)
0
10
15
80
20
30
40
50
0
10
15
70
20
30
40
50
0
10
15
60
20
30
40
50
0
10
15
50
20
30
40
50
0
10
15
40
20
30
40
50
WIND CORRECTED BRAKES ON SPEED (KIAS)*
100
120
140
160
PRESSURE ALTITUDE (1000 FT)
5 10 0
5 10 0
5 10 0
5
25.3 28.9 30.9 35.0 40.2 40.4 45.9 53.0 50.8 57.9
26.1 29.8 31.9 36.2 41.5 41.8 47.5 54.8 52.5 59.9
26.5 30.3 32.4 36.7 42.1 42.4 48.2 55.6 53.3 60.7
26.9 30.7 32.8 37.2 42.7 42.9 48.8 56.3 54.0 61.5
27.6 31.5 33.7 38.2 43.8 44.0 50.0 57.7 55.3 63.1
27.9 31.9 34.1 38.7 44.4 44.7 50.9 58.8 56.3 64.3
28.0 32.1 34.3 39.0 44.9 45.2 51.5 59.7 57.1 65.4
22.8 26.0 27.7 31.3 35.9 36.1 41.0 47.2 45.3 51.6
23.5 26.8 28.6 32.4 37.1 37.3 42.3 48.7 46.8 53.3
23.9 27.2 29.0 32.8 37.6 37.8 43.0 49.4 47.5 54.0
24.2 27.6 29.4 33.3 38.1 38.4 43.5 50.1 48.1 54.8
24.8 28.3 30.2 34.1 39.1 39.3 44.6 51.4 49.3 56.1
25.1 28.6 30.5 34.6 39.6 39.9 45.3 52.2 50.1 57.1
25.2 28.8 30.7 34.8 40.0 40.2 45.8 52.9 50.7 58.0
20.3 23.1 24.4 27.6 31.6 31.7 35.9 41.2 39.6 45.0
20.9 23.8 25.2 28.5 32.6 32.7 37.1 42.6 40.9 46.5
21.2 24.2 25.6 29.0 33.1 33.2 37.6 43.2 41.5 47.1
21.5 24.5 26.0 29.4 33.5 33.6 38.1 43.8 42.0 47.8
22.1 25.1 26.6 30.1 34.4 34.5 39.1 44.9 43.1 49.0
22.3 25.4 26.9 30.5 34.9 35.0 39.7 45.6 43.8 49.8
22.4 25.5 27.0 30.6 35.1 35.2 40.0 46.0 44.2 50.4
17.7 20.2 21.2 23.9 27.3 27.2 30.8 35.3 33.8 38.3
18.3 20.8 21.9 24.7 28.2 28.1 31.8 36.5 34.9 39.6
18.6 21.1 22.2 25.1 28.6 28.6 32.3 37.0 35.4 40.2
18.9 21.4 22.5 25.4 29.0 28.9 32.8 37.5 35.9 40.7
19.3 22.0 23.1 26.1 29.7 29.7 33.6 38.4 36.8 41.8
19.5 22.2 23.4 26.4 30.1 30.1 34.0 39.0 37.4 42.4
19.6 22.3 23.4 26.5 30.3 30.2 34.2 39.3 37.6 42.8
15.2 17.3 17.9 20.2 23.0 22.8 25.8 29.4 28.1 31.8
15.8 17.9 18.5 20.9 23.8 23.6 26.6 30.4 29.0 32.8
16.0 18.1 18.8 21.2 24.1 23.9 27.0 30.8 29.4 33.3
16.2 18.4 19.1 21.5 24.5 24.2 27.4 31.3 29.8 33.8
16.6 18.9 19.6 22.1 25.1 24.9 28.1 32.1 30.6 34.6
16.8 19.1 19.8 22.3 25.4 25.2 28.4 32.5 31.0 35.1
16.8 19.1 19.8 22.3 25.5 25.2 28.6 32.7 31.1 35.3
ad
ed
80
U
*To correct for wind, enter table with the brakes on speed minus one half the headwind or plus 1.5 times the
tailwind. If ground speed is used for brakes on speed, ignore wind and enter table with sea level, 15°C.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.11.31
Performance Inflight - QRH
Advisory Information
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ADVISORY INFORMATION
Recommended Brake Cooling Schedule
Adjusted Brake Energy Per Brake (Millions of Foot Pounds)
No Reverse Thrust
REFERENCE BRAKE ENERGY PER BRAKE (MILLIONS OF FOOT POUNDS)
10
20
30
40
50
60
70
80
90
10
20
30
40
50
60
70
80
90
7.8
16.3
25.3
34.7
44.7
55.0
65.7
76.6
87.9
7.5
15.4
23.6
32.4
41.8
51.8
62.5
74.1
86.5
7.3
14.7
22.3
30.2
38.6
47.6
57.4
68.1
80.0
7.0
13.8
20.5
27.4
34.8
42.7
51.5
61.3
72.4
6.7
13.1
19.2
25.3
31.8
38.8
46.6
55.4
65.5
or
pr
in
te
d
LANDING
EVENT
RTO MAX MAN
MAX MAN
MAX AUTO
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
Two Engine Detent Reverse Thrust
REFERENCE BRAKE ENERGY PER BRAKE (MILLIONS OF FOOT POUNDS)
10
20
30
40
50
60
70
80
90
10
20
30
40
50
60
70
80
90
7.0
14.6
22.8
31.4
40.5
49.9
59.7
69.8
80.0
5.8
12.3
19.5
27.2
35.6
44.5
53.9
63.7
74.1
4.3
9.2
14.7
20.7
27.2
34.4
42.0
50.2
59.0
2.5
5.6
9.1
13.1
17.8
23.0
28.8
35.2
42.3
1.8
3.8
6.1
8.8
11.9
15.5
19.6
24.4
29.8
ad
ed
LANDING
EVENT
RTO MAX MAN
MAX MAN
MAX AUTO
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
EVENT ADJUSTED BRAKE ENERGY (MILLIONS OF FOOT POUNDS)
16 & BELOW
17
20
23
25
28
32
33 TO 48
49 & ABOVE
BRAKE TEMPERATURE MONITOR SYSTEM INDICATION ON CDS
UP TO 2.4
2.6
3.1
3.5
3.9
4.4
4.9
5.0 TO 7.5
7.5 & ABOVE
NO SPECIAL
1
2
3
4
5
6
FUSE PLUG
PROCEDURE
CAUTION
MELT ZONE
REQUIRED
10
20
30
40
50
60
if
INFLIGHT
GEAR DOWN
GROUND
do
w
nl
o
Cooling Time (Minutes) - Category C Steel Brakes
Cooling Time (Minutes) - Category N Carbon Brakes
on
tro
lle
d
EVENT ADJUSTED BRAKE ENERGY (MILLIONS OF FOOT POUNDS)
16 & BELOW
17
19
20.9 23.5 26.9 29.4
30 TO 41
41 & ABOVE
BRAKE TEMPERATURE MONITOR SYSTEM INDICATION ON CDS
UP TO 2.5
2.6
3
3.3
3.8
4.5
4.9
5.0 TO 7.1
7.1 & ABOVE
NO SPECIAL
1
4
5
6
7
7.6
FUSE PLUG
PROCEDURE
CAUTION
MELT ZONE
REQUIRED
6.7
16.0 24.1 34.2 45.9 53.3
INFLIGHT
GEAR DOWN
GROUND
U
nc
Observe maximum quick turnaround limit.
Table shows energy per brake added by a single stop with all brakes operating. Energy is assumed to be
equally distributed among the operating brakes. Total energy is the sum of residual energy plus energy
added.
Add 1.0 million foot pounds per brake for each taxi mile.
When in caution zone, wheel fuse plugs may melt. Delay takeoff and inspect after one hour. If overheat occurs
after takeoff, extend gear soon for at least 7 minutes.
When in fuse plug melt zone, clear runway immediately. Unless required, do not set parking brake. Do not
approach gear or attempt to taxi for one hour. Tire, wheel and brake replacement may be required. If
overheat occurs after takeoff, extend gear soon for at least 12 minutes.
Brake temperature monitor system (BTMS) indication on CDS systems page may be used 10 to 15 minutes
after airplane has come to a complete stop or inflight with gear retracted to determine recommended cooling
schedule.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.11.32
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Engine Inoperative
Section 12
Engine
file
Highlight
Inoperative
ENGINE INOP
Engine Inoperative
Engine Inoperative
Initial Max Continuous %N1
Based on .79M, A/C high and anti-ice off
27
95.9
96.5
97.2
97.9
98.1
97.3
96.5
95.8
95.0
94.2
93.4
92.6
91.8
29
95.6
96.2
96.8
97.6
98.5
98.5
97.7
96.9
96.2
95.4
94.6
93.7
92.9
PRESSURE ALTITUDE (1000 FT)
31
33
35
37
95.5
95.2
94.8
94.3
96.1
96.0
95.5
95.1
96.7
96.7
96.2
95.8
97.4
97.4
97.0
96.6
98.3
98.2
97.8
97.5
99.2
99.1
98.6
98.3
99.0
99.9
99.5
99.2
98.2
99.5
100.4
100.1
97.4
98.7
99.8
100.4
96.6
97.9
99.0
99.6
95.8
97.0
98.2
98.7
94.9
96.2
97.3
97.9
94.1
95.3
96.5
97.0
25
-1.2
-4.2
41
93.2
94.1
95.0
95.9
96.8
97.8
98.7
99.7
100.0
99.2
98.3
97.5
96.6
27
-1.1
-4.4
PRESSURE ALTITUDE (1000 FT)
29
31
33
35
37
-1.0
-0.9
-0.8
-0.8
-0.8
-4.5
-4.7
-5.0
-4.8
-4.8
39
-0.8
-4.8
41
-0.8
-4.8
U
nc
on
tro
lle
d
if
ENGINE ANTI-ICE
ENGINE & WING ANTI-ICE
do
w
nl
o
%N1 Adjustments for Engine Bleeds
BLEED CONFIGURATION
39
94.0
94.8
95.6
96.4
97.2
98.1
99.0
99.9
100.2
99.4
98.5
97.7
96.8
or
pr
in
te
d
20
15
10
5
0
-5
-10
-15
-20
-25
-30
-35
-40
25
96.1
96.7
97.3
97.5
96.8
96.0
95.2
94.4
93.6
92.8
91.9
91.1
90.3
ad
ed
TAT (°C)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.12.1
Performance Inflight - QRH
Engine Inoperative
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ENGINE INOP
Max Continuous %N1
37000 FT to 29000 FT Pressure Altitudes
-35
99.6
98.9
98.0
97.2
-30
98.9
99.8
98.8
98.1
-50
96.8
96.4
95.3
94.0
-45
97.7
97.3
96.2
94.9
-40
98.6
98.2
97.1
95.8
-35
99.5
99.1
98.0
96.6
-30
99.2
100.0
98.8
97.5
-45
97.7
97.3
96.2
94.5
93.9
-40
98.5
98.2
97.1
95.4
94.7
-35
99.4
99.1
97.9
96.2
95.6
-30
100.2
99.9
98.8
97.1
96.4
-25
99.3
100.8
99.6
97.9
97.2
-45
97.6
97.3
95.9
94.0
92.6
-40
98.5
98.2
96.8
94.9
93.5
-35
99.4
99.1
97.6
95.7
94.3
-30
100.3
100.0
98.5
96.6
95.1
-25
100.4
100.8
99.3
97.4
95.9
-40
98.4
97.8
96.5
94.4
92.3
92.3
-35
99.3
98.7
97.4
95.2
93.1
93.1
-30
100.1
99.5
98.2
96.1
93.9
93.9
-25
101.0
100.4
99.1
96.9
94.7
94.7
-20
100.5
101.2
99.9
97.7
95.5
95.5
TAT (°C)
-25
98.1
99.5
99.7
98.9
TAT (°C)
-25
98.4
99.9
99.6
98.3
TAT (°C)
-20
98.5
99.9
100.4
98.7
98.1
TAT (°C)
-20
99.5
101.0
100.2
98.2
96.7
TAT (°C)
-15
99.6
100.7
100.7
98.5
96.3
96.3
if
d
-20
96.9
98.7
100.1
99.7
-15
95.6
97.8
99.3
100.5
-10
94.0
96.8
98.5
100.2
-5
92.5
95.6
97.7
99.3
0
91.1
94.5
96.7
98.5
-15
96.1
98.0
99.5
99.9
-10
94.7
97.0
98.9
99.7
-5
93.3
95.8
98.0
98.9
0
92.0
94.7
97.0
98.1
-10
96.0
98.0
99.6
99.9
99.7
-5
94.6
96.8
98.7
99.1
100.4
0
93.2
95.6
97.7
98.2
100.0
5
92.0
94.5
96.7
97.4
99.2
-15
98.5
100.1
100.7
99.0
97.5
-10
97.3
99.1
99.9
99.8
98.3
-5
95.9
98.0
99.1
99.1
99.1
0
94.5
96.7
98.1
98.2
99.3
5
93.2
95.5
97.1
97.3
98.4
-10
98.5
99.7
100.4
99.3
97.0
97.0
-5
97.2
98.7
99.5
99.4
97.8
97.8
0
95.7
97.5
98.6
98.5
98.6
98.6
5
94.4
96.2
97.5
97.5
97.8
99.3
10
93.1
95.1
96.6
96.8
97.0
99.4
-20
97.3
98.9
100.2
99.1
-15
97.3
99.0
100.2
99.5
98.9
or
pr
in
te
d
-40
98.7
98.1
97.1
96.4
ad
ed
-45
97.9
97.2
96.2
95.5
do
w
nl
o
-50
97.0
96.3
95.3
94.6
on
tro
lle
37000 FT PRESS ALT
KIAS M
-55
160
.51
96.0
200
.63
95.4
240
.74
94.4
280
.86
93.7
35000 FT PRESS ALT
KIAS M
-55
160
.49
95.9
200
.60
95.5
240
.71
94.4
280
.82
93.2
33000 FT PRESS ALT
KIAS M
-50
160
.47
96.8
200
.58
96.4
240
.68
95.3
280
.79
93.6
320
.89
93.0
31000 FT PRESS ALT
KIAS M
-50
160
.45
96.7
200
.55
96.5
240
.66
95.0
280
.76
93.2
320
.85
91.8
29000 FT PRESS ALT
KIAS M
-45
160
.43
97.5
200
.53
96.9
240
.63
95.7
280
.73
93.6
320
.82
91.4
360
.91
91.4
%N1 Adjustments for Engine Bleeds
BLEED CONFIGURATION
PRESSURE ALTITUDE (1000 FT)
31
33
35
-0.9
-0.8
-0.8
-4.3
-4.5
-4.7
37
-0.8
-4.7
U
nc
ENGINE ANTI-ICE ON
ENGINE & WING ANTI-ICE ON
29
-0.9
-4.1
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.12.2
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Engine Inoperative
737 Flight Crew Operations Manual
ENGINE INOP
Max Continuous %N1
27000 FT to 20000 FT Pressure Altitudes
-30
100.0
98.9
97.6
95.5
93.4
92.7
-25
100.8
99.8
98.4
96.3
94.2
93.5
-20
101.5
100.6
99.2
97.1
95.0
94.3
-35
99.0
97.7
95.9
94.1
91.8
90.5
-30
99.9
98.5
96.8
94.9
92.6
91.3
-25
100.7
99.4
97.6
95.7
93.4
92.1
-20
101.6
100.2
98.4
96.5
94.2
93.0
-15
101.7
101.0
99.2
97.3
95.0
93.8
-35
98.5
97.2
95.6
93.8
91.4
89.8
-30
99.4
98.1
96.4
94.6
92.3
90.7
-25
100.3
98.9
97.2
95.4
93.1
91.5
-20
101.1
99.7
98.0
96.2
93.9
92.4
-30
98.4
97.1
95.6
94.0
91.8
89.9
-25
99.2
98.0
96.4
94.8
92.6
90.7
-20
100.1
98.8
97.2
95.6
93.4
91.6
-15
100.9
99.6
98.0
96.4
94.2
92.4
-10
101.0
100.4
98.8
97.1
95.0
93.2
-30
97.4
96.2
94.7
93.3
91.1
89.3
-25
98.2
97.0
95.5
94.1
92.0
90.2
-20
99.0
97.9
96.3
94.8
92.8
91.0
-15
99.8
98.7
97.1
95.6
93.6
91.8
-10
100.6
99.4
97.9
96.4
94.4
92.6
nc
TAT (°C)
-15
100.6
101.1
100.1
97.9
95.7
95.1
TAT (°C)
-10
100.7
100.9
100.0
98.1
95.8
94.6
TAT (°C)
-10
100.8
101.0
99.6
97.8
95.5
94.0
TAT (°C)
-5
99.9
100.1
99.6
97.9
95.8
94.0
TAT (°C)
-5
100.2
100.2
98.7
97.2
95.2
93.5
-15
101.9
100.6
98.8
97.0
94.7
93.2
do
w
nl
o
if
d
-10
99.6
100.2
100.7
98.7
96.5
95.9
-5
98.4
99.2
99.7
99.4
97.3
96.6
0
97.0
98.1
98.7
98.7
98.0
97.4
5
95.7
96.9
97.7
97.7
97.9
98.2
10
94.4
95.7
96.8
96.9
97.2
98.7
-5
99.6
99.9
99.8
98.8
96.6
95.4
0
98.4
98.9
98.9
98.9
97.3
96.2
5
97.0
97.7
97.9
97.9
97.9
97.0
10
95.8
96.6
96.9
96.9
97.2
97.7
15
94.5
95.5
96.0
96.2
96.5
97.5
-5
99.7
99.9
99.9
98.6
96.3
94.8
0
98.5
98.9
99.0
99.1
97.1
95.6
5
97.2
97.8
97.9
98.0
97.8
96.4
10
96.0
96.7
97.0
97.0
97.2
97.2
15
94.7
95.6
96.1
96.3
96.5
97.2
0
98.7
98.9
99.1
98.7
96.6
94.8
5
97.5
97.8
98.1
98.4
97.4
95.6
10
96.3
96.8
97.1
97.4
97.5
96.4
15
95.2
95.8
96.2
96.6
96.8
97.0
20
94.0
94.8
95.4
95.8
96.1
96.4
0
98.9
99.1
99.3
97.9
96.0
94.3
5
97.7
97.8
98.2
98.5
96.8
95.1
10
96.6
96.8
97.1
97.6
97.6
95.8
15
95.5
95.8
96.2
96.7
96.9
96.6
20
94.4
94.9
95.4
95.9
96.2
96.4
or
pr
in
te
d
-35
99.1
98.1
96.7
94.6
92.6
91.8
ad
ed
-40
98.2
97.2
95.9
93.8
91.7
91.0
on
tro
lle
27000 FT PRESS ALT
KIAS M
-45
160
.41
97.3
200
.51
96.3
240
.60
95.0
280
.70
93.0
320
.79
90.9
360
.88
90.2
25000 FT PRESS ALT
KIAS M
-40
160
.39
98.2
200
.49
96.8
240
.58
95.1
280
.67
93.2
320
.76
90.9
360
.85
89.6
24000 FT PRESS ALT
KIAS M
-40
160
.38
97.7
200
.48
96.4
240
.57
94.7
280
.66
93.0
320
.75
90.6
360
.83
89.0
22000 FT PRESS ALT
KIAS M
-35
160
.37
97.5
200
.46
96.3
240
.55
94.8
280
.63
93.2
320
.72
90.9
360
.80
89.0
20000 FT PRESS ALT
KIAS M
-35
160
.35
96.5
200
.44
95.4
240
.53
93.9
280
.61
92.4
320
.69
90.3
360
.77
88.5
U
%N1 Adjustments for Engine Bleeds
BLEED CONFIGURATION
ENGINE ANTI-ICE ON
ENGINE & WING ANTI-ICE ON
20
-0.9
-3.6
PRESSURE ALTITUDE (1000 FT)
22
24
25
-0.9
-1.0
-1.0
-3.8
-3.8
-3.9
27
-1.0
-4.0
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.12.3
Performance Inflight - QRH
Engine Inoperative
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ENGINE INOP
Max Continuous %N1
18000 FT to 12000 FT Pressure Altitudes
-15
98.4
97.5
96.0
94.5
92.8
91.2
-10
99.2
98.2
96.8
95.3
93.6
92.0
-5
100.0
99.0
97.6
96.1
94.4
92.8
-25
95.8
94.7
93.3
91.8
90.3
88.9
-20
96.6
95.5
94.1
92.6
91.1
89.7
-15
97.4
96.3
94.9
93.5
91.9
90.6
-10
98.2
97.1
95.7
94.3
92.8
91.4
-5
99.0
97.8
96.5
95.1
93.6
92.2
-20
95.7
94.4
92.9
91.7
90.4
89.1
-15
96.5
95.2
93.8
92.5
91.2
89.9
-10
97.3
96.0
94.6
93.4
92.1
90.7
-5
98.0
96.7
95.4
94.2
92.9
91.6
0
98.8
97.5
96.2
95.0
93.7
92.4
-15
95.6
93.5
92.5
91.4
90.3
89.1
-10
96.4
94.3
93.3
92.2
91.2
90.0
-5
97.1
95.1
94.1
93.0
92.0
90.8
0
97.9
95.9
94.9
93.8
92.8
91.6
5
98.6
96.7
95.7
94.6
93.6
92.4
TAT (°C)
0
98.9
99.3
98.3
96.8
95.2
93.6
TAT (°C)
0
99.4
98.6
97.2
95.9
94.4
93.0
TAT (°C)
5
99.2
98.3
96.9
95.8
94.5
93.2
TAT (°C)
10
97.9
97.1
96.4
95.4
94.4
93.2
do
w
nl
o
if
d
5
97.5
98.0
98.2
97.6
96.0
94.4
10
96.5
96.7
97.1
97.5
96.8
95.2
15
95.5
95.9
96.2
96.6
96.9
96.0
20
94.5
95.0
95.4
95.8
96.2
96.4
25
93.5
94.1
94.6
95.1
95.5
95.8
10
97.0
97.0
97.3
97.4
95.9
94.6
15
96.1
96.0
96.3
96.7
96.7
95.4
20
95.2
95.2
95.5
95.8
96.1
96.2
25
94.2
94.4
94.7
95.1
95.5
95.8
10
98.2
97.5
97.4
96.5
95.3
94.0
15
97.3
96.5
96.5
96.8
96.1
94.8
20
96.4
95.7
95.6
96.0
96.2
95.5
25
95.5
94.9
94.8
95.2
95.5
95.8
30
94.6
94.1
94.1
94.5
94.8
95.2
15
96.8
96.1
96.4
96.2
95.2
93.9
20
95.9
95.1
95.5
95.9
96.0
94.7
25
95.2
94.4
94.7
95.1
95.5
95.5
30
94.4
93.6
94.0
94.4
94.8
95.1
35
93.5
92.8
93.2
93.7
94.1
94.4
5
98.2
98.2
98.0
96.6
95.2
93.8
or
pr
in
te
d
-20
97.6
96.7
95.2
93.7
92.0
90.4
ad
ed
-25
96.8
95.9
94.5
92.9
91.1
89.5
on
tro
lle
18000 FT PRESS ALT
KIAS M
-30
160
.34
96.0
200
.42
95.1
240
.51
93.7
280
.59
92.0
320
.67
90.3
360
.75
88.7
16000 FT PRESS ALT
KIAS M
-30
160
.33
95.0
200
.41
93.9
240
.49
92.5
280
.57
91.0
320
.64
89.4
360
.72
88.0
14000 FT PRESS ALT
KIAS M
-25
160
.31
94.9
200
.39
93.6
240
.47
92.1
280
.54
90.9
320
.62
89.6
360
.69
88.3
12000 FT PRESS ALT
KIAS M
-20
160
.30
94.8
200
.38
92.7
240
.45
91.6
280
.52
90.6
320
.60
89.5
360
.67
88.3
%N1 Adjustments for Engine Bleeds
12
-0.9
-3.2
PRESSURE ALTITUDE (1000 FT)
14
16
-0.9
-0.9
-3.4
-3.4
18
-0.9
-3.5
U
nc
BLEED
CONFIGURATION
ENGINE ANTI-ICE ON
ENGINE & WING ANTI-ICE ON
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.12.4
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Engine Inoperative
737 Flight Crew Operations Manual
ENGINE INOP
Max Continuous %N1
10000 FT to 1000 FT Pressure Altitudes
-5
95.2
93.8
92.8
91.9
91.0
90.0
0
95.9
94.6
93.6
92.7
91.8
90.8
5
96.7
95.4
94.4
93.5
92.6
91.6
-5
91.4
90.8
90.0
89.3
88.6
87.7
0
92.2
91.6
90.8
90.1
89.4
88.5
5
93.0
92.4
91.6
90.9
90.2
89.3
10
93.8
93.2
92.4
91.7
90.9
90.1
15
94.5
93.9
93.2
92.5
91.7
90.8
0
91.3
90.7
89.6
89.1
88.4
87.6
5
92.1
91.5
90.4
89.9
89.2
88.4
10
92.8
92.3
91.2
90.6
90.0
89.1
15
93.6
93.1
92.0
91.4
90.7
89.9
0
89.8
89.5
88.6
88.1
87.5
86.7
5
90.6
90.3
89.4
88.8
88.2
87.5
10
91.4
91.0
90.2
89.6
89.0
88.2
15
92.2
91.8
90.9
90.4
89.8
89.0
TAT (°C)
10
97.5
96.1
95.2
94.3
93.4
92.3
TAT (°C)
20
95.1
94.7
93.9
93.3
92.5
91.6
TAT (°C)
25
94.6
94.6
93.5
92.9
92.2
91.4
TAT (°C)
25
93.7
93.3
92.5
91.9
91.3
90.5
20
94.4
93.8
92.7
92.2
91.5
90.6
do
w
nl
o
if
d
15
96.5
96.1
95.9
95.1
94.2
93.1
20
95.6
95.2
95.4
95.7
95.0
93.9
25
94.9
94.4
94.6
95.0
95.4
94.7
30
94.2
93.7
93.8
94.2
94.7
95.0
35
93.4
92.9
93.1
93.5
93.9
94.3
25
94.4
94.4
94.4
94.0
93.2
92.3
30
93.6
93.7
93.7
94.0
94.0
93.1
35
92.9
93.0
92.9
93.2
93.6
93.8
40
92.2
92.3
92.2
92.5
92.9
93.3
45
91.4
91.5
91.5
91.8
92.2
92.6
30
93.9
94.0
93.5
93.7
93.0
92.1
35
93.2
93.3
92.8
93.1
93.5
92.8
40
92.4
92.5
92.0
92.4
92.8
93.1
45
91.6
91.8
91.3
91.7
92.0
92.4
50
90.7
91.0
90.6
91.0
91.3
91.7
30
93.4
93.7
93.2
92.6
92.0
91.2
35
92.7
93.0
92.8
93.1
92.7
91.9
40
91.9
92.2
92.0
92.3
92.7
92.6
45
91.2
91.5
91.3
91.6
91.9
92.3
50
90.3
90.7
90.6
90.9
91.2
91.6
or
pr
in
te
d
-10
94.4
93.0
92.0
91.1
90.2
89.2
ad
ed
-15
93.5
92.1
91.1
90.3
89.4
88.3
on
tro
lle
10000 FT PRESS ALT
KIAS M
-20
160
.29
92.7
200
.36
91.3
240
.43
90.3
280
.51
89.5
320
.58
88.6
360
.65
87.5
5000 FT PRESS ALT
KIAS M
-10
160
.26
90.5
200
.33
90.0
240
.40
89.2
280
.46
88.5
320
.53
87.8
360
.59
86.9
3000 FT PRESS ALT
KIAS M
-5
160
.26
90.5
200
.32
89.9
240
.38
88.8
280
.45
88.3
320
.51
87.6
360
.57
86.8
1000 FT PRESS ALT
KIAS M
-5
160
.25
89.0
200
.31
88.7
240
.37
87.8
280
.43
87.3
320
.49
86.7
360
.55
85.9
20
92.9
92.6
91.7
91.1
90.5
89.7
%N1 Adjustments for Engine Bleeds
1
-0.6
-2.9
PRESSURE ALTITUDE (1000 FT)
3
5
-0.8
-0.8
-3.0
-2.7
10
-0.8
-3.2
U
nc
BLEED
CONFIGURATION
ENGINE ANTI-ICE ON
ENGINE & WING ANTI-ICE ON
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.12.5
Performance Inflight - QRH
Engine Inoperative
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ENGINE INOP
MAX CONTINUOUS THRUST
Driftdown Speed/Level Off Altitude
100 ft/min residual rate of climb
OPTIMUM
DRIFTDOWN
SPEED (KIAS)
269
262
254
246
238
229
219
209
199
187
U
nc
on
tro
lle
d
if
do
w
nl
o
ad
ed
Includes APU fuel burn.
LEVEL OFF ALTITUDE (FT)
ISA + 10°C
ISA + 15°C
ISA + 20°C
& BELOW
16300
14700
12300
18400
16800
14900
20400
19000
17300
22500
21200
19700
24700
23500
22100
26800
25800
24600
29100
28100
27000
31200
30400
29400
33300
32600
31700
35600
34900
34000
or
pr
in
te
d
WEIGHT (1000 KG)
START
LEVEL OFF
DRIFTDOWN
85
81
80
76
75
72
70
67
65
62
60
57
55
53
50
48
45
43
40
38
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.12.6
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Engine Inoperative
737 Flight Crew Operations Manual
ENGINE INOP
MAX CONTINUOUS THRUST
Driftdown/LRC Cruise Range Capability
Ground to Air Miles Conversion
or
pr
in
te
d
AIR DISTANCE (NM)
TAILWIND COMPONENT (KTS)
20
40
60
80
100
95
90
86
82
78
190
180
172
164
157
284
270
258
246
235
379
360
344
328
314
474
451
429
410
392
569
541
515
492
471
664
631
601
574
549
758
721
687
656
628
853
811
773
738
706
948
901
859
820
785
1043
991
945
902
863
1138
1081
1030
984
942
1232
1171
1116
1066
1020
1327
1261
1202
1148
1098
1422
1351
1288
1230
1177
1517
1441
1373
1312
1255
1611
1531
1459
1393
1333
1706
1621
1545
1475
1411
ad
ed
GROUND
DISTANCE
(NM)
100
200
300
400
500
600
700
800
900
1000
1100
1200
1300
1400
1500
1600
1700
1800
do
w
nl
o
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
100
80
60
40
20
138
128
120
112
106
275
256
239
225
212
413
384
359
337
317
551
512
479
449
423
689
640
598
562
529
826
768
718
674
635
964
896
838
786
741
1102
1025
957
898
846
1240
1153
1077
1011
952
1377
1281
1197
1123
1058
1515
1409
1317
1235
1164
1653
1537
1436
1348
1270
1792
1666
1556
1460
1375
1930
1794
1676
1573
1481
2068
1922
1796
1685
1587
2207
2051
1916
1798
1693
2345
2180
2036
1910
1799
2484
2309
2156
2023
1905
Driftdown/Cruise Fuel and Time
45
0.4
0.8
1.3
1.8
2.2
2.7
3.1
3.6
4.0
4.4
4.8
5.3
5.7
6.1
6.5
6.9
7.3
7.7
if
40
0.4
0.8
1.2
1.6
2.0
2.4
2.8
3.2
3.6
4.0
4.4
4.8
5.2
5.5
5.9
6.3
6.6
7.0
U
nc
on
tro
lle
100
200
300
400
500
600
700
800
900
1000
1100
1200
1300
1400
1500
1600
1700
1800
FUEL REQUIRED (1000 KG)
WEIGHT AT START OF DRIFTDOWN (1000 KG)
50
55
60
65
70
75
0.4
0.4
0.4
0.5
0.5
0.5
0.9
0.9
1.0
1.0
1.1
1.1
1.4
1.5
1.6
1.7
1.7
1.8
1.9
2.0
2.2
2.3
2.4
2.6
2.4
2.6
2.8
3.0
3.1
3.3
2.9
3.1
3.3
3.6
3.8
4.0
3.4
3.6
3.9
4.2
4.4
4.7
3.9
4.2
4.5
4.8
5.0
5.4
4.3
4.7
5.0
5.4
5.7
6.0
4.8
5.2
5.6
6.0
6.3
6.7
5.3
5.7
6.1
6.6
6.9
7.4
5.7
6.2
6.7
7.1
7.6
8.1
6.2
6.7
7.2
7.7
8.2
8.7
6.6
7.2
7.7
8.3
8.8
9.4
7.1
7.7
8.3
8.9
9.4
10.0
7.5
8.2
8.8
9.4
10.0
10.7
8.0
8.6
9.3
10.0
10.6
11.3
8.4
9.1
9.8
10.5
11.2
12.0
d
AIR DIST
(NM)
80
0.5
1.2
1.9
2.7
3.5
4.2
5.0
5.7
6.4
7.1
7.8
8.6
9.3
10.0
10.7
11.3
12.0
12.7
85
0.5
1.2
2.0
2.9
3.7
4.5
5.2
6.0
6.8
7.6
8.3
9.1
9.8
10.6
11.3
12.1
12.8
13.5
TIME
(HR:MIN)
0:17
0:33
0:50
1:06
1:23
1:39
1:56
2:12
2:29
2:46
3:02
3:19
3:36
3:52
4:09
4:26
4:43
4:59
Includes APU fuel burn.
Driftdown at optimum driftdown speed and cruise at long range cruise speed.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.12.7
Performance Inflight - QRH
Engine Inoperative
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Altitude Capability
100 ft/min residual rate of climb
85
80
75
70
65
60
55
50
45
40
ISA + 10°C & BELOW
9500
12400
15300
18400
21100
23700
26300
29000
31400
33800
PRESSURE ALTITUDE (FT)
ISA + 15°C
6400
9500
12800
15800
18600
21800
24700
27700
30500
33000
U
nc
on
tro
lle
d
if
do
w
nl
o
ad
ed
With engine anti-ice on, decrease altitude capability by 2000 ft.
With engine and wing anti-ice on, decrease altitude capability by 6500 ft.
ISA + 20°C
3400
6500
9800
13200
16300
19400
22400
25800
29200
31800
or
pr
in
te
d
WEIGHT (1000 KG)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.12.8
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Engine Inoperative
737 Flight Crew Operations Manual
ENGINE INOP
Long Range Cruise Control
94.0
.593
288
2674
92.3
.582
283
2520
90.4
.563
274
2330
88.3
.543
263
2139
85.9
.520
252
1950
83.4
.495
239
1762
80.6
.469
227
1582
77.8
.445
215
1416
if
29
31
93.9
.596
268
2295
91.9
.585
263
2143
89.5
.563
253
1953
87.0
.538
241
1764
84.1
.511
228
1577
81.0
.480
214
1392
93.7
.597
258
2114
91.4
.585
252
1958
88.7
.561
241
1767
85.9
.533
229
1580
82.8
.502
215
1394
96.4
.614
254
2146
93.3
.597
247
1938
90.7
.583
241
1777
87.7
.556
229
1586
84.6
.525
216
1400
96.2
.614
244
1971
92.7
.596
236
1765
89.7
.578
229
1600
86.4
.548
216
1410
95.7
.613
233
1793
91.8
.593
225
1593
88.3
.571
216
1421
94.8
.610
222
1613
90.7
.589
214
1424
U
nc
94.0
.595
278
2481
92.2
.584
273
2330
90.0
.564
263
2140
87.7
.541
252
1950
85.2
.516
240
1762
82.3
.489
227
1575
79.4
.462
214
1402
27
or
pr
in
te
d
94.0
.590
299
2870
92.5
.579
293
2709
90.7
.562
284
2518
88.7
.542
274
2327
86.5
.521
263
2137
84.2
.498
251
1948
81.6
.475
239
1764
79.1
.452
227
1594
76.2
.429
215
1434
PRESSURE ALTITUDE (1000 FT)
19
21
23
25
ad
ed
17
do
w
nl
o
15
d
10
91.8
.561
311
3067
90.1
.545
302
2875
88.4
.528
293
2684
86.5
.510
282
2494
84.5
.491
271
2306
82.3
.471
261
2124
80.2
.453
250
1954
77.8
.434
240
1791
75.5
.415
229
1636
73.0
.395
218
1485
on
tro
lle
WEIGHT
(1000 KG)
%N1
MACH
85
KIAS
FF/ENG
%N1
MACH
80
KIAS
FF/ENG
%N1
MACH
75
KIAS
FF/ENG
%N1
MACH
70
KIAS
FF/ENG
%N1
MACH
65
KIAS
FF/ENG
%N1
MACH
60
KIAS
FF/ENG
%N1
MACH
55
KIAS
FF/ENG
%N1
MACH
50
KIAS
FF/ENG
%N1
MACH
45
KIAS
FF/ENG
%N1
MACH
40
KIAS
FF/ENG
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.12.9
Performance Inflight - QRH
Engine Inoperative
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Diversion Fuel and Time
Ground to Air Miles Conversion
GROUND
DISTANCE
(NM)
200
400
600
800
1000
1200
1400
1600
1800
2000
AIR DISTANCE (NM)
TAILWIND COMPONENT (KTS)
20
40
60
80
100
190
180
172
164
158
379
361
344
328
315
570
542
517
494
473
759
721
687
657
630
949
902
859
820
786
1139
1082
1031
984
943
1328
1262
1202
1147
1099
1518
1442
1373
1311
1256
1707
1622
1544
1474
1412
1896
1801
1715
1637
1568
or
pr
in
te
d
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
100
80
60
40
20
298
272
249
230
214
600
547
501
462
429
903
823
753
694
644
1209
1100
1005
926
859
1516
1379
1259
1159
1075
1825
1659
1513
1393
1290
2137
1940
1768
1626
1506
2450
2222
2024
1860
1722
2766
2507
2281
2095
1938
3083
2792
2539
2331
2155
ad
ed
Reference Fuel and Time Required at Check Point
PRESSURE ALTITUDE (1000 FT)
18
22
26
FUEL
TIME
FUEL
TIME
FUEL
TIME
FUEL
TIME
FUEL
TIME
(1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN)
200
1.4
0:43
1.2
0:41
1.1
0:39
1.0
0:38
0.9
0:37
400
2.8
1:23
2.6
1:19
2.4
1:14
2.2
1:11
2.1
1:09
600
4.3
2:04
3.9
1:57
3.6
1:50
3.4
1:45
3.2
1:42
800
5.7
2:46
5.2
2:36
4.9
2:26
4.5
2:19
4.4
2:14
1000
7.1
3:28
6.6
3:15
6.1
3:03
5.7
2:53
5.5
2:47
1200
8.5
4:10
7.9
3:55
7.3
3:40
6.8
3:28
6.6
3:21
1400
9.8
4:53
9.1
4:36
8.5
4:18
8.0
4:02
7.7
3:54
1600
11.2
5:36
10.4
5:16
9.7
4:55
9.1
4:38
8.7
4:28
1800
12.5
6:20
11.7
5:58
10.9
5:34
10.2
5:13
9.8
5:02
2000
13.9
7:05
12.9
6:39
12.0
6:13
11.3
5:49
10.8
5:36
AIR
DIST
(NM)
14
on
tro
lle
d
if
do
w
nl
o
10
Fuel Required Adjustments (1000 KG)
U
nc
REFERENCE FUEL REQUIRED
(1000 KG)
1
2
3
4
5
6
7
8
9
10
11
12
13
14
40
-0.1
-0.3
-0.4
-0.6
-0.7
-0.8
-1.0
-1.1
-1.3
-1.4
-1.6
-1.7
-1.9
-2.0
45
-0.1
-0.2
-0.3
-0.4
-0.5
-0.6
-0.8
-0.9
-1.0
-1.1
-1.2
-1.3
-1.4
-1.5
WEIGHT AT CHECK POINT (1000 KG)
50
55
60
65
70
-0.1
0.0
0.0
0.1
0.1
-0.1
-0.1
0.0
0.2
0.3
-0.2
-0.1
0.0
0.3
0.5
-0.3
-0.1
0.0
0.3
0.7
-0.4
-0.2
0.0
0.4
0.9
-0.4
-0.2
0.0
0.5
1.1
-0.5
-0.3
0.0
0.6
1.2
-0.6
-0.3
0.0
0.6
1.4
-0.7
-0.3
0.0
0.7
1.5
-0.7
-0.4
0.0
0.7
1.6
-0.8
-0.4
0.0
0.8
1.7
-0.9
-0.4
0.0
0.8
1.9
-0.9
-0.5
0.0
0.9
2.0
-1.0
-0.5
0.0
0.9
2.0
75
0.2
0.6
0.9
1.2
1.4
1.7
2.0
2.2
2.4
2.6
2.8
3.0
3.2
3.4
80
0.3
0.8
1.2
1.6
2.0
2.4
2.8
3.2
3.5
3.8
4.1
4.4
4.7
4.9
Includes APU fuel burn.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.12.10
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Engine Inoperative
737 Flight Crew Operations Manual
ENGINE INOP
MAX CONTINUOUS THRUST
Holding
Flaps Up
30000
35000
ad
ed
or
pr
in
te
d
PRESSURE ALTITUDE (FT)
10000
15000
20000
25000
88.3
92.8
252
253
2750
2800
86.5
91.0
244
245
2570
2610
84.7
89.1
95.0
236
238
239
2400
2420
2490
82.8
87.1
92.1
228
229
231
2230
2250
2270
80.8
85.0
89.7
97.7
220
221
222
224
2070
2070
2080
2230
78.5
82.8
87.4
93.7
211
212
213
214
1910
1910
1910
1970
76.3
80.5
84.9
90.0
202
203
204
205
1750
1740
1730
1760
73.8
77.8
82.3
87.0
192
193
194
195
1600
1580
1570
1570
70.9
75.0
79.4
84.0
185
185
185
185
1440
1420
1400
1400
67.8
72.0
76.2
80.7
178
178
178
178
1300
1270
1250
1240
if
do
w
nl
o
5000
84.1
251
2730
82.4
243
2570
80.5
236
2400
78.6
227
2240
76.7
219
2090
74.6
210
1930
72.3
201
1770
69.7
192
1620
66.9
185
1470
64.0
178
1330
d
1500
81.1
250
2740
79.5
242
2580
77.8
235
2420
76.0
227
2260
74.0
219
2100
71.7
210
1950
69.4
200
1800
66.9
192
1650
64.2
185
1500
61.1
178
1350
on
tro
lle
WEIGHT
(1000 KG)
%N1
85
KIAS
FF/ENG
%N1
80
KIAS
FF/ENG
%N1
75
KIAS
FF/ENG
%N1
70
KIAS
FF/ENG
%N1
65
KIAS
FF/ENG
%N1
60
KIAS
FF/ENG
%N1
55
KIAS
FF/ENG
%N1
50
KIAS
FF/ENG
%N1
45
KIAS
FF/ENG
%N1
40
KIAS
FF/ENG
94.9
196
1680
89.6
186
1450
85.4
178
1260
94.0
178
1360
U
nc
This table includes 5% additional fuel for holding in a racetrack pattern.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.12.11
Performance Inflight - QRH
Engine Inoperative
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
ENGINE INOP
ADVISORY INFORMATION
Gear Down Landing Rate of Climb Available
Flaps 15
RATE OF CLIMB (FT/MIN)
PRESSURE ALTITUDE (FT)
2000
4000
0
-290
-270
-240
-210
-190
-160
-130
-110
-80
-50
-30
-30
-30
-20
-20
-10
-10
-370
-350
-320
-300
-270
-250
-220
-190
-160
-140
-110
-100
-90
-90
-90
-90
-430
-410
-380
-360
-330
-310
-280
-260
-230
-170
-170
-160
-160
-170
6000
8000
or
pr
in
te
d
-2000
-220
-200
-170
-140
-120
-90
-60
-30
-20
-10
-10
-10
0
0
10
10
10
do
w
nl
o
52
50
48
46
44
42
40
38
36
34
32
30
20
10
0
-20
-40
-490
-470
-450
-420
-400
-370
-350
-240
-240
-240
-250
-250
-560
-540
-520
-490
-470
-340
-320
-320
-330
-340
6000
8000
-680
-660
-640
-610
-590
-570
-540
-440
-440
-450
-460
-480
-750
-730
-710
-690
-660
-540
-530
-530
-550
-570
ad
ed
TAT (°C)
Rate of climb capability shown is valid for 60000 kg, gear down at VREF15+5.
Decrease rate of climb 130 ft/min per 5000 kg greater than 60000 kg.
Increase rate of climb 180 ft/min per 5000 kg less than 60000 kg.
-2000
-400
-370
-350
-320
-300
-270
-250
-220
-200
-200
-200
-200
-200
-190
-190
-200
-200
0
-470
-440
-420
-400
-370
-340
-320
-290
-270
-240
-220
-220
-220
-220
-220
-220
-230
U
nc
on
tro
lle
52
50
48
46
44
42
40
38
36
34
32
30
20
10
0
-20
-40
RATE OF CLIMB (FT/MIN)
PRESSURE ALTITUDE (FT)
2000
4000
d
TAT (°C)
if
Flaps 30
-550
-530
-500
-480
-460
-430
-410
-380
-360
-330
-300
-290
-290
-290
-300
-310
-610
-590
-570
-540
-520
-500
-470
-450
-420
-360
-370
-370
-380
-390
Rate of climb capability shown is valid for 60000 kg, gear down at VREF30+5.
Decrease rate of climb 130 ft/min per 5000 kg greater than 60000 kg.
Increase rate of climb 180 ft/min per 5000 kg less than 60000 kg.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.12.12
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Gear Down
Section 13
GearHighlight
file
Down
GEAR DOWN
Gear Down
Gear Down
Long Range Cruise Altitude Capability
Max Cruise Thrust, 100 ft/min residual rate of climb
ISA + 20°C
9300
12600
15700
18600
21800
25300
28100
30700
33000
35400
or
pr
in
te
d
PRESSURE ALTITUDE (FT)
ISA + 15°C
12500
15500
18500
21500
24400
27100
29600
31900
34100
36500
U
nc
on
tro
lle
d
if
do
w
nl
o
85
80
75
70
65
60
55
50
45
40
ISA + 10°C & BELOW
15500
18400
21100
23700
26100
28600
30800
32900
35100
37500
ad
ed
WEIGHT (1000 KG)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.13.1
Performance Inflight - QRH
Gear Down
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
GEAR DOWN
Gear Down
Long Range Cruise Control
91.7
.557
240
1950
89.5
.543
233
1806
87.4
.525
225
1661
85.0
.504
216
1512
82.5
.482
206
1367
79.7
.458
196
1224
76.6
.434
185
1085
if
33
35
91.6
.560
231
1805
89.1
.544
224
1658
86.8
.525
216
1515
84.2
.502
206
1368
81.4
.477
196
1224
78.3
.452
185
1083
94.5
.578
229
1836
91.3
.562
222
1664
88.5
.545
215
1517
86.0
.523
206
1374
83.1
.498
196
1230
80.0
.471
185
1089
94.5
.580
220
1696
90.9
.562
213
1523
87.8
.544
205
1377
85.0
.520
196
1235
81.8
.491
185
1092
94.1
.581
211
1555
90.2
.561
203
1381
86.8
.541
195
1237
83.6
.513
185
1094
93.5
.580
201
1411
89.1
.559
193
1239
85.5
.535
185
1096
92.5
.578
191
1265
87.7
.554
183
1097
U
nc
31
or
pr
in
te
d
91.7
.554
248
2101
89.8
.541
242
1960
87.9
.524
234
1812
85.6
.504
225
1661
83.3
.484
216
1515
80.7
.463
206
1371
78.0
.441
196
1231
74.9
.417
185
1098
PRESSURE ALTITUDE (1000 FT)
25
27
29
ad
ed
23
do
w
nl
o
21
on
tro
lle
10
85.9
.482
267
2421
84.2
.468
259
2271
82.5
.454
251
2123
80.6
.440
243
1977
78.6
.425
235
1835
76.5
.409
226
1696
74.4
.393
217
1559
71.9
.376
207
1424
69.1
.358
197
1294
66.2
.340
187
1170
d
WEIGHT
(1000 KG)
%N1
85
MACH
KIAS
FF/ENG
%N1
80
MACH
KIAS
FF/ENG
%N1
75
MACH
KIAS
FF/ENG
%N1
70
MACH
KIAS
FF/ENG
%N1
65
MACH
KIAS
FF/ENG
%N1
60
MACH
KIAS
FF/ENG
%N1
55
MACH
KIAS
FF/ENG
%N1
50
MACH
KIAS
FF/ENG
%N1
45
MACH
KIAS
FF/ENG
%N1
40
MACH
KIAS
FF/ENG
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.13.2
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Gear Down
737 Flight Crew Operations Manual
GEAR DOWN
Long Range Cruise Enroute Fuel and Time
Ground to Air Miles Conversion
GROUND
DISTANCE
(NM)
200
400
600
800
1000
1200
1400
1600
1800
AIR DISTANCE (NM)
TAILWIND COMPONENT (KTS)
20
40
60
80
100
188
178
168
160
153
377
357
338
321
307
566
535
507
483
461
754
713
676
643
614
943
891
844
803
766
1131
1069
1013
962
918
1320
1247
1181
1122
1070
1508
1424
1348
1280
1221
1695
1600
1514
1438
1371
Reference Fuel and Time Required at Check Point
or
pr
in
te
d
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
100
80
60
40
20
324
290
260
236
217
654
583
523
474
435
989
880
787
713
653
1329
1181
1054
953
871
1674
1484
1322
1194
1090
2024
1791
1593
1436
1310
2381
2103
1865
1680
1530
2743
2417
2140
1924
1751
3113
2737
2418
2171
1972
PRESSURE ALTITUDE (1000 FT)
20
24
28
FUEL
TIME
FUEL
TIME
FUEL
TIME
FUEL
TIME
FUEL
TIME
(1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN)
200
2.4
0:49
2.2
0:47
1.9
0:44
1.7
0:42
1.6
0:41
400
4.9
1:36
4.5
1:31
4.0
1:25
3.7
1:20
3.5
1:17
600
7.4
2:25
6.8
2:17
6.1
2:06
5.7
1:59
5.4
1:54
800
9.8
3:14
9.1
3:03
8.1
2:48
7.6
2:38
7.2
2:31
1000
12.1
4:04
11.3
3:50
10.1
3:30
9.5
3:18
9.0
3:08
1200
14.4
4:56
13.5
4:39
12.1
4:14
11.3
3:58
10.7
3:46
1400
16.7
5:49
15.6
5:28
14.0
4:58
13.1
4:40
12.4
4:24
1600
18.9
6:43
17.7
6:18
15.9
5:44
14.9
5:22
14.1
5:03
1800
21.1
7:38
19.7
7:10
17.7
6:30
16.6
6:05
15.7
5:43
14
ad
ed
10
do
w
nl
o
AIR
DIST
(NM)
if
Fuel Required Adjustments (1000 KG)
U
nc
on
tro
lle
d
REFERENCE FUEL REQUIRED
(1000 KG)
2
4
6
8
10
12
14
16
18
20
22
40
-0.3
-0.7
-1.0
-1.3
-1.7
-2.0
-2.4
-2.7
-3.0
-3.4
-3.7
WEIGHT AT CHECK POINT (1000 KG)
50
60
70
-0.2
0.0
0.3
-0.3
0.0
0.6
-0.5
0.0
0.9
-0.7
0.0
1.2
-0.8
0.0
1.4
-1.0
0.0
1.6
-1.2
0.0
1.8
-1.3
0.0
2.0
-1.5
0.0
2.2
-1.7
0.0
2.4
-1.8
0.0
2.5
80
0.7
1.3
2.0
2.6
3.2
3.7
4.2
4.6
5.0
5.3
5.6
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.13.3
Performance Inflight - QRH
Gear Down
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
GEAR DOWN
Descent
VREF40 + 70 KIAS
FUEL (KG)
DISTANCE (NM)
21
20
19
19
18
17
17
16
15
14
13
13
12
11
8
6
4
280
270
270
260
260
250
250
240
230
230
220
210
200
190
170
140
110
91
86
81
77
72
68
64
60
56
52
48
44
40
36
26
16
9
U
nc
on
tro
lle
d
if
do
w
nl
o
Allowances for a straight-in approach are included.
or
pr
in
te
d
TIME (MIN)
ad
ed
PRESSURE ALTITUDE
(FT)
41000
39000
37000
35000
33000
31000
29000
27000
25000
23000
21000
19000
17000
15000
10000
5000
1500
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.13.4
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Gear Down
737 Flight Crew Operations Manual
GEAR DOWN
Holding
Flaps Up
30000
35000
ad
ed
or
pr
in
te
d
PRESSURE ALTITUDE (FT)
10000
15000
20000
25000
82.7
87.0
92.0
230
230
230
2220
2240
2260
81.1
85.4
90.0
225
225
225
2100
2100
2110
79.4
83.7
88.3
94.8
220
220
220
220
1970
1970
1970
2050
77.6
81.9
86.4
91.8
216
216
216
216
1850
1840
1840
1870
75.9
80.1
84.5
89.3
211
211
211
211
1730
1720
1710
1730
74.0
78.0
82.5
87.1
204
204
204
204
1610
1600
1580
1590
71.9
75.9
80.3
84.8
198
198
198
198
1490
1480
1460
1460
69.6
73.7
78.0
82.4
192
192
192
192
1380
1360
1330
1330
67.1
71.4
75.5
79.9
185
185
185
185
1270
1250
1220
1210
64.6
68.7
72.9
77.3
178
178
178
178
1160
1130
1110
1090
if
do
w
nl
o
5000
78.5
230
2230
77.0
225
2110
75.4
220
1990
73.7
216
1870
71.9
211
1750
69.8
204
1630
67.8
198
1520
65.6
192
1400
63.3
185
1290
60.6
178
1180
d
1500
75.8
230
2240
74.2
225
2120
72.5
220
2000
70.8
216
1890
69.0
211
1770
67.1
204
1660
65.1
198
1540
62.8
192
1430
60.3
185
1310
57.9
178
1200
on
tro
lle
WEIGHT
(1000 KG)
%N1
85
KIAS
FF/ENG
%N1
80
KIAS
FF/ENG
%N1
75
KIAS
FF/ENG
%N1
70
KIAS
FF/ENG
%N1
65
KIAS
FF/ENG
%N1
60
KIAS
FF/ENG
%N1
55
KIAS
FF/ENG
%N1
50
KIAS
FF/ENG
%N1
45
KIAS
FF/ENG
%N1
40
KIAS
FF/ENG
94.3
204
1670
90.4
198
1500
87.1
192
1350
84.5
185
1220
81.7
178
1100
91.5
185
1270
86.8
178
1110
U
nc
This table includes 5% additional fuel for holding in a racetrack pattern.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.13.5
Performance Inflight - QRH
Gear Down
do
w
nl
o
ad
ed
or
pr
in
te
d
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
U
nc
on
tro
lle
d
if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.13.6
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Gear Down, Engine Inop
GearHighlight
file
Down, Engine Inop
Section 14
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Driftdown Speed/Level Off Altitude
or
pr
in
te
d
Gear Down, Engine Inop
Gear Down, Engine Inoperative
100 ft/min residual rate of climb
OPTIMUM
DRIFTDOWN
SPEED (KIAS)
218
213
208
202
196
190
183
176
Includes APU fuel burn.
LEVEL OFF ALTITUDE (FT)
ISA + 10°C
ISA + 15°C
ISA + 20°C
& BELOW
1500
4700
2200
8000
5900
3400
11100
9300
7100
14000
12900
10900
16900
16000
14800
19800
18700
17600
22800
21700
20600
ad
ed
WEIGHT (1000 KG)
START
LEVEL OFF
DRIFTDOWN
75
70
70
66
65
61
60
57
55
52
50
47
45
43
40
38
do
w
nl
o
Long Range Cruise Altitude Capability
100 ft/min residual rate of climb
d
PRESSURE ALTITUDE (FT)
ISA + 15°C
ISA + 20°C
3200
8200
13000
16900
20500
5300
10400
15700
19300
U
nc
on
tro
lle
65
60
55
50
45
40
ISA + 10°C & BELOW
1600
6300
10600
14400
18000
21700
if
WEIGHT (1000 KG)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.14.1
Performance Inflight - QRH
Gear Down, Engine Inop
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Control
91.0
.374
210
2906
88.2
.359
202
2630
85.4
.344
193
2374
82.5
.329
184
2133
PRESSURE ALTITUDE (1000 FT)
11
13
15
17
92.8
.387
209
2913
89.9
.371
201
2626
86.9
.355
192
2356
83.9
.339
183
2107
91.7
.384
200
2633
88.6
.367
191
2351
85.4
.349
182
2088
94.2
.398
199
2657
90.4
.380
190
2352
87.0
.361
181
2076
19
21
23
or
pr
in
te
d
9
ad
ed
7
91.9
.375
219
3191
89.3
.362
211
2909
86.7
.348
203
2647
84.0
.334
195
2400
81.1
.320
186
2166
92.7
.393
189
2359
88.8
.374
180
2069
96.6
.408
189
2417
90.8
.387
179
2065
94.1
.402
179
2101
98.4
.418
178
2201
U
nc
on
tro
lle
d
if
5
90.2
.364
220
3192
87.8
.351
212
2924
85.3
.338
204
2672
82.7
.325
196
2432
79.8
.311
188
2206
do
w
nl
o
WEIGHT
(1000 KG)
%N1
MACH
60
KIAS
FF/ENG
%N1
MACH
55
KIAS
FF/ENG
%N1
MACH
50
KIAS
FF/ENG
%N1
MACH
45
KIAS
FF/ENG
%N1
MACH
40
KIAS
FF/ENG
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.14.2
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Gear Down, Engine Inop
737 Flight Crew Operations Manual
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Diversion Fuel and Time
Ground to Air Miles Conversion
AIR DISTANCE (NM)
TAILWIND COMPONENT (KTS)
20
40
60
80
100
93
88
83
78
75
187
175
165
156
148
280
262
246
232
220
373
349
328
309
293
466
436
409
385
365
559
523
490
462
438
652
610
572
538
510
745
696
652
614
581
838
782
733
690
653
931
868
813
765
724
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GROUND
DISTANCE
(NM)
100
200
300
400
500
600
700
800
900
1000
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AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
100
80
60
40
20
172
151
134
120
109
352
308
270
242
219
533
465
408
364
330
716
623
545
486
440
900
783
684
609
551
1086
943
823
733
661
1273
1105
964
856
772
1462
1267
1103
980
883
1653
1431
1245
1104
994
1845
1595
1386
1228
1105
Reference Fuel and Time Required at Check Point
PRESSURE ALTITUDE (1000 FT)
10
14
FUEL
TIME
FUEL
TIME
(1000 KG)
(HR:MIN)
(1000 KG)
(HR:MIN)
1.1
0:26
1.0
0:26
2.4
0:50
2.3
0:48
3.7
1:15
3.6
1:11
4.9
1:39
4.8
1:35
6.1
2:04
6.0
1:58
7.3
2:29
7.1
2:22
8.5
2:55
8.3
2:46
9.7
3:20
9.4
3:10
10.9
3:46
10.5
3:35
12.0
4:12
11.6
3:59
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TIME
(HR:MIN)
0:27
0:53
1:18
1:44
2:10
2:37
3:03
3:30
3:58
4:25
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FUEL
(1000 KG)
1.3
2.6
3.9
5.2
6.5
7.8
9.1
10.3
11.6
12.8
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300
400
500
600
700
800
900
1000
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AIR DIST
(NM)
Fuel Required Adjustments (1000 KG)
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REFERENCE FUEL REQUIRED
(1000 KG)
1
2
3
4
5
6
7
8
9
10
11
12
13
14
40
-0.2
-0.3
-0.5
-0.6
-0.8
-1.0
-1.1
-1.3
-1.5
-1.6
-1.8
-1.9
-2.1
-2.3
WEIGHT AT CHECK POINT (1000 KG)
50
60
70
-0.1
0.0
0.1
-0.2
0.0
0.3
-0.3
0.0
0.5
-0.3
0.0
0.7
-0.4
0.0
0.9
-0.5
0.0
1.0
-0.6
0.0
1.2
-0.7
0.0
1.4
-0.7
0.0
1.6
-0.8
0.0
1.8
-0.9
0.0
1.9
-1.0
0.0
2.1
-1.1
0.0
2.3
-1.1
0.0
2.5
80
0.3
0.6
1.0
1.3
1.7
2.0
2.4
2.7
3.1
3.5
3.8
4.2
4.5
4.9
Includes APU fuel burn.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.14.3
Performance Inflight - QRH
Gear Down, Engine Inop
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Holding
Flaps Up
15000
90.5
211
3380
88.2
204
3110
85.9
198
2860
83.4
192
2620
80.7
185
2380
77.8
178
2160
92.8
192
2670
89.6
185
2400
86.5
178
2140
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PRESSURE ALTITUDE (FT)
5000
10000
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1500
89.4
216
3610
87.4
211
3360
85.2
204
3110
82.9
198
2860
80.4
192
2630
77.8
185
2400
75.1
178
2180
92.9
204
3150
90.4
198
2880
87.7
192
2620
85.0
185
2380
82.1
178
2140
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WEIGHT
(1000 KG)
%N1
70
KIAS
FF/ENG
%N1
65
KIAS
FF/ENG
%N1
60
KIAS
FF/ENG
%N1
55
KIAS
FF/ENG
%N1
50
KIAS
FF/ENG
%N1
45
KIAS
FF/ENG
%N1
40
KIAS
FF/ENG
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This table includes 5% additional fuel for holding in a racetrack pattern.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.14.4
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Text
Section 15
TextHighlight
File
Introduction
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This chapter contains information to supplement performance data from
the Flight Management Computer (FMC). In addition, sufficient inflight
data is provided to complete a flight with the FMC inoperative. In the event
of conflict between data presented in this chapter and that contained in the
approved Airplane Flight Manual, the Flight Manual shall always take
precedence.
General
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Flight with Unreliable Airspeed / Turbulent Air Penetration
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Pitch attitude and average %N1 information is provided for use in all
phases of flight in the event of unreliable airspeed/Mach indications
resulting from blocking or freezing of the pitot system. Loss of radome or
turbulent air may also cause unreliable airspeed/Mach indications. The
cruise table in this section may also be used for turbulent air penetration.
Pitch attitude is shown in bold type for emphasis since altitude and/or
vertical speed indications may also be unreliable.
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Max Climb %N1
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This table shows Max Climb %N1 for a 280/.78 climb speed schedule,
normal engine bleed for packs on or off and anti-ice off. Enter the table
with airport pressure altitude and TAT and read %N1. %N1 adjustments are
shown for anti-ice operation.
Go-around %N1
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To find Max Go-around %N1 based on normal engine bleed for packs on
(AUTO) and anti-ice on or off, enter the Go-around %N1 table with airport
pressure altitude and reported OAT or TAT and read %N1. For packs OFF
or HIGH operation, apply the %N1 adjustment shown below the table.
VREF
This table contains flaps 40, 30 and 15 reference speeds for a given weight.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.15.1
Performance Inflight - QRH
Text
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Advisory Information
Runway Surface Condition Correlation
Normal Configuration Landing Distance
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When landing on slippery runways or runways contaminated with ice,
snow, slush, or standing water, the reported braking action must be
considered. A table is provided that correlates runway condition code to
runway surface condition description and reported braking action that can
then be used to determine the appropriate Normal Configuration Landing
Distance or Non-Normal Configuration Landing Distance.
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Tables are provided as advisory information for normal configuration
landing distances on dry runways and runways with good,
good-to-medium, medium, medium-to-poor, and poor reported braking
action. Landing distances (reference distances plus adjustments) are 115%
of the actual landing distance. The Normal Configuration Landing
Distance tables should be used enroute to make a landing distance
assessment for time of arrival.
if
The reference landing distance is the distance from threshold to complete
stop. It includes an air distance allowance of 1500 ft from threshold to
touchdown. The reference distance is based on a reference landing weight
and speed at sea level, standard day, zero wind, zero slope, two-engine
detent No. 2 reverse thrust, and auto speedbrakes.
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To use these tables, determine the reference landing distance for the
selected braking configuration and reported braking action. Adjust this
reference distance for landing weight, altitude, wind, slope, temperature,
approach speed, and the number of operative thrust reversers. Each
correction is applied independently to the reference landing distance. A
correction for use of manual speedbrakes is provided in the table notes.
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Use of the autobrake system commands the airplane to a constant
deceleration rate. In some conditions, such as a runway with "poor"
reported braking action, the airplane may not be able to achieve these
deceleration rates. In these cases, runway slope and inoperative reversers
influence the stopping distance. Since it cannot be determined quickly
when this becomes a factor, it is appropriate to add the effects of slope and
inoperative reversers when using the autobrake system.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.15.2
D6-27370-8AS-NOK
September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Text
737 Flight Crew Operations Manual
Non-normal Configuration Landing Distance
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Advisory information is provided to support non-normal configurations
that affect landing. Landing distances and adjustments are provided for dry
runways and runways with good, good-to-medium, medium,
medium-to-poor, and poor reported braking action. Landing distances
(reference distances plus adjustments) are representative of the actual
landing distance, and are not factored. The Non-Normal Configuration
Landing Distance tables should be used enroute to make a landing distance
assessment for time of arrival.
The reference landing distance is the distance from threshold to complete
stop. It includes an air distance allowance of 1500 ft from threshold to
touchdown. The reference distance is based on a reference landing weight
and speed at sea level, standard day, zero wind, zero slope, and maximum
available reverse thrust.
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Tables for Non-Normal Configuration Landing Distance in this section are
similar in format and used in the same manner as tables for the Normal
Configuration Landing Distance previously described.
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Recommended Brake Cooling Schedule
Advisory information is provided to assist in avoiding the problems
associated with hot brakes. For normal operation, most landings are at
weights below the AFM quick turnaround limit weight.
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Use of the recommended cooling schedule will help avoid brake overheat
and fuse plug problems that could result from repeated landings at short
time intervals or a rejected takeoff.
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Enter the Recommended Brake Cooling Schedule table with the airplane
weight and brakes on speed, adjusted for wind at the appropriate
temperature and altitude condition. Instructions for applying wind
adjustments are included below the table. Linear interpolation may be used
to obtain intermediate values. The resulting number is the reference brake
energy per brake in millions of foot-pounds, and represents the amount of
energy absorbed by each brake during a rejected takeoff. Notes providing
adjustments for wind are included below the table.
To determine the energy per brake absorbed during landing, enter the
appropriate Adjusted Brake Energy Per Brake table (No Reverse Thrust or
2 Engine Reverse) with the reference brake energy per brake and the type
of braking used during landing (Max Manual, Max Auto, or Autobrake).
The resulting number is the adjusted brake energy per brake and represents
the energy absorbed in each brake during the landing.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.15.3
Performance Inflight - QRH
Text
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
The recommended cooling time is found in the appropriate (steel or carbon
brakes) final table by entering with the adjusted brake energy per brake.
Times are provided for ground cooling and inflight gear down cooling.
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Brake Temperature Monitor System (BTMS) indications are also shown. If
brake cooling is determined from the BTMS, use the hottest brake
indication 10 to 15 minutes after the airplane has come to a complete stop,
or inflight with gear retracted to determine recommended cooling
schedule.
Engine Inoperative
Initial Max Continuous %N1
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Max Continuous %N1
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The Initial Max Continuous %N1 setting for use following an engine
failure is shown. The table is based on the typical all engine cruise speed
of.79M to provide a target %N1 setting at the start of driftdown. Once
driftdown is established, the Max Continuous %N1 table should be used to
determine %N1 for the given conditions.
Power setting is based on one engine operating with one A/C pack
operating and all anti-ice bleeds off. Enter the table with pressure altitude,
TAT, and IAS or Mach to read %N1.
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It is desirable to maintain engine thrust level within the limits of the Max
Cruise thrust rating. However, where thrust level in excess of Max Cruise
rating is required, such as for meeting terrain clearance, ATC altitude
assignments, or to attain maximum range capability, it is permissible to use
the thrust needed up to the Max Continuous thrust rating. The Max
Continuous thrust rating is intended primarily for emergency use at the
discretion of the pilot and is the maximum thrust that may be used
continuously.
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Driftdown Speed/Level Off Altitude
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The table shows optimum driftdown speed as a function of cruise weight
at start of driftdown. Also shown are the approximate weight and pressure
altitude at which the airplane will level off considering 100 ft/min residual
rate of climb.
The level off altitude is dependent on air temperature (ISA deviation).
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.15.4
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September 30, 2022
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Performance Inflight - QRH
Text
737 Flight Crew Operations Manual
Driftdown/LRC Range Capability
This table shows the range capability from the start of driftdown.
Driftdown is continued to level off altitude. As weight decreases due to
fuel burn, the airplane is accelerated to Long Range Cruise speed. Cruise
is continued at level off altitude and Long Range Cruise speed.
Long Range Cruise Altitude Capability
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To determine fuel required, enter the Ground to Air Miles Conversion table
with the desired ground distance and adjust for anticipated winds to obtain
air distance to destination. Then enter the Driftdown/Cruise Fuel and Time
table with air distance and weight at start of driftdown to determine fuel
and time required. If altitudes other than the level off altitude is used, fuel
and time required may be obtained by using the Engine Inoperative Long
Range Cruise Enroute Fuel and Time table.
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Long Range Cruise Control
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The table shows the maximum altitude that can be maintained at a given
weight and air temperature (ISA deviation), based on Long Range Cruise
speed, Max Continuous thrust, and 100 ft/min residual rate of climb.
The table provides target %N1, engine inoperative Long Range Cruise
Mach number, IAS and fuel flow for the airplane weight and pressure
altitude. The fuel flow values in this table reflect single engine fuel burn.
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APU Operation During Flight
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For APU operation during flight, increase fuel flow according to the
following table. These increments include the APU fuel flow and the effect
of increased drag from the APU door.
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PRESSURE ALTITUDE (1000 FT)
39
35
31
25
20
15
10
5
APU FUEL FLOW (KG/HR)
45
45
50
60
65
75
85
95
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.15.5
Performance Inflight - QRH
Text
737 Flight Crew Operations Manual
737-800W/CFM56-7B24
JAA
Category C/N Brakes
Long Range Cruise Diversion Fuel and Time
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Tables are provided for crews to determine the fuel and time required to
proceed to an alternate airfield with one engine inoperative. The data is
based on single engine Long Range Cruise speed and .78/280/250 descent.
Enter with Air Distance as determined from the Ground to Air Miles
Conversion table and read Fuel and Time required at the cruise pressure
altitude. Adjust the fuel obtained for deviation from the reference weight
at checkpoint as required by entering the off reference fuel adjustments
table with the fuel required for the reference weight and the actual weight
at checkpoint. Read fuel required and time for the actual weight.
Holding
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Target %N1, indicated airspeed and fuel flow per engine information is
tabulated for holding with flaps up based on the FMC optimum holding
speed schedule. This is the higher of the maximum endurance speed and
the maneuvering speed. Small variations in airspeed will not appreciably
affect the overall endurance time. Enter the table with weight and pressure
altitude to read %N1, IAS and fuel flow per engine.
Gear Down Landing Rate of Climb Available
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Rate of climb data is provided as guidance information in the event an
engine inoperative landing (manual or autoland) is planned. The tables
show gear down rate of climb available for Flaps 15 and Flaps 30. Enter
the table with TAT and pressure altitude to read rate of climb available.
Apply adjustments shown to correct for weight.
Gear Down
This section contains performance for airplane operation with the landing
gear extended. The data is based on engine bleeds for normal air
conditioning.
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Note: The Flight Management Computer System (FMCS) does not
contain special provisions for operation with landing gear extended.
As a result, the FMCS may generate inappropriate enroute speed
schedules, display non-conservative predictions of fuel burn,
estimated time of arrival (ETA), maximum altitude, and compute
overly shallow descent path. An accurate estimated time of arrival
(ETA) is available if current speed or Mach is entered into the
VNAV cruise page.
Tables for gear down performance in this section are identical in format
and used in the same manner as tables for the gear up configuration
previously described.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.15.6
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1
Section
737-800WSFP1
CFM56-7B24
CFM56-7B24
C KG MC FAA
KG M
CATC/N
FAA CATC/N
TALPA TALPA
(FMC Model
(FMC737-800W.1)
Model 737-800W.1)
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Table of Contents
Section 20
737-800WSFP1 CFM56-7B24 C KG M FAA CATC/N TALPA (FMC
Model 737-800W.1)
Pkg Model Identification . . . . . . . . . . . . . . . . . . . PI-QRH.ModID.20.1
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General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.20.1
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Flight With Unreliable Airspeed/
Turbulent Air Penetration . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.20.1
CLIMB (280/.76) . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.20.1
CRUISE (.76/280) . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.20.1
DESCENT (.76/280) . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.20.2
HOLDING (VREF40 + 70). . . . . . . . . . . . . . . . . . . PI-QRH.20.2
TERMINAL AREA (5000 FT) . . . . . . . . . . . . . . . . PI-QRH.20.3
Airport Altitude = -2000 FT . . . . . . . . . . . . . . . . PI-QRH.20.3
Airport Altitude = -1000 FT . . . . . . . . . . . . . . . . PI-QRH.20.4
Airport Altitude = SEA LEVEL . . . . . . . . . . . . . PI-QRH.20.5
Airport Altitude = 1000 FT . . . . . . . . . . . . . . . . PI-QRH.20.6
Airport Altitude = 2000 FT . . . . . . . . . . . . . . . . PI-QRH.20.7
Airport Altitude = 3000 FT . . . . . . . . . . . . . . . . PI-QRH.20.8
Airport Altitude = 4000 FT . . . . . . . . . . . . . . . . PI-QRH.20.9
Airport Altitude = 5000 FT . . . . . . . . . . . . . . . PI-QRH.20.10
Airport Altitude = 6000 FT . . . . . . . . . . . . . . . .PI-QRH.20.11
Airport Altitude = 7000 FT . . . . . . . . . . . . . . . PI-QRH.20.12
Airport Altitude = 8000 FT . . . . . . . . . . . . . . . PI-QRH.20.13
Airport Altitude = 9000 FT . . . . . . . . . . . . . . . PI-QRH.20.14
Airport Altitude = 10000 FT . . . . . . . . . . . . . . PI-QRH.20.15
Airport Altitude = 11000 FT. . . . . . . . . . . . . . . PI-QRH.20.16
Airport Altitude = 12000 FT . . . . . . . . . . . . . . PI-QRH.20.17
Airport Altitude = 13000 FT . . . . . . . . . . . . . . PI-QRH.20.18
Airport Altitude = 14000 FT . . . . . . . . . . . . . . PI-QRH.20.19
Airport Altitude = 14500 FT . . . . . . . . . . . . . . PI-QRH.20.20
FINAL APPROACH (1500 FT) . . . . . . . . . . . . . . PI-QRH.20.21
Airport Altitude = -2000 FT . . . . . . . . . . . . . . . PI-QRH.20.21
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
4
D6-27370-8AS-NOK
PI-QRH.TOC.20.1
Performance Inflight - QRH Table of Contents
737 Flight Crew Operations Manual
PI-QRH.20.21
PI-QRH.20.22
PI-QRH.20.22
PI-QRH.20.23
PI-QRH.20.23
PI-QRH.20.24
PI-QRH.20.24
PI-QRH.20.25
PI-QRH.20.25
PI-QRH.20.26
PI-QRH.20.26
PI-QRH.20.27
PI-QRH.20.27
PI-QRH.20.28
PI-QRH.20.28
PI-QRH.20.29
PI-QRH.20.29
PI-QRH.20.30
PI-QRH.20.31
PI-QRH.20.32
PI-QRH.20.33
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Airport Altitude = -1000 FT . . . . . . . . . . . . . . .
Airport Altitude = SEA LEVEL . . . . . . . . . . . .
Airport Altitude = 1000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 2000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 3000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 4000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 5000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 6000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 7000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 8000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 9000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 10000 FT. . . . . . . . . . . . . . .
Airport Altitude = 11000 FT. . . . . . . . . . . . . . .
Airport Altitude = 12000 FT. . . . . . . . . . . . . . .
Airport Altitude = 13000 FT. . . . . . . . . . . . . . .
Airport Altitude = 14000 FT. . . . . . . . . . . . . . .
Airport Altitude = 14500 FT. . . . . . . . . . . . . . .
GO-AROUND . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Max Climb %N1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Go-around %N1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
VREF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Advisory Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.21.1
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Runway Surface Condition Correlation . . . . . . . . . . . . PI-QRH.21.1
Normal Configuration Landing Distance . . . . . . . . . . . PI-QRH.21.2
Non-Normal Configuration Landing Distance . . . . . . . PI-QRH.21.8
Airspeed Unreliable (Flaps 15) . . . . . . . . . . . . . . . . PI-QRH.21.8
Airspeed Unreliable (Flaps 30) . . . . . . . . . . . . . . . . PI-QRH.21.9
Airspeed Unreliable (Flaps 40) . . . . . . . . . . . . . . . PI-QRH.21.10
All Flaps Up Landing. . . . . . . . . . . . . . . . . . . . . . . PI-QRH.21.11
ANTISKID INOPERATIVE (Flaps 15) . . . . . . . . PI-QRH.21.12
ANTISKID INOPERATIVE (Flaps 30) . . . . . . . . PI-QRH.21.13
ANTISKID INOPERATIVE (Flaps 40) . . . . . . . . PI-QRH.21.14
Jammed or Restricted Flight Controls (Flaps 15) . PI-QRH.21.15
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PI-QRH.TOC.20.2
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Performance Inflight - QRH Table of Contents
737 Flight Crew Operations Manual
PI-QRH.21.16
PI-QRH.21.17
PI-QRH.21.18
PI-QRH.21.19
PI-QRH.21.20
PI-QRH.21.21
PI-QRH.21.22
PI-QRH.21.23
PI-QRH.21.24
PI-QRH.21.25
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LEADING EDGE FLAPS TRANSIT (Flaps 15) .
LOSS OF SYSTEM A (Flaps 15) . . . . . . . . . . . . .
LOSS OF SYSTEM A (Flaps 30) . . . . . . . . . . . . .
LOSS OF SYSTEM A (Flaps 40) . . . . . . . . . . . . .
LOSS OF SYSTEM A AND SYSTEM B
(Flaps 15). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
LOSS OF SYSTEM B (Flaps 15) . . . . . . . . . . . . .
MANUAL REVERSION (Flaps 15). . . . . . . . . . .
One Engine Inoperative Landing (Flaps 15) . . . . .
One Engine Inoperative Landing (Flaps 30) . . . . .
Stabilizer Trim Inoperative (Flaps 15) . . . . . . . . .
Trailing Edge Flap Asymmetry (1 ≤ Flap
Lever <15) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flap Asymmetry (Flap Lever
15 or 25) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flap Asymmetry (Flap Lever 30) . .
Trailing Edge Flap Disagree (1 ≤ Indicated
Flaps <15) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flap Disagree (15 ≤ Indicated
Flaps <30) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flap Disagree (30 ≤ Indicated
Flaps <40) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flaps Up Landing . . . . . . . . . . . . . .
Recommended Brake Cooling Schedule . . . . . . . . . .
PI-QRH.21.26
PI-QRH.21.27
PI-QRH.21.28
PI-QRH.21.29
PI-QRH.21.30
PI-QRH.21.31
PI-QRH.21.32
PI-QRH.21.33
Engine Inoperative . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.22.1
U
nc
Initial Max Continuous %N1 . . . . . . . . . . . . . . . . . . . . PI-QRH.22.1
Max Continuous %N1 . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.22.2
Driftdown Speed/Level Off Altitude . . . . . . . . . . . . . . PI-QRH.22.6
Driftdown/LRC Cruise Range Capability . . . . . . . . . . PI-QRH.22.7
Long Range Cruise Altitude Capability . . . . . . . . . . . . PI-QRH.22.8
Long Range Cruise Control . . . . . . . . . . . . . . . . . . . . . PI-QRH.22.9
Long Range Cruise Diversion Fuel and Time . . . . . . PI-QRH.22.10
Holding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.22.11
Gear Down Landing Rate of Climb Available . . . . . . PI-QRH.22.12
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
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PI-QRH.TOC.20.3
Performance Inflight - QRH Table of Contents
737 Flight Crew Operations Manual
Gear Down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.23.1
PI-QRH.23.1
PI-QRH.23.2
PI-QRH.23.3
PI-QRH.23.4
PI-QRH.23.5
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Long Range Cruise Altitude Capability . . . . . . . . . . . .
Long Range Cruise Control . . . . . . . . . . . . . . . . . . . . .
Long Range Cruise Enroute Fuel and Time . . . . . . . . .
Descent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Holding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Gear Down, Engine Inoperative . . . . . . . . . . . . . . . . . . . .PI-QRH.24.1
ad
ed
Driftdown Speed/Level Off Altitude. . . . . . . . . . . . . . .
Long Range Cruise Altitude Capability . . . . . . . . . . . .
Long Range Cruise Control . . . . . . . . . . . . . . . . . . . . .
Long Range Cruise Diversion Fuel and Time. . . . . . . .
Holding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
PI-QRH.24.1
PI-QRH.24.1
PI-QRH.24.2
PI-QRH.24.3
PI-QRH.24.4
Text. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.25.1
PI-QRH.25.1
PI-QRH.25.1
PI-QRH.25.2
PI-QRH.25.4
PI-QRH.25.6
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Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Advisory Information . . . . . . . . . . . . . . . . . . . . . . . . . .
Engine Inoperative . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Gear Down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.TOC.20.4
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September 30, 2022
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Pkg Model Identification
Section 20
Pkg Model Identification
File Model
Pkg
highlight
Identification
General
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The table below shows the airplanes that have been identified with the following
performance package. Note, some airplanes may be identified with more than one
performance package. This configuration table information reflects the Boeing
delivered configuration updated for service bulletin incorporations in
conformance with the policy stated in the introduction section of the FCOM. The
performance data is prepared for the owner/operator named on the title page. The
intent of this information is to assist flight crews and airlines in knowing which
performance package is applicable to a given airplane. The performance package
model identification information is based on Boeing's knowledge of the airline's
fleet at a point in time approximately three months prior to the page date. Notice
of Errata (NOE) will not be provided to airlines to identify airplanes that are
moved between performance packages within this manual or airplanes added to
the airline's fleet whose performance packages are already represented in this
manual. These types of changes will be updated in the next block revision.
Owners/operators are responsible for ensuring the operational documentation they
are using is complete and matches the current configuration of their airplanes, and
the accuracy and validity of all information furnished by the owner/operator or
any other party. Owners/operators receiving active revision service are
responsible to ensure that any modifications to the listed airplanes are properly
reflected in this manual.
d
Serial and tabulation number are supplied by Boeing.
Serial Number
Tabulation
Number
HS-DBK
37774
YR323
HS-DBQ
37794
YR339
HS-DBT
61293
YV081
HS-DBV
61295
YV083
HS-DBW
61296
YV084
HS-DBU
61294
YV097
HS-DBX
61297
YV098
HS-DBY
61299
YV099
HS-DBZ
61300
YW351
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Registry Number
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September 30, 2022
2
D6-27370-8AS-NOK
PI-QRH.ModID.20.1
Performance Inflight - QRH Pkg Model Identification
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737 Flight Crew Operations Manual
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Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.ModID.20.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
General
Section 20
General
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
file Highlight
General
40
2.0
82.9
1.0
81.2
1.0
80.7
1.0
77.2
1.0
73.6
1.0
69.8
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CRUISE (.76/280)
Flaps Up, %N1 for Level Flight
PRESSURE
ALTITUDE (FT)
PITCH ATT
40000
%N1
PITCH ATT
35000
%N1
PITCH ATT
30000
%N1
PITCH ATT
25000
%N1
PITCH ATT
20000
%N1
PITCH ATT
15000
%N1
WEIGHT (1000 KG)
50
60
70
4.0
4.0
1100
600
4.0
3.5
4.0
1900
1500
1100
6.5
6.0
6.0
3300
2600
2100
9.5
8.5
8.0
4400
3600
3000
12.5
11.0
10.0
5300
4400
3700
ad
ed
40
4.0
1700
4.0
2500
7.0
4200
11.0
5600
14.5
6700
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CLIMB (280/.76)
Flaps Up, Set Max Climb Thrust
PRESSURE
ALTITUDE (FT)
PITCH ATT
40000
V/S (FT/MIN)
PITCH ATT
30000
V/S (FT/MIN)
PITCH ATT
20000
V/S (FT/MIN)
PITCH ATT
10000
V/S (FT/MIN)
SEA
PITCH ATT
V/S (FT/MIN)
LEVEL
WEIGHT (1000 KG)
50
60
70
2.5
3.5
85.4
88.9
2.0
2.5
3.0
82.6
84.4
86.8
1.5
2.0
2.5
81.5
82.7
84.2
1.5
2.0
2.5
77.9
79.0
80.5
1.5
2.0
2.5
74.2
75.3
76.6
1.5
2.0
3.0
70.6
71.6
72.9
80
4.0
800
6.0
1700
8.0
2500
9.5
3100
80
3.5
90.4
3.0
86.1
3.0
82.3
3.5
78.2
3.5
74.4
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.1
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
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HOLDING (VREF40 + 70)
Flaps Up, %N1 for Level Flight
PRESSURE ALTITUDE (FT)
PITCH ATT
%N1
KIAS
PITCH ATT
%N1
KIAS
PITCH ATT
%N1
KIAS
40
5.0
56
177
5.0
52
177
5.0
49
177
if
15000
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10000
80
1.5
-2700
0.5
-2000
0.5
-1700
0.5
-1500
0.5
-1400
WEIGHT (1000 KG)
50
60
70
5.0
5.0
5.0
62
66
70
193
212
229
5.0
5.0
5.0
58
62
66
192
211
228
5.5
5.0
5.0
54
58
62
191
210
227
80
5.0
73
246
5.0
69
244
5.0
66
243
U
nc
5000
WEIGHT (1000 KG)
50
60
70
-0.5
0.5
1.0
-2400
-2300
-2500
-2.0
-1.0
-0.5
-2600
-2300
-2100
-2.0
-1.0
0.0
-2300
-2000
-1900
-2.0
-1.0
0.0
-2100
-1800
-1700
-2.5
-1.0
-0.5
-1900
-1700
-1500
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40
-1.5
-2700
-3.5
-3100
-3.5
-2800
-3.5
-2500
-3.5
-2300
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DESCENT (.76/280)
Flaps Up, Set Idle Thrust
PRESSURE
ALTITUDE (FT)
PITCH ATT
40000
V/S (FT/MIN)
PITCH ATT
30000
V/S (FT/MIN)
PITCH ATT
20000
V/S (FT/MIN)
PITCH ATT
10000
V/S (FT/MIN)
SEA
PITCH ATT
V/S (FT/MIN)
LEVEL
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = -2000 FT
if
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80
6.0
63.6
223
6.0
65.8
203
6.5
66.7
183
5.5
68.0
183
6.0
69.0
173
6.5
70.6
163
6.0
74.1
173
U
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WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
52.2 56.3 60.0
191
203
213
5.0
5.5
6.0
54.3 58.5 62.3
171
183
193
5.5
6.0
6.5
54.4 58.9 63.1
151
163
173
4.5
5.0
5.5
55.6 60.2 64.4
151
163
173
5.0
5.5
5.5
56.3 61.1 65.3
141
153
163
6.0
6.0
6.5
57.6 62.5 66.8
131
143
153
5.5
5.5
6.0
61.2 66.1 70.2
141
153
163
ad
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40
4.5
47.5
177
5.0
49.6
157
5.5
49.3
137
4.5
50.4
137
5.0
50.9
127
6.0
52.1
117
5.0
55.5
127
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FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.3
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = -1000 FT
if
d
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tro
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80
6.5
64.4
223
6.0
66.5
203
6.5
67.5
183
5.5
68.8
183
6.0
69.8
173
6.5
71.5
163
6.0
74.9
173
or
pr
in
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WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
52.9 57.0 60.8
191
203
213
5.0
5.5
6.0
55.1 59.3 63.1
171
183
193
5.5
6.0
6.5
55.2 59.7 63.9
151
163
173
4.5
5.0
5.5
56.3 61.0 65.2
151
163
173
5.0
5.5
5.5
57.0 61.9 66.1
141
153
163
6.0
6.0
6.5
58.4 63.3 67.6
131
143
153
5.5
5.5
6.0
62.0 66.9 71.0
141
153
163
ad
ed
40
4.5
48.2
177
5.0
50.2
157
5.5
49.9
137
4.5
51.1
137
5.0
51.6
127
6.0
52.8
117
5.0
56.2
127
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FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.4
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = SEA LEVEL
if
d
or
pr
in
te
d
80
6.5
65.2
223
6.0
67.3
203
6.5
68.3
183
5.5
69.6
183
6.0
70.6
173
6.5
72.4
163
6.0
75.8
173
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
53.5 57.7 61.6
191
203
213
5.0
5.5
6.0
55.8 60.0 63.9
171
183
193
5.5
6.0
6.5
55.9 60.5 64.7
151
163
173
4.5
5.0
5.5
57.1 61.9 66.0
151
163
173
5.5
5.5
5.5
57.8 62.7 66.9
141
153
163
6.0
6.0
6.5
59.2 64.2 68.4
131
143
153
5.5
5.5
6.0
62.8 67.7 71.9
141
153
163
ad
ed
40
4.5
48.9
177
5.0
50.9
157
5.5
50.6
137
4.5
51.8
137
5.0
52.3
127
6.0
53.5
117
5.0
57.0
127
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FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.5
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 1000 FT
if
d
U
nc
on
tro
lle
80
6.5
66.0
223
6.0
68.0
203
6.5
69.1
183
5.5
70.4
183
6.0
71.5
173
6.5
73.2
163
6.0
76.6
173
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
54.3 58.4 62.4
191
203
213
5.0
5.5
6.0
56.5 60.8 64.7
171
183
193
5.5
6.0
6.5
56.6 61.3 65.5
151
163
173
4.5
5.0
5.5
57.9 62.7 66.8
151
163
173
5.5
5.5
5.5
58.6 63.5 67.7
141
153
163
6.0
6.0
6.5
60.0 65.0 69.2
131
143
153
5.5
5.5
6.0
63.6 68.5 72.8
141
153
163
ad
ed
40
4.5
49.7
177
5.0
51.6
157
5.5
51.4
137
4.5
52.6
137
5.0
53.0
127
6.0
54.3
117
5.0
57.7
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.6
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 2000 FT
if
d
or
pr
in
te
d
80
6.5
66.7
223
6.0
68.8
203
6.5
69.9
183
5.5
71.3
183
6.0
72.4
173
6.5
74.1
163
6.0
77.4
173
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
55.0 59.2 63.3
191
203
213
5.0
5.5
6.0
57.3 61.7 65.4
171
183
193
5.5
6.0
6.5
57.4 62.2 66.3
151
163
173
4.5
5.0
5.5
58.6 63.5 67.6
151
163
173
5.5
5.5
5.5
59.4 64.3 68.5
141
153
163
6.0
6.0
6.5
60.8 65.8 70.1
131
143
153
5.5
5.5
6.0
64.4 69.3 73.6
141
153
163
ad
ed
40
4.5
50.4
177
5.0
52.3
157
5.5
52.1
137
4.5
53.3
137
5.0
53.7
127
6.0
55.0
117
5.0
58.5
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.7
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 3000 FT
if
d
U
nc
on
tro
lle
80
6.5
67.4
223
6.0
69.6
203
6.5
70.7
183
5.5
72.1
183
6.0
73.3
173
6.5
74.9
163
6.0
78.2
173
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
55.8 60.0 64.1
191
203
213
5.0
5.5
6.0
58.0 62.5 66.2
171
183
193
5.5
6.0
6.5
58.2 63.0 67.1
151
163
173
4.5
5.0
5.5
59.5 64.3 68.4
151
163
173
5.5
5.5
5.5
60.2 65.2 69.4
141
153
163
6.0
6.0
6.5
61.6 66.5 71.0
131
143
153
5.5
5.5
6.0
65.2 70.2 74.5
141
153
163
ad
ed
40
4.5
51.0
177
5.0
53.1
157
5.5
52.9
137
4.5
54.0
137
5.0
54.5
127
6.0
55.8
117
5.0
59.3
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.8
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 4000 FT
if
d
or
pr
in
te
d
80
6.5
68.2
223
6.0
70.5
203
6.5
71.6
183
5.5
73.0
183
6.0
74.1
173
6.5
75.7
163
6.0
79.1
173
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
56.4 60.8 64.9
191
203
213
5.0
5.5
6.0
58.8 63.3 66.9
171
183
193
5.5
6.0
6.5
59.0 63.8 67.9
151
163
173
4.5
5.0
5.5
60.3 65.1 69.2
151
163
173
5.5
5.5
5.5
61.1 66.0 70.2
141
153
163
6.0
6.0
6.5
62.4 67.4 71.9
131
143
153
5.5
5.5
6.0
66.0 71.1 75.3
141
153
163
ad
ed
40
4.5
51.7
177
5.0
53.9
157
5.5
53.6
137
4.5
54.7
137
5.0
55.2
127
6.0
56.5
117
5.0
60.1
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.9
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 5000 FT
if
d
U
nc
on
tro
lle
80
6.5
69.0
224
6.0
71.4
204
6.5
72.5
184
5.5
73.8
184
6.0
74.9
174
6.5
76.5
164
6.0
80.0
174
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
57.2 61.6 65.6
191
203
213
5.0
5.5
6.0
59.6 64.1 67.7
171
183
193
5.5
6.0
6.5
59.8 64.6 68.7
151
163
173
4.5
5.0
5.5
61.1 65.9 70.0
151
163
173
5.5
5.5
5.5
61.9 66.7 71.1
141
153
163
6.0
6.0
6.5
63.3 68.2 72.7
131
143
153
5.5
5.5
6.0
66.8 71.9 76.1
141
153
163
ad
ed
40
4.5
52.4
177
5.0
54.6
157
5.5
54.3
137
4.5
55.5
137
5.0
56.0
127
6.0
57.3
117
5.0
61.0
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.10
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 6000 FT
if
d
or
pr
in
te
d
80
6.5
69.8
224
6.0
72.2
204
6.5
73.3
184
5.5
74.6
184
6.0
75.7
174
6.5
77.3
164
6.0
80.9
174
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
57.9 62.5 66.3
191
203
213
5.0
5.5
6.0
60.4 64.8 68.5
171
183
193
5.5
6.0
6.5
60.7 65.4 69.5
151
163
173
4.5
5.0
5.5
62.0 66.7 70.9
151
163
173
5.5
5.5
5.5
62.7 67.6 72.0
141
153
163
6.0
6.0
6.5
64.1 69.0 73.6
131
143
153
5.5
5.5
6.0
67.6 72.8 77.0
141
153
163
ad
ed
40
4.5
53.1
177
5.0
55.3
157
5.5
55.1
137
4.5
56.2
137
5.0
56.7
127
6.0
58.1
117
5.0
61.8
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.11
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 7000 FT
if
d
U
nc
on
tro
lle
80
6.5
70.6
224
6.0
73.1
204
6.5
74.1
184
5.5
75.4
184
6.0
76.5
174
6.5
78.2
164
6.0
81.8
174
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
58.7 63.3 67.1
191
203
213
5.0
5.5
6.0
61.3 65.6 69.4
171
183
193
5.5
6.0
6.5
61.5 66.2 70.4
151
163
173
4.5
5.0
5.5
62.8 67.5 71.8
151
163
173
5.5
5.5
5.5
63.5 68.4 72.8
141
153
163
6.0
6.0
6.5
64.9 69.9 74.4
131
143
153
5.5
5.5
6.0
68.5 73.7 77.8
141
153
163
ad
ed
40
4.5
53.8
177
5.0
56.1
157
5.5
55.8
137
4.5
57.0
137
5.0
57.6
127
6.0
58.9
117
5.0
62.6
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.12
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 8000 FT
if
d
or
pr
in
te
d
80
6.0
71.4
225
6.0
73.9
205
6.5
74.9
185
5.5
76.2
185
6.0
77.3
175
6.5
79.1
165
6.0
82.7
175
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
59.5 64.1 67.8
191
203
214
5.0
5.5
6.0
62.1 66.4 70.3
171
183
194
5.5
6.0
6.5
62.4 67.0 71.2
151
163
174
4.5
5.0
5.5
63.6 68.3 72.6
151
163
174
5.5
5.5
5.5
64.3 69.3 73.7
141
153
164
6.0
6.0
6.5
65.7 70.8 75.2
131
143
154
5.5
5.5
6.0
69.4 74.5 78.7
141
153
164
ad
ed
40
4.5
54.5
177
5.0
56.8
157
5.5
56.6
137
4.5
57.8
137
5.0
58.4
127
6.0
59.8
117
5.0
63.5
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.13
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 9000 FT
if
d
U
nc
on
tro
lle
80
6.0
72.2
225
6.0
74.7
205
6.5
75.7
185
5.5
77.1
185
5.5
78.2
175
6.5
80.0
165
6.0
83.6
175
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
60.4 64.9 68.6
191
204
214
5.0
5.5
6.0
62.9 67.2 71.1
171
184
194
5.5
6.0
6.5
63.1 67.8 72.1
151
164
174
4.5
5.0
5.5
64.4 69.2 73.4
151
164
174
5.5
5.5
5.5
65.1 70.2 74.5
141
154
164
6.0
6.0
6.5
66.5 71.7 76.1
131
144
154
5.5
5.5
6.0
70.3 75.3 79.6
141
154
164
ad
ed
40
4.5
55.3
177
5.0
57.6
157
5.5
57.4
137
4.5
58.7
137
5.0
59.2
127
6.0
60.6
117
5.0
64.3
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.14
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 10000 FT
if
d
or
pr
in
te
d
80
6.0
73.0
225
6.0
75.5
205
6.5
76.6
185
5.5
78.0
185
5.5
79.1
175
6.0
80.8
165
6.0
84.5
175
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
61.2 65.6 69.4
191
204
214
5.0
5.5
6.0
63.7 68.0 72.0
171
184
194
5.5
6.0
6.0
64.0 68.7 72.9
151
164
174
4.5
5.0
5.0
65.3 70.1 74.3
151
164
174
5.0
5.5
5.5
65.9 71.1 75.3
141
154
164
6.0
6.0
6.5
67.4 72.6 76.9
131
144
154
5.5
5.5
6.0
71.2 76.2 80.6
141
154
164
ad
ed
40
4.5
56.0
177
5.0
58.4
157
5.5
58.2
137
4.5
59.5
137
5.0
60.1
127
6.0
61.4
117
5.0
65.0
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.15
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 11000 FT
if
d
U
nc
on
tro
lle
80
6.0
73.8
226
6.0
76.3
206
6.5
77.5
186
5.5
79.0
186
5.5
80.1
176
6.0
81.8
166
6.0
85.5
176
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
62.2 66.3 70.3
191
204
215
5.0
5.5
6.0
64.5 69.0 73.0
171
184
195
5.5
6.0
6.0
64.9 69.7 73.8
151
164
175
4.5
5.0
5.0
66.2 71.1 75.1
151
164
175
5.0
5.5
5.5
67.0 72.1 76.2
141
154
165
6.0
6.0
6.5
68.5 73.6 78.0
131
144
155
5.5
5.5
6.0
72.2 77.2 81.6
141
154
165
ad
ed
40
4.5
56.8
177
5.0
59.4
157
5.5
59.4
137
4.5
60.7
137
5.0
61.2
127
6.0
62.6
117
5.0
66.1
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.16
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 12000 FT
if
d
or
pr
in
te
d
80
6.0
74.6
226
6.0
77.2
206
6.5
78.5
186
5.5
79.9
186
5.5
81.1
176
6.0
82.8
166
5.5
86.6
176
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
63.0 67.1 71.2
191
204
215
5.0
5.5
6.0
65.3 69.9 73.7
171
184
195
5.5
6.0
6.0
65.8 70.6 74.7
151
164
175
4.5
5.0
5.0
67.1 72.0 76.0
151
164
175
5.0
5.5
5.5
68.0 73.0 77.2
141
154
165
6.0
6.0
6.0
69.7 74.5 78.9
131
144
155
5.5
5.5
5.5
73.2 78.3 82.6
141
154
165
ad
ed
40
4.5
57.6
178
5.0
60.4
158
5.5
60.4
138
4.5
61.7
138
5.0
62.2
128
6.0
63.6
118
5.0
67.3
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.17
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 13000 FT
if
d
U
nc
on
tro
lle
80
6.0
75.4
227
6.0
78.1
207
6.0
79.4
187
5.0
80.8
187
5.5
82.0
177
6.0
83.7
167
5.5
87.6
177
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
63.7 67.9 72.0
192
205
215
5.0
5.5
6.0
66.2 70.8 74.5
172
185
195
5.5
6.0
6.0
66.7 71.6 75.6
152
165
175
4.5
5.0
5.0
68.1 72.9 77.0
152
165
175
5.0
5.5
5.5
69.1 73.9 78.2
142
155
165
6.0
6.0
6.0
70.7 75.4 79.9
132
145
155
5.5
5.5
5.5
74.2 79.3 83.6
142
155
165
ad
ed
40
4.5
58.5
178
5.0
61.3
158
5.5
61.4
138
4.5
62.6
138
5.0
63.2
128
6.0
64.7
118
5.0
68.4
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.18
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 14000 FT
if
d
or
pr
in
te
d
80
6.0
76.3
227
6.0
79.0
207
6.0
80.3
187
5.5
81.7
187
5.5
82.9
177
6.0
84.7
167
5.5
88.6
177
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
64.4 68.7 72.8
192
205
215
5.0
5.5
6.0
67.1 71.6 75.3
172
185
195
5.5
6.0
6.0
67.7 72.4 76.5
152
165
175
4.5
5.0
5.0
69.1 73.7 77.9
152
165
175
5.0
5.5
5.5
70.1 74.8 79.1
142
155
165
6.0
6.0
6.0
71.7 76.5 80.9
132
145
155
5.5
5.5
5.5
75.1 80.2 84.5
142
155
165
ad
ed
40
4.5
59.4
178
5.0
62.2
158
5.5
62.3
138
4.5
63.5
138
5.0
64.1
128
6.0
65.8
118
5.0
69.5
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.19
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 14500 FT
if
d
U
nc
on
tro
lle
80
6.0
76.7
227
6.0
79.4
207
6.0
80.7
187
5.0
82.1
187
5.5
83.4
177
6.0
85.2
167
5.5
89.2
177
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
64.8 69.2 73.2
192
205
216
5.0
5.5
6.0
67.5 72.1 75.8
172
185
196
5.5
6.0
6.0
68.2 72.9 76.9
152
165
176
4.5
5.0
5.0
69.6 74.2 78.4
152
165
176
5.0
5.5
5.5
70.6 75.2 79.6
142
155
166
6.0
6.0
6.0
72.1 77.0 81.4
132
145
156
5.5
5.5
5.5
75.6 80.7 85.0
142
155
166
ad
ed
40
4.5
59.8
178
5.0
62.6
158
5.5
62.7
138
4.5
63.9
138
5.0
64.6
128
6.0
66.3
118
5.0
70.1
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.20
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = -2000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = -1000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
43.0 46.7
49.9
143
156
167
1.0
1.0
1.5
50.8 55.1
58.6
138
150
161
0.0
0.5
0.5
55.9 60.6
64.4
130
143
153
80
2.5
52.8
178
1.5
62.0
171
0.5
67.9
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
43.6 47.3
50.5
143
156
167
1.0
1.0
1.5
51.5 55.8
59.3
138
150
161
0.0
0.5
0.5
56.6 61.3
65.2
130
143
153
80
2.5
53.5
178
1.5
62.8
171
0.5
68.7
163
or
pr
in
te
d
40
2.0
38.9
128
1.0
46.1
124
0.0
50.5
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
39.5
128
1.0
46.7
124
0.0
51.2
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.21
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = SEA LEVEL
Flap placard speed exceeded in shaded area.
Airport Altitude = 1000 FT
80
2.5
54.2
178
1.5
63.6
171
0.5
69.5
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
44.7
48.7
51.8
143
156
167
1.0
1.0
1.5
52.9
57.2
60.9
138
150
161
0.0
0.5
0.5
58.1 62.9
66.8
131
143
153
80
2.5
54.9
178
1.5
64.4
171
0.5
70.3
163
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
44.1 48.0
51.1
143
156
167
1.0
1.0
1.5
52.2
56.5
60.1
138
150
161
0.0
0.5
0.5
57.3 62.1
66.1
131
143
153
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
40.2
128
1.0
47.3
124
0.0
51.9
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
40.7
128
1.0
47.9
124
0.0
52.6
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.22
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 2000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 3000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
45.4 49.3
52.5
143
156
167
1.0
1.0
1.5
53.6 58.0
61.7
138
150
161
0.0
0.5
0.5
58.9 63.7
67.5
131
143
153
80
2.5
55.6
178
1.5
65.1
171
0.5
71.1
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
46.0 49.9
53.2
143
156
167
1.0
1.0
1.5
54.3 58.7
62.5
138
150
161
0.0
0.5
0.5
59.6 64.5
68.3
131
143
153
80
2.5
56.3
178
1.5
65.9
171
0.5
72.0
163
or
pr
in
te
d
40
2.0
41.2
128
1.0
48.6
124
0.0
53.3
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
41.7
128
1.0
49.2
124
0.0
54.1
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.23
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 4000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 5000 FT
80
2.5
57.0
178
1.5
66.7
171
0.5
72.8
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
47.3
51.2
54.6
143
157
167
1.0
1.0
1.5
55.7
60.3
64.0
138
151
161
0.0
0.5
0.5
61.2 66.1
69.9
131
143
153
80
2.5
57.7
178
1.5
67.5
171
0.5
73.6
163
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
46.7 50.5
53.9
143
157
167
1.0
1.0
1.5
55.0
59.5
63.3
138
150
161
0.0
0.5
0.5
60.4 65.4
69.1
131
143
153
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
42.2
128
1.0
49.9
124
0.0
54.8
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
42.8
129
1.0
50.6
124
0.0
55.6
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.24
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 6000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 7000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
48.0 51.9
55.3
143
157
167
1.0
1.0
1.5
56.4 61.1
64.8
138
151
161
0.0
0.5
0.5
62.0 66.8
70.8
131
143
153
80
2.5
58.4
178
1.5
68.2
171
0.5
74.5
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
48.6 52.6
56.0
143
157
167
1.0
1.0
1.5
57.2 61.9
65.6
138
151
161
0.0
0.5
0.5
62.8 67.6
71.6
131
143
153
80
2.5
59.1
178
1.5
69.0
171
0.5
75.3
163
or
pr
in
te
d
40
2.0
43.4
129
1.0
51.3
124
0.0
56.3
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
44.0
129
1.0
52.0
124
0.0
57.0
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.25
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 8000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 9000 FT
80
2.5
59.8
178
1.5
69.8
171
0.5
76.1
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
49.9
54.1
57.4
143
157
168
1.0
1.5
1.5
58.8
63.4
67.1
138
151
161
0.5
0.5
0.5
64.4 69.3
73.3
131
143
153
80
2.5
60.6
179
1.5
70.6
172
0.5
76.9
163
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
49.2 53.3
56.7
143
157
167
1.0
1.0
1.5
58.0
62.7
66.4
138
151
161
0.0
0.5
0.5
63.6 68.4
72.5
131
143
153
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
44.6
129
1.0
52.7
124
0.0
57.8
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
45.3
129
1.0
53.4
124
0.0
58.6
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.26
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 10000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 11000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
50.6 54.7
58.1
143
157
168
1.0
1.5
1.5
59.6 64.2
67.9
138
151
161
0.5
0.5
0.5
65.2 70.1
74.1
131
143
153
80
2.5
61.4
179
1.5
71.4
172
0.5
77.8
164
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
51.3 55.5
58.8
143
157
168
1.0
1.5
1.5
60.4 65.1
68.7
138
151
161
0.5
0.5
0.5
66.0 71.0
74.9
131
143
153
80
2.5
62.2
179
1.5
72.3
172
0.5
78.7
164
or
pr
in
te
d
40
2.0
45.9
129
1.0
54.2
124
0.0
59.4
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
46.7
129
1.0
54.9
124
0.0
60.2
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.27
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 12000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 13000 FT
80
2.5
62.9
179
1.5
73.0
172
0.5
79.6
164
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
52.8
56.8
60.4
143
157
168
1.0
1.5
1.5
62.0
66.6
70.4
138
151
161
0.5
0.5
0.5
67.6 72.7
76.6
131
143
154
80
2.5
63.6
179
1.5
73.8
172
0.5
80.5
165
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
52.0 56.2
59.6
143
157
168
1.0
1.5
1.5
61.2
65.8
69.5
138
151
161
0.5
0.5
0.5
66.8 71.8
75.7
131
143
153
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
47.3
129
1.0
55.6
124
0.0
61.0
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
47.9
129
1.0
56.4
124
0.0
61.9
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.28
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 14000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 14500 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
53.5 57.6
61.3
143
157
168
1.0
1.5
1.5
62.9 67.5
71.3
138
151
161
0.0
0.5
0.5
68.6 73.6
77.6
131
144
154
80
2.5
64.4
180
1.5
74.6
172
0.5
81.4
165
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
53.9 58.0
61.7
144
157
168
1.0
1.5
1.5
63.4 68.0
71.7
138
151
161
0.0
0.0
0.5
69.2 74.1
78.1
131
144
154
80
2.5
64.7
180
1.5
75.0
172
0.5
81.9
165
or
pr
in
te
d
40
2.0
48.7
129
1.0
57.4
124
0.0
62.9
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
49.1
129
1.0
58.0
124
0.0
63.4
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.29
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
GO-AROUND
Flaps 15, Gear Up, Set Go-Around Thrust
5000
SEA
LEVEL
U
nc
on
tro
lle
d
if
-2000
80
9.0
1200
175
10.5
1600
174
12.0
1900
173
13.0
2200
173
13.0
2200
173
or
pr
in
te
d
10000
WEIGHT (1000 KG)
50
60
70
13.5
11.5
10.0
2600
2100
1600
141
154
164
16.0
13.5
12.0
3100
2500
2000
141
153
163
18.0
15.0
13.0
3500
2900
2400
141
153
163
20.0
17.0
14.5
3800
3100
2600
141
153
163
20.5
17.0
15.0
3700
3100
2600
140
153
163
ad
ed
14500
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
40
17.0
3400
127
20.0
3900
127
22.5
4300
127
25.5
4600
127
25.5
4600
127
do
w
nl
o
PRESSURE ALTITUDE (FT)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.30
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Max Climb %N1
file Highlight
Based on engine bleed for packs on or off and anti-ice off
PRESSURE ALTITUDE (FT)/SPEED (KIAS/MACH)
10000
15000
20000
25000
30000
35000
280
280
280
280
280
.78
89.7
89.8
89.6
91.4
93.0
94.4
90.5
90.7
90.0
90.8
92.4
93.7
91.3
91.5
91.0
90.8
91.7
93.0
92.1
92.3
91.9
91.7
91.7
92.3
92.9
93.1
92.7
92.5
92.5
91.6
93.6
93.8
93.6
93.3
93.3
92.4
94.3
94.6
94.4
94.1
94.0
93.2
95.0
95.2
95.2
94.8
94.7
94.0
95.8
96.0
95.9
95.6
95.4
94.7
95.2
96.8
96.7
96.3
96.1
95.5
94.4
97.1
97.6
97.0
96.7
96.2
93.6
96.3
98.5
97.9
97.4
97.0
92.8
95.5
97.9
99.0
98.4
97.8
92.0
94.7
97.2
98.9
99.4
98.6
91.2
93.9
96.4
98.1
99.7
99.5
90.3
93.1
95.6
97.4
98.9
100.5
89.5
92.3
94.8
96.6
98.1
100.2
88.7
91.4
94.1
95.8
97.3
99.3
87.8
90.6
93.3
95.0
96.5
98.5
87.0
89.8
92.4
94.1
95.6
97.6
86.1
88.9
91.6
93.3
94.8
96.8
37000
.78
94.5
93.8
93.1
92.4
91.7
91.7
92.6
93.4
94.2
95.0
95.8
96.6
97.5
98.3
99.2
100.1
100.7
99.9
99.0
98.2
97.3
41000
.78
92.8
92.1
91.4
90.7
90.0
90.1
91.1
92.1
93.0
94.0
94.9
95.8
96.7
97.7
98.7
99.7
100.3
99.5
98.7
97.8
96.9
or
pr
in
te
d
5000
280
89.7
90.5
91.2
91.9
92.6
93.3
94.1
94.1
93.3
92.5
91.8
91.0
90.2
89.4
88.6
87.8
87.0
86.1
85.3
84.5
83.6
ad
ed
60
55
50
45
40
35
30
25
20
15
10
5
0
-5
-10
-15
-20
-25
-30
-35
-40
0
280
89.4
90.2
90.9
91.6
92.4
92.9
92.2
91.5
90.7
90.0
89.2
88.4
87.7
86.9
86.1
85.3
84.5
83.7
82.9
82.0
81.2
do
w
nl
o
TAT (°C)
%N1 Adjustments for Engine Bleeds
BLEED CONFIGURATION
ENGINE ANTI-ICE
ENGINE & WING ANTI-ICE*
PRESSURE ALTITUDE (1000 FT)
10
20
30
35
-0.8
-0.9
-0.9
-0.8
-2.1
-2.5
-2.7
-3.0
41
-0.8
-3.0
U
nc
on
tro
lle
d
if
*Dual bleed sources
0
-0.6
-1.8
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.20.31
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Go-around %N1
Based on engine bleed for packs on, engine and wing anti-ice on or off
0
91.8
92.6
93.3
94.1
94.9
95.8
95.7
94.9
94.2
93.4
92.6
91.8
91.0
90.2
89.4
88.6
87.8
86.9
86.1
85.2
84.4
83.5
82.6
1000
91.8
92.6
93.3
94.1
94.9
95.8
96.3
95.5
94.7
94.0
93.2
92.4
91.6
90.8
90.0
89.2
88.3
87.5
86.7
85.8
84.9
84.1
83.2
2000
3000
4000
5000
6000
7000
8000
9000 10000
92.5
93.3
94.1
94.8
95.7
96.5
96.1
95.3
94.5
93.8
93.0
92.2
91.4
90.6
89.7
88.9
88.1
87.2
86.3
85.5
84.6
83.7
92.5
93.3
94.0
94.8
95.7
96.5
96.7
95.9
95.1
94.4
93.6
92.8
92.0
91.1
90.3
89.5
88.6
87.8
86.9
86.1
85.2
84.3
93.3
94.0
94.7
95.6
96.4
97.3
96.5
95.8
95.0
94.2
93.4
92.6
91.8
90.9
90.1
89.3
88.4
87.6
86.7
85.8
84.9
93.2
94.0
94.7
95.5
96.4
97.3
97.2
96.5
95.7
94.9
94.1
93.3
92.5
91.7
90.8
90.0
89.2
88.3
87.4
86.6
85.7
93.2
93.9
94.6
95.5
96.3
97.2
97.9
97.2
96.4
95.6
94.8
94.0
93.2
92.4
91.6
90.7
89.9
89.0
88.2
87.3
86.4
93.9
94.6
95.4
96.2
97.1
98.3
97.9
97.1
96.4
95.6
94.8
94.0
93.2
92.3
91.5
90.7
89.8
89.0
88.1
87.2
93.8
94.6
95.3
96.2
97.0
98.2
98.7
97.9
97.1
96.4
95.6
94.8
94.0
93.2
92.3
91.5
90.7
89.8
89.0
88.1
94.5
95.3
96.1
97.0
98.1
99.4
98.7
98.0
97.2
96.4
95.7
94.9
94.1
93.3
92.5
91.6
90.8
90.0
89.1
PRESSURE ALTITUDE (FT)
3000 4000 5000 6000 7000
0.8
0.8
0.8
0.9
0.9
-0.1 -0.1 -0.1 -0.1 -0.1
8000
0.9
-0.1
9000 10000
1.0
0.9
-0.1 -0.1
94.4
95.2
96.0
96.9
98.0
99.4
99.5
98.8
98.1
97.3
96.5
95.8
95.0
94.2
93.4
92.6
91.8
90.9
90.1
or
pr
in
te
d
60
55
50
45
40
35
30
25
20
15
10
5
0
-5
-10
-15
-20
-25
-30
-35
-40
-45
-50
AIRPORT PRESSURE ALTITUDE (FT)
-2000
91.0
91.7
92.5
93.3
94.1
94.3
93.5
92.8
92.0
91.3
90.5
89.7
89.0
88.2
87.4
86.6
85.8
84.9
84.1
83.3
82.4
81.6
80.7
ad
ed
TAT
(°C)
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AIRPORT
OAT
°C
°F
57
134
52
125
47
116
42
108
37
99
32
90
27
81
22
72
17
63
12
54
7
45
2
36
-3
27
-8
18
-13
9
-17
1
-22
-8
-27
-17
-32
-26
-37
-35
-42
-44
-47
-53
-52
-62
%N1 Adjustments for Engine Bleeds
0
0.8
-0.1
1000
0.8
-0.1
2000
0.8
-0.1
if
-2000
0.6
-0.1
U
nc
on
tro
lle
d
BLEED
CONFIGURATION
PACKS OFF
A/C HIGH
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.32
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
VREF
file Highlight
40
159
154
148
143
139
133
127
121
114
107
15
174
169
163
157
153
147
140
133
126
119
U
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on
tro
lle
d
if
do
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ad
ed
85
80
75
70
65
60
55
50
45
40
FLAPS
30
167
162
156
151
147
141
134
128
121
114
or
pr
in
te
d
WEIGHT (1000 KG)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
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PI-QRH.20.33
Performance Inflight - QRH
General
do
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o
ad
ed
or
pr
in
te
d
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
U
nc
on
tro
lle
d
if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.20.34
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Advisory Information
Section 21
Advisory
file
Highlight
Information
ADVISORY INFORMATION
Runway Surface Condition Correlation
Advisory Information
Advisory Information
5
4
3
Dry
Wet (Smooth, Grooved or PFC) or Frost
3 mm (0.12 inches) or less of: Water, Slush, Dry Snow or Wet Snow
Compacted Snow at or below -15°C OAT
Wet (Slippery), Dry Snow or Wet Snow (any depth) over Compacted Snow
Greater than 3 mm (0.12 inches) of : Dry Snow or Wet Snow
Compacted Snow at OAT warmer than -15°C
Greater than 3 mm (0.12 inches) of: Water or Slush
Ice
Wet Ice, Water on top of Compacted Snow, Dry Snow or Wet Snow over Ice
Good
Good to Medium
Medium
Medium to Poor
Poor
Nil
U
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on
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lle
d
if
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ad
ed
2
1
0
REPORTED
BRAKING
ACTION
Dry
RUNWAY SURFACE CONDITION DESCRIPTION
or
pr
in
te
d
RUNWAY
CONDITION
CODE
6
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.1
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
1295
1635
2265
2820
3085
85/-70
80/-80
120/-130
175/-185
205/-220
25/35
35/45
60/75
80/110
100/125
-40/140
-50/180
-85/295
-120/405
-140/470
40/50
45/60
60/75
80/110
100/125
-70/230
-70/240
-85/300
-120/405
-140/470
35/-30
35/-30
5/-5
35/-50
80/-90
55/70
60/75
65/85
85/110
100/125
-90/310
-90/315
-100/350
-125/430
-140/485
70/85
70/90
70/90
85/110
100/125
-110/385
-110/390
-115/405
-130/455
-145/495
Good Reported Braking Action
1705
1820
2270
2820
3085
85/-90
90/-100
120/-130
175/-185
205/-220
40
70
115
110
105
25
0
0
90
255
45
5
0
90
385
40/-40
40/-40
60/-60
80/-80
85/-85
50
65
115
110
105
75
85
5
90
255
165
190
10
90
385
65/-50
60/-50
35/-25
55/-60
90/-95
50/-50
50/-50
60/-65
80/-80
85/-85
60
70
115
110
105
145
150
80
110
260
345
360
220
180
415
90/-75
85/-70
70/-45
75/-70
105/-100
60/-60
60/-65
65/-70
80/-80
85/-85
70
80
115
110
105
220
220
150
130
270
525
530
430
265
450
do
w
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o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
10/-10
0/0
0/0
35/-50
80/-90
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF15
25/-25
35/-35
60/-60
80/-80
85/-85
ad
ed
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
2000
2080
2375
2850
3090
110/-115
120/-120
130/-140
175/-185
205/-220
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
2295
2345
2480
2880
3095
140/-140
145/-145
145/-150
180/-190
205/-220
U
nc
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
d
Medium Reported Braking Action
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
APP
SPD
ADJ
REVERSE
THRUST
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
-135/500
-135/505
-140/510
-150/545
-160/575
165/-115
160/-110
145/-95
145/-105
165/-130
70/-70
70/-75
70/-80
85/-85
90/-90
80
85
110
110
105
350
350
315
265
365
895
900
855
685
795
-160/615
-160/615
-165/615
-175/640
-180/655
235/-155
235/-150
225/-145
220/-145
225/-160
80/-85
80/-85
80/-85
85/-90
90/-100
85
90
105
110
105
475
475
485
405
460
1270
1270
1280
1105
1140
2635
2655
2745
3035
3210
170/-170
175/-175
175/-175
195/-205
215/-225
85/110
85/110
85/110
95/125
105/140
Poor Reported Braking Action
2970
2970
3005
3195
3325
200/-200
200/-200
200/-200
215/-220
225/-230
100/130
100/130
100/130
105/145
110/150
do
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o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
ad
ed
Medium To Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
PER
5 KTS ONE NO
ABOVE REV REV
VREF15
or
pr
in
te
d
REF
DIST
if
Reference distance is based on sea level, standard day, no wind or slope, VREF15, two-engine detent No. 2
reverse thrust, and auto speedbrakes.
For max manual braking and manual speedbrakes, increase reference landing distance by 70 m.
For autobrake and manual speedbrakes, increase reference landing distance by 60 m.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
All reference distances and adjustments shown have been increased by 15%.
U
nc
on
tro
lle
d
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.3
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
1250
1555
2130
2615
2850
70/-65
70/-75
115/-120
160/-165
185/-195
25/30
30/40
50/70
75/100
85/115
-40/140
-50/165
-85/280
-115/385
-130/455
40/50
40/50
50/70
75/100
85/115
-65/225
-70/235
-85/290
-115/385
-130/455
35/-30
35/-30
5/-10
35/-45
75/-80
50/65
50/70
60/80
75/100
85/115
-85/300
-85/310
-100/340
-120/410
-135/465
65/80
65/85
65/85
75/105
85/115
-105/375
-105/380
-110/390
-125/435
-140/470
Good Reported Braking Action
1640
1755
2135
2615
2850
80/-85
85/-90
115/-120
160/-165
185/-195
40
65
100
100
90
15
0
0
90
215
40
5
0
90
345
35/-35
40/-40
50/-50
70/-70
80/-80
50
65
100
100
90
70
75
5
90
215
150
165
10
90
345
65/-50
60/-50
35/-30
55/-60
90/-85
45/-45
50/-50
60/-60
70/-70
80/-80
60
70
100
100
90
130
130
70
110
220
300
315
195
170
375
90/-70
85/-70
65/-50
75/-70
105/-85
50/-60
60/-60
65/-65
75/-75
80/-80
70
80
100
100
90
190
190
130
130
225
450
460
380
245
405
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
10/-10
0/0
0/-5
35/-45
75/-80
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF30
25/-25
35/-35
50/-50
70/-70
80/-80
ad
ed
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1910
1995
2240
2645
2860
105/-110
110/-115
125/-130
160/-170
185/-195
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
2175
2235
2345
2675
2865
125/-130
130/-140
130/-140
160/-175
185/-195
U
nc
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
d
Medium Reported Braking Action
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.4
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
APP
SPD
ADJ
REVERSE
THRUST
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
-130/485
-130/490
-135/495
-145/525
-150/550
155/-105
150/-105
140/-95
140/-105
160/-120
65/-70
65/-70
70/-70
80/-80
85/-85
75
85
95
100
90
300
295
275
245
310
-155/600
-155/600
-160/600
-165/615
-165/635
220/-145
220/-140
215/-140
205/-140
220/-150
75/-80
75/-80
75/-80
80/-85
85/-90
80
90
90
100
90
410 1060
405 1060
415 1070
360 930
390 970
2480
2515
2585
2825
2975
155/-160
160/-160
160/-160
180/-185
195/-200
75/100
80/105
80/105
85/115
90/125
Poor Reported Braking Action
2780
2790
2825
2975
3085
185/-185
185/-185
185/-185
195/-195
200/-205
85/120
90/120
90/120
90/125
100/130
do
w
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o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
ad
ed
Medium To Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
PER
5 KTS ONE NO
ABOVE REV REV
VREF30
or
pr
in
te
d
REF
DIST
755
760
725
590
685
if
Reference distance is based on sea level, standard day, no wind or slope, VREF30, two-engine detent No. 2
reverse thrust, and auto speedbrakes.
For max manual braking and manual speedbrakes, increase reference landing distance by 70 m.
For autobrake and manual speedbrakes, increase reference landing distance by 60 m.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
All reference distances and adjustments shown have been increased by 15%.
U
nc
on
tro
lle
d
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.5
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
1200
1465
1975
2450
2690
60/-60
65/-70
105/-115
145/-155
175/-180
25/30
30/35
45/65
70/85
80/105
-40/130
-45/160
-80/270
-110/375
-125/435
35/45
40/50
45/65
70/85
80/105
-65/225
-70/230
-80/275
-110/375
-125/435
35/-30
30/-30
10/-5
30/-40
65/-75
45/60
50/65
50/70
70/90
80/105
-85/295
-85/300
-90/330
-115/400
-130/450
60/75
60/80
60/80
70/90
80/110
-105/370
-105/375
-105/380
-120/425
-130/460
Good Reported Braking Action
1580
1680
1980
2450
2690
75/-80
80/-85
105/-115
145/-155
175/-180
40
65
100
105
100
15
0
0
45
165
35
0
0
45
260
35/-35
35/-35
45/-50
65/-65
75/-75
50
65
105
105
100
65
70
5
45
165
140
150
10
45
260
60/-50
55/-45
40/-30
50/-50
80/-80
45/-45
45/-45
50/-55
65/-65
75/-75
60
70
100
105
100
120
120
70
70
175
270
280
195
125
290
85/-70
80/-65
70/-50
70/-65
90/-80
50/-50
50/-50
60/-60
70/-70
75/-75
70
80
100
105
100
175
175
130
90
185
405
410
375
200
315
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
10/-10
0/0
0/-5
30/-40
65/-75
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF40
25/-25
30/-30
45/-45
65/-65
75/-75
ad
ed
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1830
1905
2090
2485
2695
100/-100
105/-105
115/-125
145/-160
175/-180
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
2085
2125
2200
2515
2700
120/-120
125/-125
125/-130
150/-160
175/-180
U
nc
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
d
Medium Reported Braking Action
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.6
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
APP
SPD
ADJ
REVERSE
THRUST
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
-130/475
-130/480
-130/485
-140/515
-150/540
150/-105
150/-100
140/-95
135/-100
150/-110
60/-65
60/-65
65/-65
70/-75
80/-80
75
85
95
100
95
275
275
255
205
265
680
680
670
520
585
-155/585
-155/585
-155/585
-160/605
-165/620
220/-140
220/-140
215/-140
200/-130
205/-145
70/-75
70/-75
70/-75
75/-80
80/-85
80
85
90
100
90
375
375
380
315
350
955
955
965
840
855
2370
2395
2445
2670
2810
145/-145
150/-150
150/-155
165/-175
180/-185
70/95
70/100
70/100
80/105
85/120
Poor Reported Braking Action
2660
2665
2690
2820
2925
175/-175
175/-175
180/-180
185/-185
190/-195
80/115
85/115
85/115
85/120
90/125
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
ad
ed
Medium To Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
PER
5 KTS ONE NO
ABOVE REV REV
VREF40
or
pr
in
te
d
REF
DIST
if
Reference distance is based on sea level, standard day, no wind or slope, VREF40, two-engine detent No. 2
reverse thrust, and auto speedbrakes.
For max manual braking and manual speedbrakes, increase reference landing distance by 65 m.
For autobrake and manual speedbrakes, increase reference landing distance by 50 m.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
All reference distances and adjustments shown have been increased by 15%.
U
nc
on
tro
lle
d
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.7
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
file Highlight
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Airspeed Unreliable (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1185
1540
2600
85/-60
70/-75
160/-170
25/30
35/45
80/105
-35/125
-50/160
-110/360
10/-10
0/0
50/-55
80/-80
85/-90
160/-170
40/50
40/55
80/105
-60/205
-60/215
-110/360
30/-30
30/-20
50/-55
25
0
160
50
5
185
35/-35
40/-40
75/-75
N/A
N/A
N/A
75
85
160
175
195
185
50/65
55/70
80/105
-80/275
-80/280
-115/385
55/-50
55/-40
65/-65
45/-45
50/-50
75/-75
N/A
N/A
N/A
145
155
180
350
365
265
60/80
65/85
65/90
-95/340
-95/345
-100/365
80/-65
75/-60
55/-50
55/-55
55/-55
65/-65
N/A
N/A
N/A
215
220
125
520
535
385
75/100
80/105
80/110
-120/440
-120/440
-125/455
140/-100
135/-95
120/-85
65/-70
65/-70
70/-75
N/A
N/A
N/A
335
335
280
875
880
800
90/120
90/125
90/125
-145/535
-145/535
-145/540
195/-130
195/-125
185/-120
75/-80
75/-80
75/-80
N/A
N/A
N/A
455 1230
450 1225
430 1215
Good To Medium Reported Braking Action
1825
1915
2625
105/-105
105/-110
165/-175
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
25/-25
35/-35
75/-75
ad
ed
1560
1680
2600
REVERSE
THRUST
ADJ
N/A
N/A
N/A
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2085
2145
2335
125/-125
125/-130
130/-140
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
150/-150
155/-155
155/-160
d
2375
2415
2540
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2665
2680
2740
175/-175
180/-180
175/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.8
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Airspeed Unreliable (Flaps 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1145
1465
2415
65/-55
65/-70
145/-155
75/-75
80/-85
145/-155
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/125
-45/155
-105/345
10/-10
0/0
45/-50
20/-20
30/-30
65/-65
N/A
N/A
N/A
20
0
135
45
5
185
35/50
40/50
70/95
-60/200
-60/210
-105/345
30/-25
30/-20
45/-50
35/-35
35/-35
65/-65
N/A
N/A
N/A
70
80
135
155
175
185
-75/265
-80/275
-110/370
55/-45
55/-40
60/-60
45/-45
45/-45
65/-70
N/A
N/A
N/A
130
135
155
305
320
255
-90/330
-95/335
-100/350
80/-60
75/-60
60/-50
50/-50
50/-55
60/-60
N/A
N/A
N/A
185
190
115
450
465
340
70/95
75/95
70/95
-115/425
-120/430
-120/440
135/-95
130/-90
120/-85
60/-60
60/-65
65/-70
N/A
N/A
N/A
290
290
240
740
745
675
80/110
85/110
80/110
-140/520
-140/525
-140/525
185/-125
180/-120
180/-115
65/-70
70/-75
70/-75
N/A
N/A
N/A
390 1025
390 1025
365 1010
ad
ed
1505
1615
2415
REVERSE
THRUST
ADJ
20/30
30/40
70/95
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1745
1830
2440
95/-95
100/-105
150/-155
45/65
50/65
75/95
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
1980
2045
2190
115/-115
120/-120
120/-125
55/75
60/80
60/80
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
140/-140
145/-145
145/-145
d
2245
2290
2380
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2510
2535
2570
160/-160
165/-165
165/-165
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.9
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Airspeed Unreliable (Flaps 40)
VREF40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1105
1375
2280
55/-50
60/-65
135/-145
20/30
30/35
65/85
-35/120
-45/150
-100/335
10/-10
0/0
40/-45
70/-75
75/-80
135/-145
35/45
35/50
65/85
-55/200
-60/210
-100/335
N/A
N/A
N/A
20
0
105
40
0
125
30/-25
30/-25
40/-45
35/-35
35/-35
60/-60
N/A
N/A
N/A
65
70
105
145
160
125
45/60
45/65
70/90
-75/265
-75/270
-105/360
55/-45
55/-45
55/-55
45/-45
45/-45
65/-65
N/A
N/A
N/A
120
125
125
280
290
195
55/70
55/75
55/75
-90/325
-90/330
-95/345
75/-60
75/-60
60/-45
50/-50
50/-50
55/-55
N/A
N/A
N/A
170
175
115
410
420
335
65/90
70/90
65/90
-115/420
-115/425
-115/435
130/-90
130/-90
120/-80
60/-60
60/-60
60/-65
N/A
N/A
N/A
265
265
235
670
675
635
75/105
80/105
75/105
-135/515
-135/515
-135/520
185/-120
185/-115
180/-115
65/-70
65/-70
65/-70
N/A
N/A
N/A
355
355
355
925
925
935
Good To Medium Reported Braking Action
1680
1755
2305
90/-95
95/-100
135/-145
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1455
1550
2280
REVERSE
THRUST
ADJ
20/-20
30/-30
60/-60
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
1905
1960
2060
110/-110
110/-115
110/-120
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
135/-135
135/-135
135/-140
d
2155
2195
2255
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2405
2425
2450
155/-155
155/-155
155/-155
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.10
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
All Flaps Up Landing
VREF40 + 55
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1470
1965
3585
190/-80
90/-85
195/-225
90/-100
90/-100
195/-225
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-45/200
-60/190
-130/435
20/-15
5/0
60/-75
35/-35
50/-50
105/-105
45
75
115
40
5
215
85
15
225
50/70
55/75
115/150
-70/235
-75/245
-130/435
40/-35
30/-25
60/-75
50/-50
55/-55
105/-105
50
75
115
110
95
215
255
250
225
-90/315
-95/320
-135/460
75/-65
70/-55
80/-85
65/-65
65/-70
110/-110
60
80
115
215
210
240
525
530
340
-110/390
-115/395
-120/420
110/-90
105/-85
65/-45
75/-75
75/-80
90/-90
70
80
125
320
325
185
795
805
570
110/145
110/145
110/150
-140/505
-145/505
-145/525
190/-135
190/-130
155/-100
90/-95
90/-95
100/-105
80
90
125
520 1395
520 1390
430 1265
130/175
130/175
130/175
-170/620
-170/615
-170/625
270/-180
270/-175
245/-155
105/-110
105/-110
110/-115
90
95
120
715 1990
710 1975
675 1955
ad
ed
1950
2135
3585
REVERSE
THRUST
ADJ
50/105
45/75
115/150
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
2335
2455
3615
125/-130
125/-130
200/-225
70/95
75/95
115/155
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2720
2775
3080
155/-160
155/-160
150/-165
85/115
90/115
90/120
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
195/-200
195/-200
190/-195
d
3155
3180
3370
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3590
3580
3660
230/-235
230/-235
225/-225
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.11
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
ANTISKID INOPERATIVE (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1860
100/-105
50/65
-80/280
50/-45
Autobrake Inoperative
Autobrake Inoperative
55/75
-95/340
75/-60
Autobrake Inoperative
Autobrake Inoperative
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
2070
120/-120
Good To Medium Reported Braking Action
2345
145/-145
45/-45
60
125
295
50/-50
65
185
460
795
70/95
-120/440 135/-95
Autobrake Inoperative
Autobrake Inoperative
60/-65
70
300
85/115
-140/535 190/-125
Autobrake Inoperative
Autobrake Inoperative
70/-75
75
410 1125
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
Good Reported Braking Action
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2615
170/-170
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
210/-210
d
3035
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
105/145
-190/760 395/-210
Autobrake Inoperative
Autobrake Inoperative
80/-95
85
710 2305
120/175
-235/985 600/-290
Autobrake Inoperative
Autobrake Inoperative
90/-110
90
1005 3480
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3455
250/-245
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.12
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
ANTISKID INOPERATIVE (Flaps 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1785
95/-100
110/-115
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-75/275
50/-40
Autobrake Inoperative
Autobrake Inoperative
40/-40
55
110
260
55/70
-90/335
75/-60
Autobrake Inoperative
Autobrake Inoperative
45/-50
65
165
395
-115/430 130/-90
Autobrake Inoperative
Autobrake Inoperative
55/-60
70
260
670
-135/520 180/-120
Autobrake Inoperative
Autobrake Inoperative
65/-70
75
355
940
ad
ed
1975
REVERSE
THRUST
ADJ
45/60
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
2225
135/-135
65/90
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2470
155/-155
75/105
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
190/-190
d
2855
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
95/135
-185/740 370/-195
Autobrake Inoperative
Autobrake Inoperative
75/-90
80
610 1895
110/160
-230/960 560/-270
Autobrake Inoperative
Autobrake Inoperative
85/-105
85
860 2845
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3235
225/-225
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.13
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
ANTISKID INOPERATIVE (Flaps 40)
VREF40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1715
90/-95
40/55
-75/270
50/-40
Autobrake Inoperative
Autobrake Inoperative
50/65
-90/330
75/-60
Autobrake Inoperative
Autobrake Inoperative
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1900
105/-110
Good To Medium Reported Braking Action
2135
130/-130
40/-40
60
100
235
45/-45
65
150
360
60/85
-115/420 130/-90
Autobrake Inoperative
Autobrake Inoperative
55/-55
70
240
605
70/100
-135/510 180/-115
Autobrake Inoperative
Autobrake Inoperative
60/-65
75
325
850
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
Good Reported Braking Action
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2370
150/-150
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
185/-185
d
2740
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
90/125
-180/730 365/-190
Autobrake Inoperative
Autobrake Inoperative
70/-85
80
560 1720
105/150
-225/945 550/-265
Autobrake Inoperative
Autobrake Inoperative
80/-100
85
795 2590
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3105
215/-215
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.14
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Jammed or Restricted Flight Controls (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1120
1420
2420
75/-60
70/-70
150/-160
75/-75
80/-85
150/-160
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/120
-45/155
-105/350
10/-10
0/0
35/-45
20/-20
30/-30
65/-65
35
60
90
20
0
105
45
5
105
35/45
40/50
70/95
-55/200
-60/210
-105/350
30/-25
30/-20
35/-45
35/-35
35/-35
65/-65
45
55
90
70
80
105
160
175
105
-75/265
-80/275
-110/370
55/-45
55/-40
55/-55
45/-45
45/-45
70/-70
55
65
90
135
140
125
325
335
180
-90/330
-95/335
-95/350
80/-65
75/-60
55/-40
50/-50
50/-55
55/-60
60
70
100
195
200
125
485
490
390
70/95
75/100
75/100
-115/430
-120/430
-120/440
140/-95
135/-95
120/-80
60/-65
60/-65
65/-70
70
75
95
310
315
275
825
825
780
85/115
85/115
85/115
-140/525
-140/525
-140/530
195/-125
195/-125
185/-115
70/-75
70/-75
70/-75
75
75
90
425 1165
425 1160
425 1165
ad
ed
1470
1570
2420
REVERSE
THRUST
ADJ
20/30
30/40
70/95
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1720
1790
2445
100/-100
100/-105
155/-165
45/60
50/65
75/95
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
1965
2010
2140
120/-120
120/-125
125/-130
55/75
60/80
60/80
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
145/-145
145/-150
150/-150
d
2245
2270
2350
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2525
2525
2555
170/-170
170/-170
170/-170
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.15
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LEADING EDGE FLAPS TRANSIT (Flaps 15)
VREF15 + 15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1230
1600
2725
80/-65
75/-75
170/-180
25/35
35/45
85/110
-40/130
-50/165
-110/370
15/-10
0/0
50/-60
80/-85
85/-90
170/-180
40/55
45/60
85/110
-60/210
-65/220
-110/370
35
65
90
25
0
175
55
5
210
35/-30
30/-20
50/-60
40/-40
40/-40
75/-75
45
65
90
85
95
175
195
215
210
55/75
60/75
85/115
-80/280
-85/290
-115/395
60/-50
55/-45
70/-70
50/-50
50/-50
80/-80
55
70
90
160
170
195
385
405
295
65/90
70/90
70/95
-100/350
-100/355
-105/370
85/-70
80/-65
60/-50
55/-60
60/-60
65/-70
60
70
95
235
240
140
575
590
430
80/110
85/110
85/115
-125/450
-125/455
-130/465
145/-105
145/-100
125/-90
65/-70
70/-75
75/-80
70
80
95
365
365
305
960
965
880
95/130
95/130
95/130
-145/545
-145/550
-150/555
205/-140
205/-130
190/-125
75/-80
80/-85
80/-85
75
85
90
490 1340
490 1340
465 1325
Good To Medium Reported Braking Action
1905
2000
2750
105/-110
110/-115
170/-180
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1630
1755
2725
REVERSE
THRUST
ADJ
25/-25
35/-35
75/-75
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2180
2245
2445
130/-130
135/-135
135/-145
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
160/-160
160/-160
160/-165
d
2485
2525
2655
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2785
2805
2865
185/-185
185/-185
185/-185
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.16
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM A (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1235
1425
2545
70/-60
65/-70
150/-165
90/-95
95/-100
150/-165
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-40/130
-45/150
-105/360
15/-15
5/0
0/-10
25/-25
30/-30
70/-70
45
60
140
30
0
0
50
5
0
45/60
45/60
70/90
-65/230
-70/230
-105/360
45/-40
40/-35
5/-10
40/-40
40/-45
70/-70
70
75
140
120
125
0
245
255
0
-85/305
-90/305
-115/385
80/-65
80/-65
30/-25
50/-55
50/-55
75/-75
80
85
140
225
225
50
510
515
250
-105/375
-105/375
-105/375
110/-90
115/-90
115/-80
60/-65
60/-65
60/-65
90
90
90
325
325
325
775
775
775
90/120
90/125
90/125
-135/480
-135/480
-135/480
185/-130
190/-135
190/-130
70/-80
75/-80
75/-80
100
100
100
500 1340
500 1345
500 1345
105/145
105/145
105/145
-160/580
-160/580
-160/580
255/-170
260/-175
260/-175
80/-90
85/-90
85/-90
105
105
105
675 1905
675 1910
675 1910
ad
ed
1720
1755
2545
REVERSE
THRUST
ADJ
25/35
30/40
70/90
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
2020
2035
2585
120/-125
125/-125
155/-170
60/80
60/80
75/95
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2315
2315
2315
145/-150
150/-150
150/-150
70/95
70/100
70/100
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
180/-180
185/-180
185/-180
d
2645
2645
2645
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2970
2970
2970
210/-210
215/-210
215/-210
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.17
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM A (Flaps 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1185
1350
2380
65/-55
60/-65
140/-150
25/30
25/35
65/85
-40/125
-45/145
-105/345
15/-15
0/0
0/-10
85/-90
90/-95
140/-150
40/55
40/55
65/85
-65/220
-65/225
-105/345
45
55
130
25
0
0
45
5
0
45/-40
40/-35
0/-10
40/-40
40/-40
65/-65
65
70
130
105
105
0
210
215
0
55/75
55/75
70/90
-85/290
-85/295
-110/370
75/-65
75/-60
25/-25
50/-50
50/-50
65/-70
75
80
130
190
190
45
430
430
200
65/90
65/90
65/90
-100/360
-100/360
-100/360
105/-85
110/-85
105/-75
55/-60
55/-60
55/-60
85
85
90
275
275
275
645
640
645
80/110
80/110
80/110
-125/465
-125/465
-125/465
175/-120
180/-125
175/-120
65/-70
65/-70
65/-70
90
90
95
420 1090
420 1085
420 1090
95/130
95/130
95/130
-150/565
-150/565
-150/565
240/-155
245/-160
245/-160
75/-80
75/-80
75/-80
95
95
95
565 1530
565 1530
565 1530
Good To Medium Reported Braking Action
1915
1920
2415
110/-115
115/-115
140/-155
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1640
1665
2380
REVERSE
THRUST
ADJ
25/-25
30/-30
65/-65
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2185
2175
2180
135/-135
135/-135
135/-135
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
165/-165
165/-165
165/-165
d
2480
2475
2480
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2775
2775
2775
190/-190
195/-190
195/-190
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.18
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM A (Flaps 40)
VREF40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1140
1270
2185
60/-50
55/-60
125/-140
80/-85
80/-90
125/-140
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/125
-40/140
-95/330
15/-15
0/0
0/-5
20/-20
25/-25
60/-60
45
55
125
25
5
0
35
10
0
40/50
40/50
60/75
-65/220
-65/220
-95/330
45/-35
35/-30
0/-5
35/-35
35/-35
60/-60
70
70
125
95
95
0
190
185
0
-85/290
-85/290
-100/355
75/-60
70/-55
30/-15
45/-45
45/-45
60/-65
80
80
125
170
170
45
375
370
190
-100/355
-100/355
-100/355
100/-80
105/-80
105/-75
55/-55
55/-55
55/-55
85
85
90
245
240
240
560
555
555
75/105
75/105
75/105
-125/455
-125/455
-125/455
165/-115
170/-120
170/-115
65/-65
65/-65
65/-65
90
90
95
370
370
370
935
930
930
85/120
90/120
90/120
-150/550
-145/550
-145/550
230/-150
235/-155
235/-155
70/-75
70/-75
70/-75
95
95
95
495 1305
495 1305
495 1305
ad
ed
1570
1570
2185
REVERSE
THRUST
ADJ
20/30
25/30
60/75
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1820
1815
2220
105/-110
105/-110
130/-140
50/70
50/70
60/80
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2070
2055
2060
125/-130
125/-130
125/-130
60/85
60/85
60/85
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
155/-155
155/-155
155/-155
d
2345
2335
2340
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2620
2615
2615
180/-180
180/-180
180/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.19
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM A AND SYSTEM B (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1685
80/-85
40/50
-60/195
35/-30
Autobrake Inoperative
Autobrake Inoperative
65/90
-100/335 100/-80
Autobrake Inoperative
Autobrake Inoperative
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
2390
135/-140
Good To Medium Reported Braking Action
2760
170/-175
40/-40
75
-5
60
60/-60
105
90
425
905
85/115
-125/430 160/-120
Autobrake Inoperative
Autobrake Inoperative
75/-75
115
225
100/135
-145/520 215/-160
Autobrake Inoperative
Autobrake Inoperative
85/-85
125
355 1385
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
Good Reported Braking Action
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
3130
200/-205
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
240/-240
d
3495
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
120/165
-180/650 345/-215
Autobrake Inoperative
Autobrake Inoperative
95/-100
130
580 2370
140/195
-210/780 475/-270
Autobrake Inoperative
Autobrake Inoperative
105/-115
135
805 3355
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3860
275/-270
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.20
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM B (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1245
55/-60
95/-95
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-40/145
15/-15
Autobrake Inoperative
Autobrake Inoperative
25/-25
40
35
55
45/60
-70/245
45/-40
Autobrake Inoperative
Autobrake Inoperative
40/-40
55
120
250
-90/325
80/-65
Autobrake Inoperative
Autobrake Inoperative
50/-50
65
215
490
-110/400 115/-90
Autobrake Inoperative
Autobrake Inoperative
60/-60
75
305
730
ad
ed
1715
REVERSE
THRUST
ADJ
25/35
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1995
120/-120
60/80
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2275
145/-145
70/95
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
175/-175
d
2575
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
85/120
-140/515 200/-130
Autobrake Inoperative
Autobrake Inoperative
70/-75
80
460 1215
100/140
-165/625 285/-170
Autobrake Inoperative
Autobrake Inoperative
80/-85
85
610 1695
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2875
200/-200
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.21
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
MANUAL REVERSION (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1685
80/-85
40/50
-60/195
35/-30
Autobrake Inoperative
Autobrake Inoperative
65/90
-100/335 100/-80
Autobrake Inoperative
Autobrake Inoperative
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
2390
135/-140
Good To Medium Reported Braking Action
2760
170/-175
40/-40
75
-5
60
60/-60
105
90
425
905
85/115
-125/430 160/-120
Autobrake Inoperative
Autobrake Inoperative
75/-75
115
225
100/135
-145/520 215/-160
Autobrake Inoperative
Autobrake Inoperative
85/-85
125
355 1385
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
Good Reported Braking Action
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
3130
200/-205
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
240/-240
d
3495
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
120/165
-180/650 345/-215
Autobrake Inoperative
Autobrake Inoperative
95/-100
130
580 2370
140/195
-210/780 475/-270
Autobrake Inoperative
Autobrake Inoperative
105/-115
135
805 3355
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3860
275/-270
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.22
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
One Engine Inoperative Landing (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1130
1420
2520
80/-60
70/-70
150/-160
75/-80
85/-90
150/-160
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/125
-45/155
-105/355
10/-10
0/0
10/-30
20/-20
30/-30
70/-70
35
60
115
0
0
0
20
0
5
35/50
40/50
70/90
-60/210
-65/220
-105/355
35/-30
35/-25
10/-30
35/-35
40/-40
70/-70
50
60
115
0
0
0
85
95
5
-80/285
-85/295
-115/385
70/-55
65/-50
35/-40
45/-45
50/-50
75/-75
60
70
115
0
0
0
180
185
55
-100/360
-100/365
-105/370
100/-80
95/-75
80/-60
55/-55
60/-60
60/-60
70
80
95
0
0
0
270
275
245
75/100
75/105
80/105
-130/475
-130/480
-135/480
185/-125
185/-120
175/-115
70/-70
70/-75
70/-75
80
90
95
0
0
0
475
480
465
90/120
90/125
95/125
-160/590
-160/590
-160/590
270/-170
270/-165
265/-170
80/-85
80/-85
80/-85
85
95
90
0
0
0
675
680
685
ad
ed
1520
1635
2520
REVERSE
THRUST
ADJ
20/30
30/40
70/90
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1820
1905
2555
100/-105
110/-115
155/-165
50/65
50/65
75/95
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2115
2175
2235
125/-130
130/-135
135/-140
60/80
60/80
65/85
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
160/-165
165/-165
165/-170
d
2485
2515
2565
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2850
2855
2890
190/-195
195/-195
195/-200
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.23
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
One Engine Inoperative Landing (Flaps 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1090
1350
2335
60/-55
60/-65
140/-145
20/25
25/35
65/85
-35/120
-45/145
-100/340
10/-10
0/0
15/-35
75/-75
80/-85
140/-145
35/45
35/50
65/85
-60/205
-60/215
-100/340
35
55
100
0
0
0
20
0
10
35/-30
30/-25
15/-35
35/-35
35/-35
65/-65
50
60
100
0
0
0
75
85
10
45/60
45/65
65/90
-80/280
-80/285
-105/370
65/-55
60/-50
40/-45
45/-45
45/-45
65/-65
60
70
100
0
0
0
155
160
55
55/75
55/75
60/75
-95/350
-100/355
-100/360
95/-75
90/-70
80/-65
50/-55
55/-55
55/-55
65
75
85
0
0
0
230
235
210
70/95
70/95
75/95
-125/460
-125/460
-130/465
170/-115
170/-110
165/-115
65/-65
65/-70
65/-70
75
85
85
0
0
0
395
395
390
85/110
85/110
85/110
-150/565
-150/565
-155/570
245/-155
245/-150
245/-160
75/-75
75/-80
75/-80
80
90
80
0
0
0
555
555
565
Good To Medium Reported Braking Action
1730
1815
2370
95/-100
100/-105
145/-150
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1460
1570
2335
REVERSE
THRUST
ADJ
20/-20
30/-30
65/-65
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2000
2055
2105
115/-120
120/-125
120/-130
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
145/-150
150/-155
150/-155
d
2325
2355
2395
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2650
2655
2685
175/-175
175/-180
175/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.24
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Stabilizer Trim Inoperative (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1120
1420
2420
75/-60
70/-70
150/-160
75/-75
80/-85
150/-160
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/120
-45/155
-105/350
10/-10
0/0
35/-45
20/-20
30/-30
65/-65
35
60
90
20
0
105
45
5
105
35/45
40/50
70/95
-55/200
-60/210
-105/350
30/-25
30/-20
35/-45
35/-35
35/-35
65/-65
45
55
90
70
80
105
160
175
105
-75/265
-80/275
-110/370
55/-45
55/-40
55/-55
45/-45
45/-45
70/-70
55
65
90
135
140
125
325
335
180
-90/330
-95/335
-95/350
80/-65
75/-60
55/-40
50/-50
50/-55
55/-60
60
70
100
195
200
125
485
490
390
70/95
75/100
75/100
-115/430
-120/430
-120/440
140/-95
135/-95
120/-80
60/-65
60/-65
65/-70
70
75
95
310
315
275
825
825
780
85/115
85/115
85/115
-140/525
-140/525
-140/530
195/-125
195/-125
185/-115
70/-75
70/-75
70/-75
75
75
90
425 1165
425 1160
425 1165
ad
ed
1470
1570
2420
REVERSE
THRUST
ADJ
20/30
30/40
70/95
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1720
1790
2445
100/-100
100/-105
155/-165
45/60
50/65
75/95
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
1965
2010
2140
120/-120
120/-125
125/-130
55/75
60/80
60/80
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
145/-145
145/-150
150/-150
d
2245
2270
2350
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2525
2525
2555
170/-170
170/-170
170/-170
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.25
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Asymmetry (1 ≤ Flap Lever <15)
VREF40 + 30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1225
1625
2765
95/-60
70/-75
160/-175
25/40
35/45
85/110
-40/130
-50/170
-110/375
15/-10
0/0
55/-60
75/-80
80/-85
160/-175
40/55
45/55
85/110
-60/210
-65/220
-110/375
40
65
90
25
0
180
55
5
220
30/-30
25/-20
55/-60
35/-40
40/-40
80/-80
45
65
90
80
70
180
175
175
220
55/70
55/75
85/115
-80/280
-85/285
-115/400
60/-50
55/-45
70/-70
45/-50
50/-50
80/-80
55
70
90
150
150
200
355
365
295
65/85
65/90
70/95
-95/345
-100/350
-105/375
85/-65
80/-65
55/-50
55/-60
60/-60
70/-70
60
70
95
220
225
125
535
550
375
80/110
80/110
85/115
-120/445
-125/450
-130/465
145/-100
140/-100
125/-90
70/-75
70/-75
75/-80
70
75
95
350
350
280
915
920
820
95/130
95/130
95/130
-145/545
-145/550
-150/555
205/-135
200/-130
190/-125
80/-85
80/-85
80/-85
75
80
95
480 1290
475 1290
435 1260
Good To Medium Reported Braking Action
1885
2000
2790
100/-105
105/-110
165/-180
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1600
1760
2765
REVERSE
THRUST
ADJ
25/-25
35/-35
80/-80
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2165
2240
2475
120/-125
125/-130
125/-135
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
150/-155
155/-155
150/-160
d
2485
2530
2685
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2800
2820
2890
180/-180
180/-180
175/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.26
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Asymmetry (Flap Lever 15 or 25)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1120
1420
2420
75/-60
70/-70
150/-160
75/-75
80/-85
150/-160
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/120
-45/155
-105/350
10/-10
0/0
35/-45
20/-20
30/-30
65/-65
35
60
90
20
0
105
45
5
105
35/45
40/50
70/95
-55/200
-60/210
-105/350
30/-25
30/-20
35/-45
35/-35
35/-35
65/-65
45
55
90
70
80
105
160
175
105
-75/265
-80/275
-110/370
55/-45
55/-40
55/-55
45/-45
45/-45
70/-70
55
65
90
135
140
125
325
335
180
-90/330
-95/335
-95/350
80/-65
75/-60
55/-40
50/-50
50/-55
55/-60
60
70
100
195
200
125
485
490
390
70/95
75/100
75/100
-115/430
-120/430
-120/440
140/-95
135/-95
120/-80
60/-65
60/-65
65/-70
70
75
95
310
315
275
825
825
780
85/115
85/115
85/115
-140/525
-140/525
-140/530
195/-125
195/-125
185/-115
70/-75
70/-75
70/-75
75
75
90
425 1165
425 1160
425 1165
ad
ed
1470
1570
2420
REVERSE
THRUST
ADJ
20/30
30/40
70/95
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1720
1790
2445
100/-100
100/-105
155/-165
45/60
50/65
75/95
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
1965
2010
2140
120/-120
120/-125
125/-130
55/75
60/80
60/80
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
145/-145
145/-150
150/-150
d
2245
2270
2350
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2525
2525
2555
170/-170
170/-170
170/-170
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.27
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Asymmetry (Flap Lever 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1080
1350
2250
60/-55
60/-65
140/-145
20/25
25/35
65/85
-35/120
-45/145
-100/335
10/-10
0/0
35/-45
70/-70
75/-80
140/-145
35/45
35/45
65/85
-55/195
-60/205
-100/335
35
55
85
20
0
95
35
5
100
30/-25
25/-20
35/-45
30/-30
35/-35
60/-60
45
55
85
65
70
95
140
155
100
45/60
45/60
65/90
-75/260
-75/265
-105/355
55/-45
50/-40
50/-55
40/-40
45/-45
60/-65
55
65
85
120
125
115
280
290
170
55/70
55/70
55/75
-90/325
-90/325
-95/340
75/-60
70/-55
55/-45
45/-50
50/-50
50/-55
60
70
85
170
175
115
415
425
340
65/90
65/90
65/90
-115/420
-115/420
-115/430
130/-90
130/-85
115/-80
55/-60
60/-60
60/-65
65
75
85
270
270
240
695
695
660
75/105
75/105
75/105
-135/510
-135/510
-135/515
180/-120
185/-115
175/-115
65/-70
65/-70
65/-70
70
80
80
365
365
365
970
965
975
Good To Medium Reported Braking Action
1640
1710
2275
90/-90
95/-100
140/-150
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1415
1505
2250
REVERSE
THRUST
ADJ
20/-20
30/-30
60/-60
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
1865
1910
2020
110/-110
115/-115
115/-120
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
135/-135
135/-135
140/-140
d
2120
2145
2215
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2370
2380
2410
155/-155
155/-155
160/-160
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.28
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Disagree (1 ≤ Indicated Flaps <15)
VREF40 + 30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1225
1625
2765
95/-60
70/-75
160/-175
75/-80
80/-85
160/-175
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-40/130
-50/170
-110/375
15/-10
0/0
55/-60
25/-25
35/-35
80/-80
40
65
90
25
0
180
55
5
220
40/55
45/55
85/110
-60/210
-65/220
-110/375
30/-30
25/-20
55/-60
35/-40
40/-40
80/-80
45
65
90
80
70
180
175
175
220
-80/280
-85/285
-115/400
60/-50
55/-45
70/-70
45/-50
50/-50
80/-80
55
70
90
150
150
200
355
365
295
-95/345
-100/350
-105/375
85/-65
80/-65
55/-50
55/-60
60/-60
70/-70
60
70
95
220
225
125
535
550
375
80/110
80/110
85/115
-120/445
-125/450
-130/465
145/-100
140/-100
125/-90
70/-75
70/-75
75/-80
70
75
95
350
350
280
915
920
820
95/130
95/130
95/130
-145/545
-145/550
-150/555
205/-135
200/-130
190/-125
80/-85
80/-85
80/-85
75
80
95
480 1290
475 1290
435 1260
ad
ed
1600
1760
2765
REVERSE
THRUST
ADJ
25/40
35/45
85/110
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1885
2000
2790
100/-105
105/-110
165/-180
55/70
55/75
85/115
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2165
2240
2475
120/-125
125/-130
125/-135
65/85
65/90
70/95
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
150/-155
155/-155
150/-160
d
2485
2530
2685
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2800
2820
2890
180/-180
180/-180
175/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.29
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Disagree (15 ≤ Indicated Flaps <30)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1120
1420
2420
75/-60
70/-70
150/-160
20/30
30/40
70/95
-35/120
-45/155
-105/350
10/-10
0/0
35/-45
75/-75
80/-85
150/-160
35/45
40/50
70/95
-55/200
-60/210
-105/350
35
60
90
20
0
105
45
5
105
30/-25
30/-20
35/-45
35/-35
35/-35
65/-65
45
55
90
70
80
105
160
175
105
45/60
50/65
75/95
-75/265
-80/275
-110/370
55/-45
55/-40
55/-55
45/-45
45/-45
70/-70
55
65
90
135
140
125
325
335
180
55/75
60/80
60/80
-90/330
-95/335
-95/350
80/-65
75/-60
55/-40
50/-50
50/-55
55/-60
60
70
100
195
200
125
485
490
390
70/95
75/100
75/100
-115/430
-120/430
-120/440
140/-95
135/-95
120/-80
60/-65
60/-65
65/-70
70
75
95
310
315
275
825
825
780
85/115
85/115
85/115
-140/525
-140/525
-140/530
195/-125
195/-125
185/-115
70/-75
70/-75
70/-75
75
75
90
425 1165
425 1160
425 1165
Good To Medium Reported Braking Action
1720
1790
2445
100/-100
100/-105
155/-165
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1470
1570
2420
REVERSE
THRUST
ADJ
20/-20
30/-30
65/-65
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
1965
2010
2140
120/-120
120/-125
125/-130
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
145/-145
145/-150
150/-150
d
2245
2270
2350
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2525
2525
2555
170/-170
170/-170
170/-170
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.30
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Disagree (30 ≤ Indicated Flaps <40)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1080
1350
2250
60/-55
60/-65
140/-145
70/-70
75/-80
140/-145
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/120
-45/145
-100/335
10/-10
0/0
35/-45
20/-20
30/-30
60/-60
35
55
85
20
0
95
35
5
100
35/45
35/45
65/85
-55/195
-60/205
-100/335
30/-25
25/-20
35/-45
30/-30
35/-35
60/-60
45
55
85
65
70
95
140
155
100
-75/260
-75/265
-105/355
55/-45
50/-40
50/-55
40/-40
45/-45
60/-65
55
65
85
120
125
115
280
290
170
-90/325
-90/325
-95/340
75/-60
70/-55
55/-45
45/-50
50/-50
50/-55
60
70
85
170
175
115
415
425
340
65/90
65/90
65/90
-115/420
-115/420
-115/430
130/-90
130/-85
115/-80
55/-60
60/-60
60/-65
65
75
85
270
270
240
695
695
660
75/105
75/105
75/105
-135/510
-135/510
-135/515
180/-120
185/-115
175/-115
65/-70
65/-70
65/-70
70
80
80
365
365
365
970
965
975
ad
ed
1415
1505
2250
REVERSE
THRUST
ADJ
20/25
25/35
65/85
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1640
1710
2275
90/-90
95/-100
140/-150
45/60
45/60
65/90
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
1865
1910
2020
110/-110
115/-115
115/-120
55/70
55/70
55/75
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
135/-135
135/-135
140/-140
d
2120
2145
2215
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2370
2380
2410
155/-155
155/-155
160/-160
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.31
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flaps Up Landing
VREF40 + 40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1325
1755
3130
110/-70
75/-75
175/-195
30/70
40/50
100/125
-40/140
-55/175
-120/400
15/-15
0/0
55/-65
85/-90
85/-95
175/-195
45/60
50/65
100/125
-65/225
-70/235
-120/400
40
70
105
30
0
170
65
10
180
40/-35
30/-20
55/-65
45/-45
45/-50
90/-90
50
70
105
95
90
170
210
220
180
60/80
65/85
100/130
-85/300
-90/305
-125/425
70/-60
65/-50
70/-75
55/-60
55/-60
90/-95
60
75
105
185
180
195
435
445
280
75/100
75/100
80/105
-105/370
-105/375
-115/395
100/-80
95/-75
60/-45
65/-70
65/-70
75/-80
65
75
115
270
270
160
655
665
485
95/125
95/125
95/130
-135/480
-135/480
-140/495
170/-120
170/-115
145/-95
80/-85
80/-85
85/-90
75
85
115
430 1135
430 1135
365 1040
110/150
110/150
110/150
-160/585
-160/585
-160/590
240/-160
240/-155
225/-140
90/-95
90/-95
95/-100
85
90
110
590 1610
585 1600
565 1595
Good To Medium Reported Braking Action
2105
2205
3160
110/-120
115/-120
180/-200
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1770
1920
3130
REVERSE
THRUST
ADJ
30/-30
40/-40
90/-90
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2435
2485
2715
135/-145
140/-145
135/-150
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
170/-180
175/-180
170/-180
d
2810
2830
2980
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3185
3175
3240
205/-210
205/-210
200/-205
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.32
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
Advisory
file
Highlight
Information
ADVISORY INFORMATION
Recommended Brake Cooling Schedule
Reference Brake Energy Per Brake (Millions of Foot Pounds)
180
10
67.3
69.5
70.5
71.4
73.2
74.8
76.3
59.7
61.6
62.5
63.4
64.9
66.2
67.4
51.8
53.6
54.4
55.1
56.5
57.5
58.3
44.1
45.5
46.2
46.8
48.0
48.8
49.3
36.4
37.6
38.2
38.7
39.7
40.2
40.6
0
60.8
62.8
63.7
64.6
66.2
67.5
68.7
54.9
56.7
57.5
58.3
59.8
60.9
61.8
48.1
49.7
50.4
51.1
52.3
53.2
53.9
40.9
42.2
42.8
43.4
44.5
45.2
45.7
33.7
34.8
35.3
35.8
36.7
37.2
37.5
5
69.6
71.9
72.9
73.9
75.7
77.4
79.0
62.7
64.8
65.7
66.5
68.2
69.6
70.9
54.8
56.6
57.4
58.2
59.6
60.7
61.7
46.4
48.0
48.7
49.3
50.6
51.4
52.1
38.2
39.5
40.0
40.6
41.6
42.2
42.6
10
81.2
83.9
85.1
86.2
88.4
90.5
92.9
72.9
75.4
76.4
77.4
79.4
81.2
83.0
63.5
65.6
66.5
67.4
69.1
70.5
71.9
53.6
55.4
56.2
56.9
58.4
59.4
60.3
43.9
45.4
46.0
46.6
47.8
48.6
49.1
or
pr
in
te
d
0
22.4
23.1
23.5
23.8
24.4
24.7
24.8
20.2
20.8
21.1
21.4
22.0
22.2
22.3
18.0
18.5
18.8
19.1
19.6
19.8
19.8
15.7
16.3
16.5
16.7
17.2
17.3
17.3
13.5
14.0
14.2
14.4
14.8
14.9
14.9
do
w
nl
o
10
19.3
20.0
20.2
20.5
21.1
21.3
21.3
17.5
18.1
18.4
18.6
19.1
19.3
19.3
15.7
16.3
16.5
16.7
17.2
17.3
17.3
14.0
14.4
14.7
14.9
15.2
15.4
15.4
12.3
12.7
12.9
13.1
13.4
13.5
13.5
if
5
17.0
17.6
17.8
18.1
18.5
18.7
18.7
15.4
15.9
16.2
16.4
16.8
17.0
17.0
13.9
14.3
14.6
14.8
15.1
15.3
15.3
12.3
12.7
12.9
13.1
13.4
13.6
13.6
10.8
11.2
11.4
11.5
11.8
11.9
11.9
d
0
15.1
15.6
15.8
16.0
16.4
16.6
16.6
13.7
14.2
14.4
14.6
14.9
15.1
15.1
12.3
12.7
12.9
13.1
13.4
13.6
13.5
11.0
11.3
11.5
11.6
11.9
12.1
12.0
9.6
10.0
10.1
10.2
10.5
10.6
10.6
nc
on
tro
lle
WEIGHT OAT
(1000 KG) (°C)
0
10
15
80
20
30
40
50
0
10
15
70
20
30
40
50
0
10
15
60
20
30
40
50
0
10
15
50
20
30
40
50
0
10
15
40
20
30
40
50
WIND CORRECTED BRAKES ON SPEED (KIAS)*
100
120
140
160
PRESSURE ALTITUDE (1000 FT)
5 10 0
5 10 0
5 10 0
5
25.3 28.9 30.9 35.0 40.2 40.4 45.9 53.0 50.8 57.9
26.1 29.8 31.9 36.2 41.5 41.8 47.5 54.8 52.5 59.9
26.5 30.3 32.4 36.7 42.1 42.4 48.2 55.6 53.3 60.7
26.9 30.7 32.8 37.2 42.7 42.9 48.8 56.3 54.0 61.5
27.6 31.5 33.7 38.2 43.8 44.0 50.0 57.7 55.3 63.1
27.9 31.9 34.1 38.7 44.4 44.7 50.9 58.8 56.3 64.3
28.0 32.1 34.3 39.0 44.9 45.2 51.5 59.7 57.1 65.4
22.8 26.0 27.7 31.3 35.9 36.1 41.0 47.2 45.3 51.6
23.5 26.8 28.6 32.4 37.1 37.3 42.3 48.7 46.8 53.3
23.9 27.2 29.0 32.8 37.6 37.8 43.0 49.4 47.5 54.0
24.2 27.6 29.4 33.3 38.1 38.4 43.5 50.1 48.1 54.8
24.8 28.3 30.2 34.1 39.1 39.3 44.6 51.4 49.3 56.1
25.1 28.6 30.5 34.6 39.6 39.9 45.3 52.2 50.1 57.1
25.2 28.8 30.7 34.8 40.0 40.2 45.8 52.9 50.7 58.0
20.3 23.1 24.4 27.6 31.6 31.7 35.9 41.2 39.6 45.0
20.9 23.8 25.2 28.5 32.6 32.7 37.1 42.6 40.9 46.5
21.2 24.2 25.6 29.0 33.1 33.2 37.6 43.2 41.5 47.1
21.5 24.5 26.0 29.4 33.5 33.6 38.1 43.8 42.0 47.8
22.1 25.1 26.6 30.1 34.4 34.5 39.1 44.9 43.1 49.0
22.3 25.4 26.9 30.5 34.9 35.0 39.7 45.6 43.8 49.8
22.4 25.5 27.0 30.6 35.1 35.2 40.0 46.0 44.2 50.4
17.7 20.2 21.2 23.9 27.3 27.2 30.8 35.3 33.8 38.3
18.3 20.8 21.9 24.7 28.2 28.1 31.8 36.5 34.9 39.6
18.6 21.1 22.2 25.1 28.6 28.6 32.3 37.0 35.4 40.2
18.9 21.4 22.5 25.4 29.0 28.9 32.8 37.5 35.9 40.7
19.3 22.0 23.1 26.1 29.7 29.7 33.6 38.4 36.8 41.8
19.5 22.2 23.4 26.4 30.1 30.1 34.0 39.0 37.4 42.4
19.6 22.3 23.4 26.5 30.3 30.2 34.2 39.3 37.6 42.8
15.2 17.3 17.9 20.2 23.0 22.8 25.8 29.4 28.1 31.8
15.8 17.9 18.5 20.9 23.8 23.6 26.6 30.4 29.0 32.8
16.0 18.1 18.8 21.2 24.1 23.9 27.0 30.8 29.4 33.3
16.2 18.4 19.1 21.5 24.5 24.2 27.4 31.3 29.8 33.8
16.6 18.9 19.6 22.1 25.1 24.9 28.1 32.1 30.6 34.6
16.8 19.1 19.8 22.3 25.4 25.2 28.4 32.5 31.0 35.1
16.8 19.1 19.8 22.3 25.5 25.2 28.6 32.7 31.1 35.3
ad
ed
80
U
*To correct for wind, enter table with the brakes on speed minus one half the headwind or plus 1.5 times the
tailwind. If ground speed is used for brakes on speed, ignore wind and enter table with sea level, 15°C.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.21.33
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Recommended Brake Cooling Schedule
Adjusted Brake Energy Per Brake (Millions of Foot Pounds)
No Reverse Thrust
REFERENCE BRAKE ENERGY PER BRAKE (MILLIONS OF FOOT POUNDS)
10
20
30
40
50
60
70
80
90
10
20
30
40
50
60
70
80
90
7.8
16.3
25.3
34.7
44.7
55.0
65.7
76.6
87.9
7.5
15.4
23.6
32.4
41.8
51.8
62.5
74.1
86.5
7.3
14.7
22.3
30.2
38.6
47.6
57.4
68.1
80.0
7.0
13.8
20.5
27.4
34.8
42.7
51.5
61.3
72.4
6.7
13.1
19.2
25.3
31.8
38.8
46.6
55.4
65.5
or
pr
in
te
d
LANDING
EVENT
RTO MAX MAN
MAX MAN
MAX AUTO
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
Two Engine Detent Reverse Thrust
REFERENCE BRAKE ENERGY PER BRAKE (MILLIONS OF FOOT POUNDS)
10
20
30
40
50
60
70
80
90
10
20
30
40
50
60
70
80
90
7.0
14.6
22.8
31.4
40.5
49.9
59.7
69.8
80.0
5.8
12.3
19.5
27.2
35.6
44.5
53.9
63.7
74.1
4.3
9.2
14.7
20.7
27.2
34.4
42.0
50.2
59.0
2.5
5.6
9.1
13.1
17.8
23.0
28.8
35.2
42.3
1.8
3.8
6.1
8.8
11.9
15.5
19.6
24.4
29.8
ad
ed
LANDING
EVENT
RTO MAX MAN
MAX MAN
MAX AUTO
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
EVENT ADJUSTED BRAKE ENERGY (MILLIONS OF FOOT POUNDS)
16 & BELOW
17
20
23
25
28
32
33 TO 48
49 & ABOVE
BRAKE TEMPERATURE MONITOR SYSTEM INDICATION ON CDS
UP TO 2.4
2.6
3.1
3.5
3.9
4.4
4.9
5.0 TO 7.5
7.5 & ABOVE
NO SPECIAL
1
2
3
4
5
6
FUSE PLUG
PROCEDURE
CAUTION
MELT ZONE
REQUIRED
10
20
30
40
50
60
if
INFLIGHT
GEAR DOWN
GROUND
do
w
nl
o
Cooling Time (Minutes) - Category C Steel Brakes
Cooling Time (Minutes) - Category N Carbon Brakes
on
tro
lle
d
EVENT ADJUSTED BRAKE ENERGY (MILLIONS OF FOOT POUNDS)
16 & BELOW
17
19
20.9 23.5 26.9 29.4
30 TO 41
41 & ABOVE
BRAKE TEMPERATURE MONITOR SYSTEM INDICATION ON CDS
UP TO 2.5
2.6
3
3.3
3.8
4.5
4.9
5.0 TO 7.1
7.1 & ABOVE
NO SPECIAL
1
4
5
6
7
7.6
FUSE PLUG
PROCEDURE
CAUTION
MELT ZONE
REQUIRED
6.7
16.0 24.1 34.2 45.9 53.3
INFLIGHT
GEAR DOWN
GROUND
U
nc
Observe maximum quick turnaround limit.
Table shows energy per brake added by a single stop with all brakes operating. Energy is assumed to be
equally distributed among the operating brakes. Total energy is the sum of residual energy plus energy
added.
Add 1.0 million foot pounds per brake for each taxi mile.
When in caution zone, wheel fuse plugs may melt. Delay takeoff and inspect after one hour. If overheat occurs
after takeoff, extend gear soon for at least 7 minutes.
When in fuse plug melt zone, clear runway immediately. Unless required, do not set parking brake. Do not
approach gear or attempt to taxi for one hour. Tire, wheel and brake replacement may be required. If
overheat occurs after takeoff, extend gear soon for at least 12 minutes.
Brake temperature monitor system (BTMS) indication on CDS systems page may be used 10 to 15 minutes
after airplane has come to a complete stop or inflight with gear retracted to determine recommended cooling
schedule.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.21.34
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Engine Inoperative
Section 22
Engine
file
Highlight
Inoperative
ENGINE INOP
Engine Inoperative
Engine Inoperative
Initial Max Continuous %N1
Based on .79M, A/C high and anti-ice off
27
95.9
96.5
97.2
97.9
98.1
97.3
96.5
95.8
95.0
94.2
93.4
92.6
91.8
29
95.6
96.2
96.8
97.6
98.5
98.5
97.7
96.9
96.2
95.4
94.6
93.7
92.9
PRESSURE ALTITUDE (1000 FT)
31
33
35
37
95.5
95.2
94.8
94.3
96.1
96.0
95.5
95.1
96.7
96.7
96.2
95.8
97.4
97.4
97.0
96.6
98.3
98.2
97.8
97.5
99.2
99.1
98.6
98.3
99.0
99.9
99.5
99.2
98.2
99.5
100.4
100.1
97.4
98.7
99.8
100.4
96.6
97.9
99.0
99.6
95.8
97.0
98.2
98.7
94.9
96.2
97.3
97.9
94.1
95.3
96.5
97.0
25
-1.2
-4.2
41
93.2
94.1
95.0
95.9
96.8
97.8
98.7
99.7
100.0
99.2
98.3
97.5
96.6
27
-1.1
-4.4
PRESSURE ALTITUDE (1000 FT)
29
31
33
35
37
-1.0
-0.9
-0.8
-0.8
-0.8
-4.5
-4.7
-5.0
-4.8
-4.8
39
-0.8
-4.8
41
-0.8
-4.8
U
nc
on
tro
lle
d
if
ENGINE ANTI-ICE
ENGINE & WING ANTI-ICE
do
w
nl
o
%N1 Adjustments for Engine Bleeds
BLEED CONFIGURATION
39
94.0
94.8
95.6
96.4
97.2
98.1
99.0
99.9
100.2
99.4
98.5
97.7
96.8
or
pr
in
te
d
20
15
10
5
0
-5
-10
-15
-20
-25
-30
-35
-40
25
96.1
96.7
97.3
97.5
96.8
96.0
95.2
94.4
93.6
92.8
91.9
91.1
90.3
ad
ed
TAT (°C)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.22.1
Performance Inflight - QRH
Engine Inoperative
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
Max Continuous %N1
37000 FT to 29000 FT Pressure Altitudes
-35
99.6
98.9
98.0
97.2
-30
98.9
99.8
98.8
98.1
-50
96.8
96.4
95.3
94.0
-45
97.7
97.3
96.2
94.9
-40
98.6
98.2
97.1
95.8
-35
99.5
99.1
98.0
96.6
-30
99.2
100.0
98.8
97.5
-45
97.7
97.3
96.2
94.5
93.9
-40
98.5
98.2
97.1
95.4
94.7
-35
99.4
99.1
97.9
96.2
95.6
-30
100.2
99.9
98.8
97.1
96.4
-25
99.3
100.8
99.6
97.9
97.2
-45
97.6
97.3
95.9
94.0
92.6
-40
98.5
98.2
96.8
94.9
93.5
-35
99.4
99.1
97.6
95.7
94.3
-30
100.3
100.0
98.5
96.6
95.1
-25
100.4
100.8
99.3
97.4
95.9
-40
98.4
97.8
96.5
94.4
92.3
92.3
-35
99.3
98.7
97.4
95.2
93.1
93.1
-30
100.1
99.5
98.2
96.1
93.9
93.9
-25
101.0
100.4
99.1
96.9
94.7
94.7
-20
100.5
101.2
99.9
97.7
95.5
95.5
TAT (°C)
-25
98.1
99.5
99.7
98.9
TAT (°C)
-25
98.4
99.9
99.6
98.3
TAT (°C)
-20
98.5
99.9
100.4
98.7
98.1
TAT (°C)
-20
99.5
101.0
100.2
98.2
96.7
TAT (°C)
-15
99.6
100.7
100.7
98.5
96.3
96.3
if
d
-20
96.9
98.7
100.1
99.7
-15
95.6
97.8
99.3
100.5
-10
94.0
96.8
98.5
100.2
-5
92.5
95.6
97.7
99.3
0
91.1
94.5
96.7
98.5
-15
96.1
98.0
99.5
99.9
-10
94.7
97.0
98.9
99.7
-5
93.3
95.8
98.0
98.9
0
92.0
94.7
97.0
98.1
-10
96.0
98.0
99.6
99.9
99.7
-5
94.6
96.8
98.7
99.1
100.4
0
93.2
95.6
97.7
98.2
100.0
5
92.0
94.5
96.7
97.4
99.2
-15
98.5
100.1
100.7
99.0
97.5
-10
97.3
99.1
99.9
99.8
98.3
-5
95.9
98.0
99.1
99.1
99.1
0
94.5
96.7
98.1
98.2
99.3
5
93.2
95.5
97.1
97.3
98.4
-10
98.5
99.7
100.4
99.3
97.0
97.0
-5
97.2
98.7
99.5
99.4
97.8
97.8
0
95.7
97.5
98.6
98.5
98.6
98.6
5
94.4
96.2
97.5
97.5
97.8
99.3
10
93.1
95.1
96.6
96.8
97.0
99.4
-20
97.3
98.9
100.2
99.1
-15
97.3
99.0
100.2
99.5
98.9
or
pr
in
te
d
-40
98.7
98.1
97.1
96.4
ad
ed
-45
97.9
97.2
96.2
95.5
do
w
nl
o
-50
97.0
96.3
95.3
94.6
on
tro
lle
37000 FT PRESS ALT
KIAS M
-55
160
.51
96.0
200
.63
95.4
240
.74
94.4
280
.86
93.7
35000 FT PRESS ALT
KIAS M
-55
160
.49
95.9
200
.60
95.5
240
.71
94.4
280
.82
93.2
33000 FT PRESS ALT
KIAS M
-50
160
.47
96.8
200
.58
96.4
240
.68
95.3
280
.79
93.6
320
.89
93.0
31000 FT PRESS ALT
KIAS M
-50
160
.45
96.7
200
.55
96.5
240
.66
95.0
280
.76
93.2
320
.85
91.8
29000 FT PRESS ALT
KIAS M
-45
160
.43
97.5
200
.53
96.9
240
.63
95.7
280
.73
93.6
320
.82
91.4
360
.91
91.4
%N1 Adjustments for Engine Bleeds
BLEED CONFIGURATION
PRESSURE ALTITUDE (1000 FT)
31
33
35
-0.9
-0.8
-0.8
-4.3
-4.5
-4.7
37
-0.8
-4.7
U
nc
ENGINE ANTI-ICE ON
ENGINE & WING ANTI-ICE ON
29
-0.9
-4.1
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.22.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Engine Inoperative
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
Max Continuous %N1
27000 FT to 20000 FT Pressure Altitudes
-30
100.0
98.9
97.6
95.5
93.4
92.7
-25
100.8
99.8
98.4
96.3
94.2
93.5
-20
101.5
100.6
99.2
97.1
95.0
94.3
-35
99.0
97.7
95.9
94.1
91.8
90.5
-30
99.9
98.5
96.8
94.9
92.6
91.3
-25
100.7
99.4
97.6
95.7
93.4
92.1
-20
101.6
100.2
98.4
96.5
94.2
93.0
-15
101.7
101.0
99.2
97.3
95.0
93.8
-35
98.5
97.2
95.6
93.8
91.4
89.8
-30
99.4
98.1
96.4
94.6
92.3
90.7
-25
100.3
98.9
97.2
95.4
93.1
91.5
-20
101.1
99.7
98.0
96.2
93.9
92.4
-30
98.4
97.1
95.6
94.0
91.8
89.9
-25
99.2
98.0
96.4
94.8
92.6
90.7
-20
100.1
98.8
97.2
95.6
93.4
91.6
-15
100.9
99.6
98.0
96.4
94.2
92.4
-10
101.0
100.4
98.8
97.1
95.0
93.2
-30
97.4
96.2
94.7
93.3
91.1
89.3
-25
98.2
97.0
95.5
94.1
92.0
90.2
-20
99.0
97.9
96.3
94.8
92.8
91.0
-15
99.8
98.7
97.1
95.6
93.6
91.8
-10
100.6
99.4
97.9
96.4
94.4
92.6
nc
TAT (°C)
-15
100.6
101.1
100.1
97.9
95.7
95.1
TAT (°C)
-10
100.7
100.9
100.0
98.1
95.8
94.6
TAT (°C)
-10
100.8
101.0
99.6
97.8
95.5
94.0
TAT (°C)
-5
99.9
100.1
99.6
97.9
95.8
94.0
TAT (°C)
-5
100.2
100.2
98.7
97.2
95.2
93.5
-15
101.9
100.6
98.8
97.0
94.7
93.2
do
w
nl
o
if
d
-10
99.6
100.2
100.7
98.7
96.5
95.9
-5
98.4
99.2
99.7
99.4
97.3
96.6
0
97.0
98.1
98.7
98.7
98.0
97.4
5
95.7
96.9
97.7
97.7
97.9
98.2
10
94.4
95.7
96.8
96.9
97.2
98.7
-5
99.6
99.9
99.8
98.8
96.6
95.4
0
98.4
98.9
98.9
98.9
97.3
96.2
5
97.0
97.7
97.9
97.9
97.9
97.0
10
95.8
96.6
96.9
96.9
97.2
97.7
15
94.5
95.5
96.0
96.2
96.5
97.5
-5
99.7
99.9
99.9
98.6
96.3
94.8
0
98.5
98.9
99.0
99.1
97.1
95.6
5
97.2
97.8
97.9
98.0
97.8
96.4
10
96.0
96.7
97.0
97.0
97.2
97.2
15
94.7
95.6
96.1
96.3
96.5
97.2
0
98.7
98.9
99.1
98.7
96.6
94.8
5
97.5
97.8
98.1
98.4
97.4
95.6
10
96.3
96.8
97.1
97.4
97.5
96.4
15
95.2
95.8
96.2
96.6
96.8
97.0
20
94.0
94.8
95.4
95.8
96.1
96.4
0
98.9
99.1
99.3
97.9
96.0
94.3
5
97.7
97.8
98.2
98.5
96.8
95.1
10
96.6
96.8
97.1
97.6
97.6
95.8
15
95.5
95.8
96.2
96.7
96.9
96.6
20
94.4
94.9
95.4
95.9
96.2
96.4
or
pr
in
te
d
-35
99.1
98.1
96.7
94.6
92.6
91.8
ad
ed
-40
98.2
97.2
95.9
93.8
91.7
91.0
on
tro
lle
27000 FT PRESS ALT
KIAS M
-45
160
.41
97.3
200
.51
96.3
240
.60
95.0
280
.70
93.0
320
.79
90.9
360
.88
90.2
25000 FT PRESS ALT
KIAS M
-40
160
.39
98.2
200
.49
96.8
240
.58
95.1
280
.67
93.2
320
.76
90.9
360
.85
89.6
24000 FT PRESS ALT
KIAS M
-40
160
.38
97.7
200
.48
96.4
240
.57
94.7
280
.66
93.0
320
.75
90.6
360
.83
89.0
22000 FT PRESS ALT
KIAS M
-35
160
.37
97.5
200
.46
96.3
240
.55
94.8
280
.63
93.2
320
.72
90.9
360
.80
89.0
20000 FT PRESS ALT
KIAS M
-35
160
.35
96.5
200
.44
95.4
240
.53
93.9
280
.61
92.4
320
.69
90.3
360
.77
88.5
U
%N1 Adjustments for Engine Bleeds
BLEED CONFIGURATION
ENGINE ANTI-ICE ON
ENGINE & WING ANTI-ICE ON
20
-0.9
-3.6
PRESSURE ALTITUDE (1000 FT)
22
24
25
-0.9
-1.0
-1.0
-3.8
-3.8
-3.9
27
-1.0
-4.0
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.22.3
Performance Inflight - QRH
Engine Inoperative
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
Max Continuous %N1
18000 FT to 12000 FT Pressure Altitudes
-15
98.4
97.5
96.0
94.5
92.8
91.2
-10
99.2
98.2
96.8
95.3
93.6
92.0
-5
100.0
99.0
97.6
96.1
94.4
92.8
-25
95.8
94.7
93.3
91.8
90.3
88.9
-20
96.6
95.5
94.1
92.6
91.1
89.7
-15
97.4
96.3
94.9
93.5
91.9
90.6
-10
98.2
97.1
95.7
94.3
92.8
91.4
-5
99.0
97.8
96.5
95.1
93.6
92.2
-20
95.7
94.4
92.9
91.7
90.4
89.1
-15
96.5
95.2
93.8
92.5
91.2
89.9
-10
97.3
96.0
94.6
93.4
92.1
90.7
-5
98.0
96.7
95.4
94.2
92.9
91.6
0
98.8
97.5
96.2
95.0
93.7
92.4
-15
95.6
93.5
92.5
91.4
90.3
89.1
-10
96.4
94.3
93.3
92.2
91.2
90.0
-5
97.1
95.1
94.1
93.0
92.0
90.8
0
97.9
95.9
94.9
93.8
92.8
91.6
5
98.6
96.7
95.7
94.6
93.6
92.4
TAT (°C)
0
98.9
99.3
98.3
96.8
95.2
93.6
TAT (°C)
0
99.4
98.6
97.2
95.9
94.4
93.0
TAT (°C)
5
99.2
98.3
96.9
95.8
94.5
93.2
TAT (°C)
10
97.9
97.1
96.4
95.4
94.4
93.2
do
w
nl
o
if
d
5
97.5
98.0
98.2
97.6
96.0
94.4
10
96.5
96.7
97.1
97.5
96.8
95.2
15
95.5
95.9
96.2
96.6
96.9
96.0
20
94.5
95.0
95.4
95.8
96.2
96.4
25
93.5
94.1
94.6
95.1
95.5
95.8
10
97.0
97.0
97.3
97.4
95.9
94.6
15
96.1
96.0
96.3
96.7
96.7
95.4
20
95.2
95.2
95.5
95.8
96.1
96.2
25
94.2
94.4
94.7
95.1
95.5
95.8
10
98.2
97.5
97.4
96.5
95.3
94.0
15
97.3
96.5
96.5
96.8
96.1
94.8
20
96.4
95.7
95.6
96.0
96.2
95.5
25
95.5
94.9
94.8
95.2
95.5
95.8
30
94.6
94.1
94.1
94.5
94.8
95.2
15
96.8
96.1
96.4
96.2
95.2
93.9
20
95.9
95.1
95.5
95.9
96.0
94.7
25
95.2
94.4
94.7
95.1
95.5
95.5
30
94.4
93.6
94.0
94.4
94.8
95.1
35
93.5
92.8
93.2
93.7
94.1
94.4
5
98.2
98.2
98.0
96.6
95.2
93.8
or
pr
in
te
d
-20
97.6
96.7
95.2
93.7
92.0
90.4
ad
ed
-25
96.8
95.9
94.5
92.9
91.1
89.5
on
tro
lle
18000 FT PRESS ALT
KIAS M
-30
160
.34
96.0
200
.42
95.1
240
.51
93.7
280
.59
92.0
320
.67
90.3
360
.75
88.7
16000 FT PRESS ALT
KIAS M
-30
160
.33
95.0
200
.41
93.9
240
.49
92.5
280
.57
91.0
320
.64
89.4
360
.72
88.0
14000 FT PRESS ALT
KIAS M
-25
160
.31
94.9
200
.39
93.6
240
.47
92.1
280
.54
90.9
320
.62
89.6
360
.69
88.3
12000 FT PRESS ALT
KIAS M
-20
160
.30
94.8
200
.38
92.7
240
.45
91.6
280
.52
90.6
320
.60
89.5
360
.67
88.3
%N1 Adjustments for Engine Bleeds
12
-0.9
-3.2
PRESSURE ALTITUDE (1000 FT)
14
16
-0.9
-0.9
-3.4
-3.4
18
-0.9
-3.5
U
nc
BLEED
CONFIGURATION
ENGINE ANTI-ICE ON
ENGINE & WING ANTI-ICE ON
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.22.4
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Engine Inoperative
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
Max Continuous %N1
10000 FT to 1000 FT Pressure Altitudes
-5
95.2
93.8
92.8
91.9
91.0
90.0
0
95.9
94.6
93.6
92.7
91.8
90.8
5
96.7
95.4
94.4
93.5
92.6
91.6
-5
91.4
90.8
90.0
89.3
88.6
87.7
0
92.2
91.6
90.8
90.1
89.4
88.5
5
93.0
92.4
91.6
90.9
90.2
89.3
10
93.8
93.2
92.4
91.7
90.9
90.1
15
94.5
93.9
93.2
92.5
91.7
90.8
0
91.3
90.7
89.6
89.1
88.4
87.6
5
92.1
91.5
90.4
89.9
89.2
88.4
10
92.8
92.3
91.2
90.6
90.0
89.1
15
93.6
93.1
92.0
91.4
90.7
89.9
0
89.8
89.5
88.6
88.1
87.5
86.7
5
90.6
90.3
89.4
88.8
88.2
87.5
10
91.4
91.0
90.2
89.6
89.0
88.2
15
92.2
91.8
90.9
90.4
89.8
89.0
TAT (°C)
10
97.5
96.1
95.2
94.3
93.4
92.3
TAT (°C)
20
95.1
94.7
93.9
93.3
92.5
91.6
TAT (°C)
25
94.6
94.6
93.5
92.9
92.2
91.4
TAT (°C)
25
93.7
93.3
92.5
91.9
91.3
90.5
20
94.4
93.8
92.7
92.2
91.5
90.6
do
w
nl
o
if
d
15
96.5
96.1
95.9
95.1
94.2
93.1
20
95.6
95.2
95.4
95.7
95.0
93.9
25
94.9
94.4
94.6
95.0
95.4
94.7
30
94.2
93.7
93.8
94.2
94.7
95.0
35
93.4
92.9
93.1
93.5
93.9
94.3
25
94.4
94.4
94.4
94.0
93.2
92.3
30
93.6
93.7
93.7
94.0
94.0
93.1
35
92.9
93.0
92.9
93.2
93.6
93.8
40
92.2
92.3
92.2
92.5
92.9
93.3
45
91.4
91.5
91.5
91.8
92.2
92.6
30
93.9
94.0
93.5
93.7
93.0
92.1
35
93.2
93.3
92.8
93.1
93.5
92.8
40
92.4
92.5
92.0
92.4
92.8
93.1
45
91.6
91.8
91.3
91.7
92.0
92.4
50
90.7
91.0
90.6
91.0
91.3
91.7
30
93.4
93.7
93.2
92.6
92.0
91.2
35
92.7
93.0
92.8
93.1
92.7
91.9
40
91.9
92.2
92.0
92.3
92.7
92.6
45
91.2
91.5
91.3
91.6
91.9
92.3
50
90.3
90.7
90.6
90.9
91.2
91.6
or
pr
in
te
d
-10
94.4
93.0
92.0
91.1
90.2
89.2
ad
ed
-15
93.5
92.1
91.1
90.3
89.4
88.3
on
tro
lle
10000 FT PRESS ALT
KIAS M
-20
160
.29
92.7
200
.36
91.3
240
.43
90.3
280
.51
89.5
320
.58
88.6
360
.65
87.5
5000 FT PRESS ALT
KIAS M
-10
160
.26
90.5
200
.33
90.0
240
.40
89.2
280
.46
88.5
320
.53
87.8
360
.59
86.9
3000 FT PRESS ALT
KIAS M
-5
160
.26
90.5
200
.32
89.9
240
.38
88.8
280
.45
88.3
320
.51
87.6
360
.57
86.8
1000 FT PRESS ALT
KIAS M
-5
160
.25
89.0
200
.31
88.7
240
.37
87.8
280
.43
87.3
320
.49
86.7
360
.55
85.9
20
92.9
92.6
91.7
91.1
90.5
89.7
%N1 Adjustments for Engine Bleeds
1
-0.6
-2.9
PRESSURE ALTITUDE (1000 FT)
3
5
-0.8
-0.8
-3.0
-2.7
10
-0.8
-3.2
U
nc
BLEED
CONFIGURATION
ENGINE ANTI-ICE ON
ENGINE & WING ANTI-ICE ON
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.22.5
Performance Inflight - QRH
Engine Inoperative
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
MAX CONTINUOUS THRUST
Driftdown Speed/Level Off Altitude
100 ft/min residual rate of climb
OPTIMUM
DRIFTDOWN
SPEED (KIAS)
269
262
254
246
238
229
219
209
199
187
U
nc
on
tro
lle
d
if
do
w
nl
o
ad
ed
Includes APU fuel burn.
LEVEL OFF ALTITUDE (FT)
ISA + 10°C
ISA + 15°C
ISA + 20°C
& BELOW
16300
14700
12300
18400
16800
14900
20400
19000
17300
22500
21200
19700
24700
23500
22100
26800
25800
24600
29100
28100
27000
31200
30400
29400
33300
32600
31700
35600
34900
34000
or
pr
in
te
d
WEIGHT (1000 KG)
START
LEVEL OFF
DRIFTDOWN
85
81
80
76
75
72
70
67
65
62
60
57
55
53
50
48
45
43
40
38
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.22.6
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Engine Inoperative
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
MAX CONTINUOUS THRUST
Driftdown/LRC Cruise Range Capability
Ground to Air Miles Conversion
or
pr
in
te
d
AIR DISTANCE (NM)
TAILWIND COMPONENT (KTS)
20
40
60
80
100
95
90
86
82
78
190
180
172
164
157
284
270
258
246
235
379
360
344
328
314
474
451
429
410
392
569
541
515
492
471
664
631
601
574
549
758
721
687
656
628
853
811
773
738
706
948
901
859
820
785
1043
991
945
902
863
1138
1081
1030
984
942
1232
1171
1116
1066
1020
1327
1261
1202
1148
1098
1422
1351
1288
1230
1177
1517
1441
1373
1312
1255
1611
1531
1459
1393
1333
1706
1621
1545
1475
1411
ad
ed
GROUND
DISTANCE
(NM)
100
200
300
400
500
600
700
800
900
1000
1100
1200
1300
1400
1500
1600
1700
1800
do
w
nl
o
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
100
80
60
40
20
138
128
120
112
106
275
256
239
225
212
413
384
359
337
317
551
512
479
449
423
689
640
598
562
529
826
768
718
674
635
964
896
838
786
741
1102
1025
957
898
846
1240
1153
1077
1011
952
1377
1281
1197
1123
1058
1515
1409
1317
1235
1164
1653
1537
1436
1348
1270
1792
1666
1556
1460
1375
1930
1794
1676
1573
1481
2068
1922
1796
1685
1587
2207
2051
1916
1798
1693
2345
2180
2036
1910
1799
2484
2309
2156
2023
1905
Driftdown/Cruise Fuel and Time
45
0.4
0.8
1.3
1.8
2.2
2.7
3.1
3.6
4.0
4.4
4.8
5.3
5.7
6.1
6.5
6.9
7.3
7.7
if
40
0.4
0.8
1.2
1.6
2.0
2.4
2.8
3.2
3.6
4.0
4.4
4.8
5.2
5.5
5.9
6.3
6.6
7.0
U
nc
on
tro
lle
100
200
300
400
500
600
700
800
900
1000
1100
1200
1300
1400
1500
1600
1700
1800
FUEL REQUIRED (1000 KG)
WEIGHT AT START OF DRIFTDOWN (1000 KG)
50
55
60
65
70
75
0.4
0.4
0.4
0.5
0.5
0.5
0.9
0.9
1.0
1.0
1.1
1.1
1.4
1.5
1.6
1.7
1.7
1.8
1.9
2.0
2.2
2.3
2.4
2.6
2.4
2.6
2.8
3.0
3.1
3.3
2.9
3.1
3.3
3.6
3.8
4.0
3.4
3.6
3.9
4.2
4.4
4.7
3.9
4.2
4.5
4.8
5.0
5.4
4.3
4.7
5.0
5.4
5.7
6.0
4.8
5.2
5.6
6.0
6.3
6.7
5.3
5.7
6.1
6.6
6.9
7.4
5.7
6.2
6.7
7.1
7.6
8.1
6.2
6.7
7.2
7.7
8.2
8.7
6.6
7.2
7.7
8.3
8.8
9.4
7.1
7.7
8.3
8.9
9.4
10.0
7.5
8.2
8.8
9.4
10.0
10.7
8.0
8.6
9.3
10.0
10.6
11.3
8.4
9.1
9.8
10.5
11.2
12.0
d
AIR DIST
(NM)
80
0.5
1.2
1.9
2.7
3.5
4.2
5.0
5.7
6.4
7.1
7.8
8.6
9.3
10.0
10.7
11.3
12.0
12.7
85
0.5
1.2
2.0
2.9
3.7
4.5
5.2
6.0
6.8
7.6
8.3
9.1
9.8
10.6
11.3
12.1
12.8
13.5
TIME
(HR:MIN)
0:17
0:33
0:50
1:06
1:23
1:39
1:56
2:12
2:29
2:46
3:02
3:19
3:36
3:52
4:09
4:26
4:43
4:59
Includes APU fuel burn.
Driftdown at optimum driftdown speed and cruise at long range cruise speed.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.22.7
Performance Inflight - QRH
Engine Inoperative
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Altitude Capability
100 ft/min residual rate of climb
85
80
75
70
65
60
55
50
45
40
ISA + 10°C & BELOW
9500
12400
15300
18400
21100
23700
26300
29000
31400
33800
PRESSURE ALTITUDE (FT)
ISA + 15°C
6400
9500
12800
15800
18600
21800
24700
27700
30500
33000
U
nc
on
tro
lle
d
if
do
w
nl
o
ad
ed
With engine anti-ice on, decrease altitude capability by 2000 ft.
With engine and wing anti-ice on, decrease altitude capability by 6500 ft.
ISA + 20°C
3400
6500
9800
13200
16300
19400
22400
25800
29200
31800
or
pr
in
te
d
WEIGHT (1000 KG)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.22.8
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Engine Inoperative
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
Long Range Cruise Control
94.0
.593
288
2674
92.3
.582
283
2520
90.4
.563
274
2330
88.3
.543
263
2139
85.9
.520
252
1950
83.4
.495
239
1762
80.6
.469
227
1582
77.8
.445
215
1416
if
29
31
93.9
.596
268
2295
91.9
.585
263
2143
89.5
.563
253
1953
87.0
.538
241
1764
84.1
.511
228
1577
81.0
.480
214
1392
93.7
.597
258
2114
91.4
.585
252
1958
88.7
.561
241
1767
85.9
.533
229
1580
82.8
.502
215
1394
96.4
.614
254
2146
93.3
.597
247
1938
90.7
.583
241
1777
87.7
.556
229
1586
84.6
.525
216
1400
96.2
.614
244
1971
92.7
.596
236
1765
89.7
.578
229
1600
86.4
.548
216
1410
95.7
.613
233
1793
91.8
.593
225
1593
88.3
.571
216
1421
94.8
.610
222
1613
90.7
.589
214
1424
U
nc
94.0
.595
278
2481
92.2
.584
273
2330
90.0
.564
263
2140
87.7
.541
252
1950
85.2
.516
240
1762
82.3
.489
227
1575
79.4
.462
214
1402
27
or
pr
in
te
d
94.0
.590
299
2870
92.5
.579
293
2709
90.7
.562
284
2518
88.7
.542
274
2327
86.5
.521
263
2137
84.2
.498
251
1948
81.6
.475
239
1764
79.1
.452
227
1594
76.2
.429
215
1434
PRESSURE ALTITUDE (1000 FT)
19
21
23
25
ad
ed
17
do
w
nl
o
15
d
10
91.8
.561
311
3067
90.1
.545
302
2875
88.4
.528
293
2684
86.5
.510
282
2494
84.5
.491
271
2306
82.3
.471
261
2124
80.2
.453
250
1954
77.8
.434
240
1791
75.5
.415
229
1636
73.0
.395
218
1485
on
tro
lle
WEIGHT
(1000 KG)
%N1
MACH
85
KIAS
FF/ENG
%N1
MACH
80
KIAS
FF/ENG
%N1
MACH
75
KIAS
FF/ENG
%N1
MACH
70
KIAS
FF/ENG
%N1
MACH
65
KIAS
FF/ENG
%N1
MACH
60
KIAS
FF/ENG
%N1
MACH
55
KIAS
FF/ENG
%N1
MACH
50
KIAS
FF/ENG
%N1
MACH
45
KIAS
FF/ENG
%N1
MACH
40
KIAS
FF/ENG
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.22.9
Performance Inflight - QRH
Engine Inoperative
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Diversion Fuel and Time
Ground to Air Miles Conversion
GROUND
DISTANCE
(NM)
200
400
600
800
1000
1200
1400
1600
1800
2000
AIR DISTANCE (NM)
TAILWIND COMPONENT (KTS)
20
40
60
80
100
190
180
172
164
158
379
361
344
328
315
570
542
517
494
473
759
721
687
657
630
949
902
859
820
786
1139
1082
1031
984
943
1328
1262
1202
1147
1099
1518
1442
1373
1311
1256
1707
1622
1544
1474
1412
1896
1801
1715
1637
1568
or
pr
in
te
d
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
100
80
60
40
20
298
272
249
230
214
600
547
501
462
429
903
823
753
694
644
1209
1100
1005
926
859
1516
1379
1259
1159
1075
1825
1659
1513
1393
1290
2137
1940
1768
1626
1506
2450
2222
2024
1860
1722
2766
2507
2281
2095
1938
3083
2792
2539
2331
2155
ad
ed
Reference Fuel and Time Required at Check Point
PRESSURE ALTITUDE (1000 FT)
18
22
26
FUEL
TIME
FUEL
TIME
FUEL
TIME
FUEL
TIME
FUEL
TIME
(1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN)
200
1.4
0:43
1.2
0:41
1.1
0:39
1.0
0:38
0.9
0:37
400
2.8
1:23
2.6
1:19
2.4
1:14
2.2
1:11
2.1
1:09
600
4.3
2:04
3.9
1:57
3.6
1:50
3.4
1:45
3.2
1:42
800
5.7
2:46
5.2
2:36
4.9
2:26
4.5
2:19
4.4
2:14
1000
7.1
3:28
6.6
3:15
6.1
3:03
5.7
2:53
5.5
2:47
1200
8.5
4:10
7.9
3:55
7.3
3:40
6.8
3:28
6.6
3:21
1400
9.8
4:53
9.1
4:36
8.5
4:18
8.0
4:02
7.7
3:54
1600
11.2
5:36
10.4
5:16
9.7
4:55
9.1
4:38
8.7
4:28
1800
12.5
6:20
11.7
5:58
10.9
5:34
10.2
5:13
9.8
5:02
2000
13.9
7:05
12.9
6:39
12.0
6:13
11.3
5:49
10.8
5:36
AIR
DIST
(NM)
14
on
tro
lle
d
if
do
w
nl
o
10
Fuel Required Adjustments (1000 KG)
U
nc
REFERENCE FUEL REQUIRED
(1000 KG)
1
2
3
4
5
6
7
8
9
10
11
12
13
14
40
-0.1
-0.3
-0.4
-0.6
-0.7
-0.8
-1.0
-1.1
-1.3
-1.4
-1.6
-1.7
-1.9
-2.0
45
-0.1
-0.2
-0.3
-0.4
-0.5
-0.6
-0.8
-0.9
-1.0
-1.1
-1.2
-1.3
-1.4
-1.5
WEIGHT AT CHECK POINT (1000 KG)
50
55
60
65
70
-0.1
0.0
0.0
0.1
0.1
-0.1
-0.1
0.0
0.2
0.3
-0.2
-0.1
0.0
0.3
0.5
-0.3
-0.1
0.0
0.3
0.7
-0.4
-0.2
0.0
0.4
0.9
-0.4
-0.2
0.0
0.5
1.1
-0.5
-0.3
0.0
0.6
1.2
-0.6
-0.3
0.0
0.6
1.4
-0.7
-0.3
0.0
0.7
1.5
-0.7
-0.4
0.0
0.7
1.6
-0.8
-0.4
0.0
0.8
1.7
-0.9
-0.4
0.0
0.8
1.9
-0.9
-0.5
0.0
0.9
2.0
-1.0
-0.5
0.0
0.9
2.0
75
0.2
0.6
0.9
1.2
1.4
1.7
2.0
2.2
2.4
2.6
2.8
3.0
3.2
3.4
80
0.3
0.8
1.2
1.6
2.0
2.4
2.8
3.2
3.5
3.8
4.1
4.4
4.7
4.9
Includes APU fuel burn.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.22.10
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Engine Inoperative
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
MAX CONTINUOUS THRUST
Holding
Flaps Up
30000
35000
ad
ed
or
pr
in
te
d
PRESSURE ALTITUDE (FT)
10000
15000
20000
25000
88.3
92.8
252
253
2750
2800
86.5
91.0
244
245
2570
2610
84.7
89.1
95.0
236
238
239
2400
2420
2490
82.8
87.1
92.1
228
229
231
2230
2250
2270
80.8
85.0
89.7
97.7
220
221
222
224
2070
2070
2080
2230
78.5
82.8
87.4
93.7
211
212
213
214
1910
1910
1910
1970
76.3
80.5
84.9
90.0
202
203
204
205
1750
1740
1730
1760
73.8
77.8
82.3
87.0
192
193
194
195
1600
1580
1570
1570
71.0
75.0
79.4
84.0
184
184
184
185
1440
1430
1400
1400
67.8
72.0
76.2
80.7
177
177
177
177
1300
1270
1250
1240
if
do
w
nl
o
5000
84.1
251
2730
82.4
243
2570
80.5
236
2400
78.6
227
2240
76.7
219
2090
74.6
210
1930
72.3
201
1770
69.7
191
1620
66.9
184
1470
64.0
177
1330
d
1500
81.1
250
2740
79.5
242
2580
77.8
235
2420
76.0
227
2260
74.0
219
2100
71.7
210
1950
69.4
200
1800
67.0
191
1650
64.3
184
1500
61.1
177
1350
on
tro
lle
WEIGHT
(1000 KG)
%N1
85
KIAS
FF/ENG
%N1
80
KIAS
FF/ENG
%N1
75
KIAS
FF/ENG
%N1
70
KIAS
FF/ENG
%N1
65
KIAS
FF/ENG
%N1
60
KIAS
FF/ENG
%N1
55
KIAS
FF/ENG
%N1
50
KIAS
FF/ENG
%N1
45
KIAS
FF/ENG
%N1
40
KIAS
FF/ENG
94.9
196
1680
89.6
186
1450
85.4
177
1260
94.1
177
1360
U
nc
This table includes 5% additional fuel for holding in a racetrack pattern.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.22.11
Performance Inflight - QRH
Engine Inoperative
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
ADVISORY INFORMATION
Gear Down Landing Rate of Climb Available
Flaps 15
RATE OF CLIMB (FT/MIN)
PRESSURE ALTITUDE (FT)
2000
4000
0
-160
-130
-110
-80
-50
-20
0
30
60
90
100
110
120
120
130
140
150
-230
-210
-180
-160
-130
-110
-80
-50
-20
0
30
50
60
60
70
80
-290
-260
-240
-220
-190
-160
-140
-110
-80
-20
-10
-10
0
0
6000
8000
or
pr
in
te
d
-2000
-90
-70
-40
-10
10
40
70
100
120
120
120
120
130
140
150
160
170
do
w
nl
o
52
50
48
46
44
42
40
38
36
34
32
30
20
10
0
-20
-40
-350
-320
-300
-280
-250
-220
-200
-90
-80
-80
-80
-80
-410
-390
-360
-340
-310
-180
-160
-160
-160
-160
6000
8000
-670
-640
-620
-600
-580
-550
-530
-420
-430
-430
-440
-450
-730
-710
-690
-670
-650
-530
-510
-510
-530
-550
ad
ed
TAT (°C)
Rate of climb capability shown is valid for 60000 kg, gear down at VREF15+5.
Decrease rate of climb 120 ft/min per 5000 kg greater than 60000 kg.
Increase rate of climb 160 ft/min per 5000 kg less than 60000 kg.
-2000
-390
-360
-340
-310
-290
-260
-240
-210
-190
-190
-190
-190
-180
-180
-180
-180
-180
0
-460
-430
-410
-380
-360
-330
-310
-280
-260
-230
-210
-210
-210
-200
-200
-200
-210
U
nc
on
tro
lle
52
50
48
46
44
42
40
38
36
34
32
30
20
10
0
-20
-40
RATE OF CLIMB (FT/MIN)
PRESSURE ALTITUDE (FT)
2000
4000
d
TAT (°C)
if
Flaps 30
-540
-520
-490
-470
-440
-420
-400
-370
-340
-320
-290
-280
-280
-270
-280
-290
-600
-580
-550
-530
-510
-480
-460
-440
-410
-350
-350
-350
-360
-370
Rate of climb capability shown is valid for 60000 kg, gear down at VREF30+5.
Decrease rate of climb 130 ft/min per 5000 kg greater than 60000 kg.
Increase rate of climb 160 ft/min per 5000 kg less than 60000 kg.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.22.12
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Gear Down
Section 23
GearHighlight
file
Down
GEAR DOWN
Gear Down
Gear Down
Long Range Cruise Altitude Capability
Max Cruise Thrust, 100 ft/min residual rate of climb
ISA + 20°C
9300
12600
15700
18600
21800
25300
28100
30700
33000
35400
or
pr
in
te
d
PRESSURE ALTITUDE (FT)
ISA + 15°C
12500
15500
18500
21500
24400
27100
29600
31900
34100
36500
U
nc
on
tro
lle
d
if
do
w
nl
o
85
80
75
70
65
60
55
50
45
40
ISA + 10°C & BELOW
15500
18400
21100
23700
26100
28600
30800
32900
35100
37500
ad
ed
WEIGHT (1000 KG)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.23.1
Performance Inflight - QRH
Gear Down
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
GEAR DOWN
Gear Down
Long Range Cruise Control
91.7
.557
240
1950
89.5
.543
233
1806
87.4
.525
225
1661
85.0
.504
216
1512
82.5
.482
206
1367
79.7
.458
196
1224
76.6
.434
185
1085
if
33
35
91.6
.560
231
1805
89.1
.544
224
1658
86.8
.525
216
1515
84.2
.502
206
1368
81.4
.477
196
1224
78.3
.452
185
1083
94.5
.578
229
1836
91.3
.562
222
1664
88.5
.545
215
1517
86.0
.523
206
1374
83.1
.498
196
1230
80.0
.471
185
1089
94.5
.580
220
1696
90.9
.562
213
1523
87.8
.544
205
1377
85.0
.520
196
1235
81.8
.491
185
1092
94.1
.581
211
1555
90.2
.561
203
1381
86.8
.541
195
1237
83.6
.513
185
1094
93.5
.580
201
1411
89.1
.559
193
1239
85.5
.535
185
1096
92.5
.578
191
1265
87.7
.554
183
1097
U
nc
31
or
pr
in
te
d
91.7
.554
248
2101
89.8
.541
242
1960
87.9
.524
234
1812
85.6
.504
225
1661
83.3
.484
216
1515
80.7
.463
206
1371
78.0
.441
196
1231
74.9
.417
185
1098
PRESSURE ALTITUDE (1000 FT)
25
27
29
ad
ed
23
do
w
nl
o
21
on
tro
lle
10
85.9
.482
267
2421
84.2
.468
259
2271
82.5
.454
251
2123
80.6
.440
243
1977
78.6
.425
235
1835
76.5
.409
226
1696
74.4
.393
217
1559
71.9
.376
207
1424
69.1
.358
197
1294
66.2
.340
187
1170
d
WEIGHT
(1000 KG)
%N1
85
MACH
KIAS
FF/ENG
%N1
80
MACH
KIAS
FF/ENG
%N1
75
MACH
KIAS
FF/ENG
%N1
70
MACH
KIAS
FF/ENG
%N1
65
MACH
KIAS
FF/ENG
%N1
60
MACH
KIAS
FF/ENG
%N1
55
MACH
KIAS
FF/ENG
%N1
50
MACH
KIAS
FF/ENG
%N1
45
MACH
KIAS
FF/ENG
%N1
40
MACH
KIAS
FF/ENG
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.23.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Gear Down
Category C/N Brakes
737 Flight Crew Operations Manual
GEAR DOWN
Long Range Cruise Enroute Fuel and Time
Ground to Air Miles Conversion
GROUND
DISTANCE
(NM)
200
400
600
800
1000
1200
1400
1600
1800
AIR DISTANCE (NM)
TAILWIND COMPONENT (KTS)
20
40
60
80
100
188
178
168
160
153
377
357
338
321
307
566
535
507
483
461
754
713
676
643
614
943
891
844
803
766
1131
1069
1013
962
918
1320
1247
1181
1122
1070
1508
1424
1348
1280
1221
1695
1600
1514
1438
1371
Reference Fuel and Time Required at Check Point
or
pr
in
te
d
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
100
80
60
40
20
324
290
260
236
217
654
583
523
474
435
989
880
787
713
653
1329
1181
1054
953
871
1674
1484
1322
1194
1090
2024
1791
1593
1436
1310
2381
2103
1865
1680
1530
2743
2417
2140
1924
1751
3113
2737
2418
2171
1972
PRESSURE ALTITUDE (1000 FT)
20
24
28
FUEL
TIME
FUEL
TIME
FUEL
TIME
FUEL
TIME
FUEL
TIME
(1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN)
200
2.4
0:49
2.2
0:47
1.9
0:44
1.7
0:42
1.6
0:41
400
4.9
1:36
4.5
1:31
4.0
1:25
3.7
1:20
3.5
1:17
600
7.4
2:25
6.8
2:17
6.1
2:06
5.7
1:59
5.4
1:54
800
9.8
3:14
9.1
3:03
8.1
2:48
7.6
2:38
7.2
2:31
1000
12.1
4:04
11.3
3:50
10.1
3:30
9.5
3:18
9.0
3:08
1200
14.4
4:56
13.5
4:39
12.1
4:14
11.3
3:58
10.7
3:46
1400
16.7
5:49
15.6
5:28
14.0
4:58
13.1
4:40
12.4
4:24
1600
18.9
6:43
17.7
6:18
15.9
5:44
14.9
5:22
14.1
5:03
1800
21.1
7:38
19.7
7:10
17.7
6:30
16.6
6:05
15.7
5:43
14
ad
ed
10
do
w
nl
o
AIR
DIST
(NM)
if
Fuel Required Adjustments (1000 KG)
U
nc
on
tro
lle
d
REFERENCE FUEL REQUIRED
(1000 KG)
2
4
6
8
10
12
14
16
18
20
22
40
-0.3
-0.7
-1.0
-1.3
-1.7
-2.0
-2.4
-2.7
-3.0
-3.4
-3.7
WEIGHT AT CHECK POINT (1000 KG)
50
60
70
-0.2
0.0
0.3
-0.3
0.0
0.6
-0.5
0.0
0.9
-0.7
0.0
1.2
-0.8
0.0
1.4
-1.0
0.0
1.6
-1.2
0.0
1.8
-1.3
0.0
2.0
-1.5
0.0
2.2
-1.7
0.0
2.4
-1.8
0.0
2.5
80
0.7
1.3
2.0
2.6
3.2
3.7
4.2
4.6
5.0
5.3
5.6
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.23.3
Performance Inflight - QRH
Gear Down
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
GEAR DOWN
Descent
VREF40 + 70 KIAS
FUEL (KG)
DISTANCE (NM)
21
20
19
19
18
17
17
16
15
14
13
13
12
11
8
6
4
280
270
270
260
260
250
250
240
230
230
220
210
200
190
170
140
110
91
86
81
77
72
68
64
60
56
52
48
44
40
36
26
16
9
U
nc
on
tro
lle
d
if
do
w
nl
o
Allowances for a straight-in approach are included.
or
pr
in
te
d
TIME (MIN)
ad
ed
PRESSURE ALTITUDE
(FT)
41000
39000
37000
35000
33000
31000
29000
27000
25000
23000
21000
19000
17000
15000
10000
5000
1500
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.23.4
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Gear Down
Category C/N Brakes
737 Flight Crew Operations Manual
GEAR DOWN
Holding
Flaps Up
30000
35000
ad
ed
or
pr
in
te
d
PRESSURE ALTITUDE (FT)
10000
15000
20000
25000
82.7
86.9
91.9
229
229
229
2220
2230
2250
81.0
85.3
89.9
224
224
224
2090
2090
2100
79.2
83.6
88.1
218
218
218
1960
1960
1960
77.5
81.8
86.2
91.7
213
213
213
213
1840
1830
1830
1860
75.8
80.0
84.4
89.1
209
209
209
209
1720
1710
1700
1720
73.9
77.9
82.3
86.9
203
203
203
203
1600
1590
1580
1580
71.8
75.8
80.2
84.7
197
197
197
197
1490
1470
1450
1450
69.4
73.6
77.8
82.3
191
191
191
191
1370
1350
1330
1320
67.0
71.2
75.3
79.8
184
184
184
184
1260
1240
1210
1200
64.5
68.5
72.8
77.1
177
177
177
177
1150
1130
1100
1080
if
do
w
nl
o
5000
78.4
229
2220
76.9
224
2100
75.3
218
1970
73.5
213
1850
71.7
209
1740
69.7
203
1620
67.6
197
1510
65.5
191
1400
63.1
184
1290
60.4
177
1170
d
1500
75.7
229
2240
74.1
224
2110
72.3
218
1990
70.6
213
1870
68.8
209
1760
66.9
203
1650
65.0
197
1530
62.7
191
1420
60.2
184
1310
57.7
177
1200
on
tro
lle
WEIGHT
(1000 KG)
%N1
85
KIAS
FF/ENG
%N1
80
KIAS
FF/ENG
%N1
75
KIAS
FF/ENG
%N1
70
KIAS
FF/ENG
%N1
65
KIAS
FF/ENG
%N1
60
KIAS
FF/ENG
%N1
55
KIAS
FF/ENG
%N1
50
KIAS
FF/ENG
%N1
45
KIAS
FF/ENG
%N1
40
KIAS
FF/ENG
94.1
203
1660
90.2
197
1490
87.0
191
1350
84.4
184
1220
81.5
177
1090
91.3
184
1260
86.6
177
1110
U
nc
This table includes 5% additional fuel for holding in a racetrack pattern.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.23.5
Performance Inflight - QRH
Gear Down
do
w
nl
o
ad
ed
or
pr
in
te
d
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
U
nc
on
tro
lle
d
if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.23.6
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Gear Down, Engine Inop
GearHighlight
file
Down, Engine Inop
Section 24
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Driftdown Speed/Level Off Altitude
or
pr
in
te
d
Gear Down, Engine Inop
Gear Down, Engine Inoperative
100 ft/min residual rate of climb
OPTIMUM
DRIFTDOWN
SPEED (KIAS)
218
213
208
202
196
190
183
176
Includes APU fuel burn.
LEVEL OFF ALTITUDE (FT)
ISA + 10°C
ISA + 15°C
ISA + 20°C
& BELOW
1500
4700
2200
8000
5900
3400
11100
9300
7100
14000
12900
10900
16900
16000
14800
19800
18700
17600
22800
21700
20600
ad
ed
WEIGHT (1000 KG)
START
LEVEL OFF
DRIFTDOWN
75
70
70
66
65
61
60
57
55
52
50
47
45
43
40
38
do
w
nl
o
Long Range Cruise Altitude Capability
100 ft/min residual rate of climb
d
PRESSURE ALTITUDE (FT)
ISA + 15°C
ISA + 20°C
3200
8200
13000
16900
20500
5300
10400
15700
19300
U
nc
on
tro
lle
65
60
55
50
45
40
ISA + 10°C & BELOW
1600
6300
10600
14400
18000
21700
if
WEIGHT (1000 KG)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.24.1
Performance Inflight - QRH
Gear Down, Engine Inop
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Control
91.0
.374
210
2906
88.2
.359
202
2630
85.4
.344
193
2374
82.5
.329
184
2133
PRESSURE ALTITUDE (1000 FT)
11
13
15
17
92.8
.387
209
2913
89.9
.371
201
2626
86.9
.355
192
2356
83.9
.339
183
2107
91.7
.384
200
2633
88.6
.367
191
2351
85.4
.349
182
2088
94.2
.398
199
2657
90.4
.380
190
2352
87.0
.361
181
2076
19
21
23
or
pr
in
te
d
9
ad
ed
7
91.9
.375
219
3191
89.3
.362
211
2909
86.7
.348
203
2647
84.0
.334
195
2400
81.1
.320
186
2166
92.7
.393
189
2359
88.8
.374
180
2069
96.6
.408
189
2417
90.8
.387
179
2065
94.1
.402
179
2101
98.4
.418
178
2201
U
nc
on
tro
lle
d
if
5
90.2
.364
220
3192
87.8
.351
212
2924
85.3
.338
204
2672
82.7
.325
196
2432
79.8
.311
188
2206
do
w
nl
o
WEIGHT
(1000 KG)
%N1
MACH
60
KIAS
FF/ENG
%N1
MACH
55
KIAS
FF/ENG
%N1
MACH
50
KIAS
FF/ENG
%N1
MACH
45
KIAS
FF/ENG
%N1
MACH
40
KIAS
FF/ENG
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.24.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Gear Down, Engine Inop
Category C/N Brakes
737 Flight Crew Operations Manual
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Diversion Fuel and Time
Ground to Air Miles Conversion
AIR DISTANCE (NM)
TAILWIND COMPONENT (KTS)
20
40
60
80
100
93
88
83
78
75
187
175
165
156
148
280
262
246
232
220
373
349
328
309
293
466
436
409
385
365
559
523
490
462
438
652
610
572
538
510
745
696
652
614
581
838
782
733
690
653
931
868
813
765
724
or
pr
in
te
d
GROUND
DISTANCE
(NM)
100
200
300
400
500
600
700
800
900
1000
ad
ed
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
100
80
60
40
20
172
151
134
120
109
352
308
270
242
219
533
465
408
364
330
716
623
545
486
440
900
783
684
609
551
1086
943
823
733
661
1273
1105
964
856
772
1462
1267
1103
980
883
1653
1431
1245
1104
994
1845
1595
1386
1228
1105
Reference Fuel and Time Required at Check Point
PRESSURE ALTITUDE (1000 FT)
10
14
FUEL
TIME
FUEL
TIME
(1000 KG)
(HR:MIN)
(1000 KG)
(HR:MIN)
1.1
0:26
1.0
0:26
2.4
0:50
2.3
0:48
3.7
1:15
3.6
1:11
4.9
1:39
4.8
1:35
6.1
2:04
6.0
1:58
7.3
2:29
7.1
2:22
8.5
2:55
8.3
2:46
9.7
3:20
9.4
3:10
10.9
3:46
10.5
3:35
12.0
4:12
11.6
3:59
do
w
nl
o
TIME
(HR:MIN)
0:27
0:53
1:18
1:44
2:10
2:37
3:03
3:30
3:58
4:25
if
FUEL
(1000 KG)
1.3
2.6
3.9
5.2
6.5
7.8
9.1
10.3
11.6
12.8
on
tro
lle
100
200
300
400
500
600
700
800
900
1000
6
d
AIR DIST
(NM)
Fuel Required Adjustments (1000 KG)
U
nc
REFERENCE FUEL REQUIRED
(1000 KG)
1
2
3
4
5
6
7
8
9
10
11
12
13
14
40
-0.2
-0.3
-0.5
-0.6
-0.8
-1.0
-1.1
-1.3
-1.5
-1.6
-1.8
-1.9
-2.1
-2.3
WEIGHT AT CHECK POINT (1000 KG)
50
60
70
-0.1
0.0
0.1
-0.2
0.0
0.3
-0.3
0.0
0.5
-0.3
0.0
0.7
-0.4
0.0
0.9
-0.5
0.0
1.0
-0.6
0.0
1.2
-0.7
0.0
1.4
-0.7
0.0
1.6
-0.8
0.0
1.8
-0.9
0.0
1.9
-1.0
0.0
2.1
-1.1
0.0
2.3
-1.1
0.0
2.5
80
0.3
0.6
1.0
1.3
1.7
2.0
2.4
2.7
3.1
3.5
3.8
4.2
4.5
4.9
Includes APU fuel burn.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
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PI-QRH.24.3
Performance Inflight - QRH
Gear Down, Engine Inop
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Holding
Flaps Up
15000
90.3
209
3360
88.1
203
3090
85.7
197
2840
83.2
191
2600
80.5
184
2370
77.7
177
2140
92.6
191
2650
89.5
184
2380
86.4
177
2130
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PRESSURE ALTITUDE (FT)
5000
10000
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1500
89.2
213
3580
87.3
209
3340
85.1
203
3090
82.8
197
2850
80.2
191
2610
77.7
184
2390
75.0
177
2170
92.7
203
3130
90.2
197
2860
87.6
191
2610
84.9
184
2360
82.0
177
2120
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WEIGHT
(1000 KG)
%N1
70
KIAS
FF/ENG
%N1
65
KIAS
FF/ENG
%N1
60
KIAS
FF/ENG
%N1
55
KIAS
FF/ENG
%N1
50
KIAS
FF/ENG
%N1
45
KIAS
FF/ENG
%N1
40
KIAS
FF/ENG
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This table includes 5% additional fuel for holding in a racetrack pattern.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.24.4
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Text
Section 25
TextHighlight
File
Introduction
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This chapter contains information to supplement performance data from
the Flight Management Computer (FMC). In addition, sufficient inflight
data is provided to complete a flight with the FMC inoperative. In the event
of conflict between data presented in this chapter and that contained in the
approved Airplane Flight Manual, the Flight Manual shall always take
precedence.
General
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Flight with Unreliable Airspeed / Turbulent Air Penetration
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Pitch attitude and average %N1 information is provided for use in all
phases of flight in the event of unreliable airspeed/Mach indications
resulting from blocking or freezing of the pitot system. Loss of radome or
turbulent air may also cause unreliable airspeed/Mach indications. The
cruise table in this section may also be used for turbulent air penetration.
Pitch attitude is shown in bold type for emphasis since altitude and/or
vertical speed indications may also be unreliable.
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Max Climb %N1
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This table shows Max Climb %N1 for a 280/.78 climb speed schedule,
normal engine bleed for packs on or off and anti-ice off. Enter the table
with airport pressure altitude and TAT and read %N1. %N1 adjustments are
shown for anti-ice operation.
Go-around %N1
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To find Max Go-around %N1 based on normal engine bleed for packs on
(AUTO) and anti-ice on or off, enter the Go-around %N1 table with airport
pressure altitude and reported OAT or TAT and read %N1. For packs OFF
or HIGH operation, apply the %N1 adjustment shown below the table.
VREF
This table contains flaps 40, 30 and 15 reference speeds for a given weight.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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Performance Inflight - QRH
Text
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Advisory Information
Runway Surface Condition Correlation
Normal Configuration Landing Distance
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When landing on slippery runways or runways contaminated with ice,
snow, slush, or standing water, the reported braking action must be
considered. A table is provided that correlates runway condition code to
runway surface condition description and reported braking action that can
then be used to determine the appropriate Normal Configuration Landing
Distance or Non-Normal Configuration Landing Distance.
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Tables are provided as advisory information for normal configuration
landing distances on dry runways and runways with good,
good-to-medium, medium, medium-to-poor, and poor reported braking
action. Landing distances (reference distances plus adjustments) are 115%
of the actual landing distance. The Normal Configuration Landing
Distance tables should be used enroute to make a landing distance
assessment for time of arrival.
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The reference landing distance is the distance from threshold to complete
stop. It includes an air distance allowance of 1500 ft from threshold to
touchdown. The reference distance is based on a reference landing weight
and speed at sea level, standard day, zero wind, zero slope, two-engine
detent No. 2 reverse thrust, and auto speedbrakes.
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To use these tables, determine the reference landing distance for the
selected braking configuration and reported braking action. Adjust this
reference distance for landing weight, altitude, wind, slope, temperature,
approach speed, and the number of operative thrust reversers. Each
correction is applied independently to the reference landing distance. A
correction for use of manual speedbrakes is provided in the table notes.
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Use of the autobrake system commands the airplane to a constant
deceleration rate. In some conditions, such as a runway with "poor"
reported braking action, the airplane may not be able to achieve these
deceleration rates. In these cases, runway slope and inoperative reversers
influence the stopping distance. Since it cannot be determined quickly
when this becomes a factor, it is appropriate to add the effects of slope and
inoperative reversers when using the autobrake system.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Text
Category C/N Brakes
737 Flight Crew Operations Manual
Non-normal Configuration Landing Distance
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Advisory information is provided to support non-normal configurations
that affect landing. Landing distances and adjustments are provided for dry
runways and runways with good, good-to-medium, medium,
medium-to-poor, and poor reported braking action. Landing distances
(reference distances plus adjustments) are representative of the actual
landing distance, and are not factored. The Non-Normal Configuration
Landing Distance tables should be used enroute to make a landing distance
assessment for time of arrival.
The reference landing distance is the distance from threshold to complete
stop. It includes an air distance allowance of 1500 ft from threshold to
touchdown. The reference distance is based on a reference landing weight
and speed at sea level, standard day, zero wind, zero slope, and maximum
available reverse thrust.
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Tables for Non-Normal Configuration Landing Distance in this section are
similar in format and used in the same manner as tables for the Normal
Configuration Landing Distance previously described.
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Recommended Brake Cooling Schedule
Advisory information is provided to assist in avoiding the problems
associated with hot brakes. For normal operation, most landings are at
weights below the AFM quick turnaround limit weight.
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Use of the recommended cooling schedule will help avoid brake overheat
and fuse plug problems that could result from repeated landings at short
time intervals or a rejected takeoff.
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Enter the Recommended Brake Cooling Schedule table with the airplane
weight and brakes on speed, adjusted for wind at the appropriate
temperature and altitude condition. Instructions for applying wind
adjustments are included below the table. Linear interpolation may be used
to obtain intermediate values. The resulting number is the reference brake
energy per brake in millions of foot-pounds, and represents the amount of
energy absorbed by each brake during a rejected takeoff. Notes providing
adjustments for wind are included below the table.
To determine the energy per brake absorbed during landing, enter the
appropriate Adjusted Brake Energy Per Brake table (No Reverse Thrust or
2 Engine Reverse) with the reference brake energy per brake and the type
of braking used during landing (Max Manual, Max Auto, or Autobrake).
The resulting number is the adjusted brake energy per brake and represents
the energy absorbed in each brake during the landing.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
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Performance Inflight - QRH
Text
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
The recommended cooling time is found in the appropriate (steel or carbon
brakes) final table by entering with the adjusted brake energy per brake.
Times are provided for ground cooling and inflight gear down cooling.
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Brake Temperature Monitor System (BTMS) indications are also shown. If
brake cooling is determined from the BTMS, use the hottest brake
indication 10 to 15 minutes after the airplane has come to a complete stop,
or inflight with gear retracted to determine recommended cooling
schedule.
Engine Inoperative
Initial Max Continuous %N1
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Max Continuous %N1
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The Initial Max Continuous %N1 setting for use following an engine
failure is shown. The table is based on the typical all engine cruise speed
of.79M to provide a target %N1 setting at the start of driftdown. Once
driftdown is established, the Max Continuous %N1 table should be used to
determine %N1 for the given conditions.
Power setting is based on one engine operating with one A/C pack
operating and all anti-ice bleeds off. Enter the table with pressure altitude,
TAT, and IAS or Mach to read %N1.
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It is desirable to maintain engine thrust level within the limits of the Max
Cruise thrust rating. However, where thrust level in excess of Max Cruise
rating is required, such as for meeting terrain clearance, ATC altitude
assignments, or to attain maximum range capability, it is permissible to use
the thrust needed up to the Max Continuous thrust rating. The Max
Continuous thrust rating is intended primarily for emergency use at the
discretion of the pilot and is the maximum thrust that may be used
continuously.
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Driftdown Speed/Level Off Altitude
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The table shows optimum driftdown speed as a function of cruise weight
at start of driftdown. Also shown are the approximate weight and pressure
altitude at which the airplane will level off considering 100 ft/min residual
rate of climb.
The level off altitude is dependent on air temperature (ISA deviation).
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
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D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B24
Performance Inflight - QRH
FAA
Text
Category C/N Brakes
737 Flight Crew Operations Manual
Driftdown/LRC Range Capability
This table shows the range capability from the start of driftdown.
Driftdown is continued to level off altitude. As weight decreases due to
fuel burn, the airplane is accelerated to Long Range Cruise speed. Cruise
is continued at level off altitude and Long Range Cruise speed.
Long Range Cruise Altitude Capability
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To determine fuel required, enter the Ground to Air Miles Conversion table
with the desired ground distance and adjust for anticipated winds to obtain
air distance to destination. Then enter the Driftdown/Cruise Fuel and Time
table with air distance and weight at start of driftdown to determine fuel
and time required. If altitudes other than the level off altitude is used, fuel
and time required may be obtained by using the Engine Inoperative Long
Range Cruise Enroute Fuel and Time table.
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Long Range Cruise Control
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The table shows the maximum altitude that can be maintained at a given
weight and air temperature (ISA deviation), based on Long Range Cruise
speed, Max Continuous thrust, and 100 ft/min residual rate of climb.
The table provides target %N1, engine inoperative Long Range Cruise
Mach number, IAS and fuel flow for the airplane weight and pressure
altitude. The fuel flow values in this table reflect single engine fuel burn.
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APU Operation During Flight
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For APU operation during flight, increase fuel flow according to the
following table. These increments include the APU fuel flow and the effect
of increased drag from the APU door.
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PRESSURE ALTITUDE (1000 FT)
39
35
31
25
20
15
10
5
APU FUEL FLOW (KG/HR)
45
45
50
60
65
75
85
95
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.25.5
Performance Inflight - QRH
Text
737-800WSFP1/CFM56-7B24
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Long Range Cruise Diversion Fuel and Time
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Tables are provided for crews to determine the fuel and time required to
proceed to an alternate airfield with one engine inoperative. The data is
based on single engine Long Range Cruise speed and .78/280/250 descent.
Enter with Air Distance as determined from the Ground to Air Miles
Conversion table and read Fuel and Time required at the cruise pressure
altitude. Adjust the fuel obtained for deviation from the reference weight
at checkpoint as required by entering the off reference fuel adjustments
table with the fuel required for the reference weight and the actual weight
at checkpoint. Read fuel required and time for the actual weight.
Holding
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Target %N1, indicated airspeed and fuel flow per engine information is
tabulated for holding with flaps up based on the FMC optimum holding
speed schedule. This is the higher of the maximum endurance speed and
the maneuvering speed. Small variations in airspeed will not appreciably
affect the overall endurance time. Enter the table with weight and pressure
altitude to read %N1, IAS and fuel flow per engine.
Gear Down Landing Rate of Climb Available
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Rate of climb data is provided as guidance information in the event an
engine inoperative landing (manual or autoland) is planned. The tables
show gear down rate of climb available for Flaps 15 and Flaps 30. Enter
the table with TAT and pressure altitude to read rate of climb available.
Apply adjustments shown to correct for weight.
Gear Down
This section contains performance for airplane operation with the landing
gear extended. The data is based on engine bleeds for normal air
conditioning.
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Note: The Flight Management Computer System (FMCS) does not
contain special provisions for operation with landing gear extended.
As a result, the FMCS may generate inappropriate enroute speed
schedules, display non-conservative predictions of fuel burn,
estimated time of arrival (ETA), maximum altitude, and compute
overly shallow descent path. An accurate estimated time of arrival
(ETA) is available if current speed or Mach is entered into the
VNAV cruise page.
Tables for gear down performance in this section are identical in format
and used in the same manner as tables for the gear up configuration
previously described.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.25.6
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1
Section
737-800WSFP1
CFM56-7B26
CFM56-7B26
C M KGCFAA
M KG
CATC/N
FAA CATC/N
TALPA TALPA
(FMC Model
(FMC737-800W.1)
Model 737-800W.1)
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Table of Contents
Section 30
737-800WSFP1 CFM56-7B26 C M KG FAA CATC/N TALPA (FMC
Model 737-800W.1)
Pkg Model Identification . . . . . . . . . . . . . . . . . . . PI-QRH.ModID.30.1
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General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.30.1
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Flight With Unreliable Airspeed/
Turbulent Air Penetration . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.30.1
CLIMB (280/.76) . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.30.1
CRUISE (.76/280) . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.30.1
DESCENT (.76/280) . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.30.2
HOLDING (VREF40 + 70). . . . . . . . . . . . . . . . . . . PI-QRH.30.2
TERMINAL AREA (5000 FT) . . . . . . . . . . . . . . . . PI-QRH.30.3
Airport Altitude = -2000 FT . . . . . . . . . . . . . . . . PI-QRH.30.3
Airport Altitude = -1000 FT . . . . . . . . . . . . . . . . PI-QRH.30.4
Airport Altitude = SEA LEVEL . . . . . . . . . . . . . PI-QRH.30.5
Airport Altitude = 1000 FT . . . . . . . . . . . . . . . . PI-QRH.30.6
Airport Altitude = 2000 FT . . . . . . . . . . . . . . . . PI-QRH.30.7
Airport Altitude = 3000 FT . . . . . . . . . . . . . . . . PI-QRH.30.8
Airport Altitude = 4000 FT . . . . . . . . . . . . . . . . PI-QRH.30.9
Airport Altitude = 5000 FT . . . . . . . . . . . . . . . PI-QRH.30.10
Airport Altitude = 6000 FT . . . . . . . . . . . . . . . .PI-QRH.30.11
Airport Altitude = 7000 FT . . . . . . . . . . . . . . . PI-QRH.30.12
Airport Altitude = 8000 FT . . . . . . . . . . . . . . . PI-QRH.30.13
Airport Altitude = 9000 FT . . . . . . . . . . . . . . . PI-QRH.30.14
Airport Altitude = 10000 FT . . . . . . . . . . . . . . PI-QRH.30.15
Airport Altitude = 11000 FT. . . . . . . . . . . . . . . PI-QRH.30.16
Airport Altitude = 12000 FT . . . . . . . . . . . . . . PI-QRH.30.17
Airport Altitude = 13000 FT . . . . . . . . . . . . . . PI-QRH.30.18
Airport Altitude = 14000 FT . . . . . . . . . . . . . . PI-QRH.30.19
Airport Altitude = 14500 FT . . . . . . . . . . . . . . PI-QRH.30.20
FINAL APPROACH (1500 FT) . . . . . . . . . . . . . . PI-QRH.30.21
Airport Altitude = -2000 FT . . . . . . . . . . . . . . . PI-QRH.30.21
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
4
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PI-QRH.TOC.30.1
Performance Inflight - QRH Table of Contents
737 Flight Crew Operations Manual
PI-QRH.30.21
PI-QRH.30.22
PI-QRH.30.22
PI-QRH.30.23
PI-QRH.30.23
PI-QRH.30.24
PI-QRH.30.24
PI-QRH.30.25
PI-QRH.30.25
PI-QRH.30.26
PI-QRH.30.26
PI-QRH.30.27
PI-QRH.30.27
PI-QRH.30.28
PI-QRH.30.28
PI-QRH.30.29
PI-QRH.30.29
PI-QRH.30.30
PI-QRH.30.31
PI-QRH.30.32
PI-QRH.30.33
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Airport Altitude = -1000 FT . . . . . . . . . . . . . . .
Airport Altitude = SEA LEVEL . . . . . . . . . . . .
Airport Altitude = 1000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 2000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 3000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 4000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 5000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 6000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 7000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 8000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 9000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 10000 FT. . . . . . . . . . . . . . .
Airport Altitude = 11000 FT. . . . . . . . . . . . . . .
Airport Altitude = 12000 FT. . . . . . . . . . . . . . .
Airport Altitude = 13000 FT. . . . . . . . . . . . . . .
Airport Altitude = 14000 FT. . . . . . . . . . . . . . .
Airport Altitude = 14500 FT. . . . . . . . . . . . . . .
GO-AROUND . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Max Climb %N1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Go-around %N1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
VREF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Advisory Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.31.1
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Runway Surface Condition Correlation . . . . . . . . . . . . PI-QRH.31.1
Normal Configuration Landing Distance . . . . . . . . . . . PI-QRH.31.2
Non-Normal Configuration Landing Distance . . . . . . . PI-QRH.31.8
Airspeed Unreliable (Flaps 15) . . . . . . . . . . . . . . . . PI-QRH.31.8
Airspeed Unreliable (Flaps 30) . . . . . . . . . . . . . . . . PI-QRH.31.9
Airspeed Unreliable (Flaps 40) . . . . . . . . . . . . . . . PI-QRH.31.10
All Flaps Up Landing. . . . . . . . . . . . . . . . . . . . . . . PI-QRH.31.11
ANTISKID INOPERATIVE (Flaps 15) . . . . . . . . PI-QRH.31.12
ANTISKID INOPERATIVE (Flaps 30) . . . . . . . . PI-QRH.31.13
ANTISKID INOPERATIVE (Flaps 40) . . . . . . . . PI-QRH.31.14
Jammed or Restricted Flight Controls (Flaps 15) . PI-QRH.31.15
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PI-QRH.TOC.30.2
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Performance Inflight - QRH Table of Contents
737 Flight Crew Operations Manual
PI-QRH.31.16
PI-QRH.31.17
PI-QRH.31.18
PI-QRH.31.19
PI-QRH.31.20
PI-QRH.31.21
PI-QRH.31.22
PI-QRH.31.23
PI-QRH.31.24
PI-QRH.31.25
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LEADING EDGE FLAPS TRANSIT (Flaps 15) .
LOSS OF SYSTEM A (Flaps 15) . . . . . . . . . . . . .
LOSS OF SYSTEM A (Flaps 30) . . . . . . . . . . . . .
LOSS OF SYSTEM A (Flaps 40) . . . . . . . . . . . . .
LOSS OF SYSTEM A AND SYSTEM B
(Flaps 15). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
LOSS OF SYSTEM B (Flaps 15) . . . . . . . . . . . . .
MANUAL REVERSION (Flaps 15). . . . . . . . . . .
One Engine Inoperative Landing (Flaps 15) . . . . .
One Engine Inoperative Landing (Flaps 30) . . . . .
Stabilizer Trim Inoperative (Flaps 15) . . . . . . . . .
Trailing Edge Flap Asymmetry (1 ≤ Flap
Lever <15) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flap Asymmetry (Flap Lever
15 or 25) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flap Asymmetry (Flap Lever 30) . .
Trailing Edge Flap Disagree (1 ≤ Indicated
Flaps <15) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flap Disagree (15 ≤ Indicated
Flaps <30) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flap Disagree (30 ≤ Indicated
Flaps <40) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flaps Up Landing . . . . . . . . . . . . . .
Recommended Brake Cooling Schedule . . . . . . . . . .
PI-QRH.31.26
PI-QRH.31.27
PI-QRH.31.28
PI-QRH.31.29
PI-QRH.31.30
PI-QRH.31.31
PI-QRH.31.32
PI-QRH.31.33
Engine Inoperative . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.32.1
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Initial Max Continuous %N1 . . . . . . . . . . . . . . . . . . . . PI-QRH.32.1
Max Continuous %N1 . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.32.2
Driftdown Speed/Level Off Altitude . . . . . . . . . . . . . . PI-QRH.32.6
Driftdown/LRC Cruise Range Capability . . . . . . . . . . PI-QRH.32.7
Long Range Cruise Altitude Capability . . . . . . . . . . . . PI-QRH.32.8
Long Range Cruise Control . . . . . . . . . . . . . . . . . . . . . PI-QRH.32.9
Long Range Cruise Diversion Fuel and Time . . . . . . PI-QRH.32.10
Holding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.32.11
Gear Down Landing Rate of Climb Available . . . . . . PI-QRH.32.12
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.TOC.30.3
Performance Inflight - QRH Table of Contents
737 Flight Crew Operations Manual
Gear Down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.33.1
PI-QRH.33.1
PI-QRH.33.2
PI-QRH.33.3
PI-QRH.33.4
PI-QRH.33.5
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Long Range Cruise Altitude Capability . . . . . . . . . . . .
Long Range Cruise Control . . . . . . . . . . . . . . . . . . . . .
Long Range Cruise Enroute Fuel and Time . . . . . . . . .
Descent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Holding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Gear Down, Engine Inoperative . . . . . . . . . . . . . . . . . . . .PI-QRH.34.1
ad
ed
Driftdown Speed/Level Off Altitude. . . . . . . . . . . . . . .
Long Range Cruise Altitude Capability . . . . . . . . . . . .
Long Range Cruise Control . . . . . . . . . . . . . . . . . . . . .
Long Range Cruise Diversion Fuel and Time. . . . . . . .
Holding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
PI-QRH.34.1
PI-QRH.34.1
PI-QRH.34.2
PI-QRH.34.3
PI-QRH.34.4
Text. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.35.1
PI-QRH.35.1
PI-QRH.35.1
PI-QRH.35.2
PI-QRH.35.4
PI-QRH.35.6
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Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Advisory Information . . . . . . . . . . . . . . . . . . . . . . . . . .
Engine Inoperative . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Gear Down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.TOC.30.4
D6-27370-8AS-NOK
September 30, 2022
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Pkg Model Identification
Section 30
Pkg Model Identification
File Model
Pkg
highlight
Identification
General
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The table below shows the airplanes that have been identified with the following
performance package. Note, some airplanes may be identified with more than one
performance package. This configuration table information reflects the Boeing
delivered configuration updated for service bulletin incorporations in
conformance with the policy stated in the introduction section of the FCOM. The
performance data is prepared for the owner/operator named on the title page. The
intent of this information is to assist flight crews and airlines in knowing which
performance package is applicable to a given airplane. The performance package
model identification information is based on Boeing's knowledge of the airline's
fleet at a point in time approximately three months prior to the page date. Notice
of Errata (NOE) will not be provided to airlines to identify airplanes that are
moved between performance packages within this manual or airplanes added to
the airline's fleet whose performance packages are already represented in this
manual. These types of changes will be updated in the next block revision.
Owners/operators are responsible for ensuring the operational documentation they
are using is complete and matches the current configuration of their airplanes, and
the accuracy and validity of all information furnished by the owner/operator or
any other party. Owners/operators receiving active revision service are
responsible to ensure that any modifications to the listed airplanes are properly
reflected in this manual.
d
Serial and tabulation number are supplied by Boeing.
Serial Number
Tabulation
Number
HS-DBR
43420
YR591
HS-DBS
43421
YR592
HS-DBP
39336
YS823
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Registry Number
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September 30, 2022
2
D6-27370-8AS-NOK
PI-QRH.ModID.30.1
Performance Inflight - QRH Pkg Model Identification
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737 Flight Crew Operations Manual
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if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.ModID.30.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
General
Section 30
General
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
file Highlight
General
40
2.0
82.9
1.0
81.2
1.0
80.7
1.0
77.2
1.0
73.6
1.0
69.8
or
pr
in
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CRUISE (.76/280)
Flaps Up, %N1 for Level Flight
PRESSURE
ALTITUDE (FT)
PITCH ATT
40000
%N1
PITCH ATT
35000
%N1
PITCH ATT
30000
%N1
PITCH ATT
25000
%N1
PITCH ATT
20000
%N1
PITCH ATT
15000
%N1
WEIGHT (1000 KG)
50
60
70
4.0
4.0
1100
600
4.0
3.5
4.0
1900
1500
1100
6.5
6.0
6.0
3300
2600
2100
9.5
8.5
8.0
4400
3600
3000
12.5
11.0
10.0
5300
4400
3700
ad
ed
40
4.0
1700
4.0
2500
7.0
4200
11.0
5600
14.5
6700
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CLIMB (280/.76)
Flaps Up, Set Max Climb Thrust
PRESSURE
ALTITUDE (FT)
PITCH ATT
40000
V/S (FT/MIN)
PITCH ATT
30000
V/S (FT/MIN)
PITCH ATT
20000
V/S (FT/MIN)
PITCH ATT
10000
V/S (FT/MIN)
SEA
PITCH ATT
V/S (FT/MIN)
LEVEL
WEIGHT (1000 KG)
50
60
70
2.5
3.5
85.4
88.9
2.0
2.5
3.0
82.6
84.4
86.8
1.5
2.0
2.5
81.5
82.7
84.2
1.5
2.0
2.5
77.9
79.0
80.5
1.5
2.0
2.5
74.2
75.3
76.6
1.5
2.0
3.0
70.6
71.6
72.9
80
4.0
800
6.0
1700
8.0
2500
9.5
3100
80
3.5
90.4
3.0
86.1
3.0
82.3
3.5
78.2
3.5
74.4
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.1
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
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HOLDING (VREF40 + 70)
Flaps Up, %N1 for Level Flight
PRESSURE ALTITUDE (FT)
PITCH ATT
%N1
KIAS
PITCH ATT
%N1
KIAS
PITCH ATT
%N1
KIAS
40
5.0
56
177
5.0
52
177
5.0
49
177
if
15000
on
tro
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d
10000
80
1.5
-2700
0.5
-2000
0.5
-1700
0.5
-1500
0.5
-1400
WEIGHT (1000 KG)
50
60
70
5.0
5.0
5.0
62
66
70
193
212
229
5.0
5.0
5.0
58
62
66
192
211
228
5.5
5.0
5.0
54
58
62
191
210
227
80
5.0
73
246
5.0
69
244
5.0
66
243
U
nc
5000
WEIGHT (1000 KG)
50
60
70
-0.5
0.5
1.0
-2400
-2300
-2500
-2.0
-1.0
-0.5
-2600
-2300
-2100
-2.0
-1.0
0.0
-2300
-2000
-1900
-2.0
-1.0
0.0
-2100
-1800
-1700
-2.5
-1.0
-0.5
-1900
-1700
-1500
or
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40
-1.5
-2700
-3.5
-3100
-3.5
-2800
-3.5
-2500
-3.5
-2300
ad
ed
DESCENT (.76/280)
Flaps Up, Set Idle Thrust
PRESSURE
ALTITUDE (FT)
PITCH ATT
40000
V/S (FT/MIN)
PITCH ATT
30000
V/S (FT/MIN)
PITCH ATT
20000
V/S (FT/MIN)
PITCH ATT
10000
V/S (FT/MIN)
SEA
PITCH ATT
V/S (FT/MIN)
LEVEL
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = -2000 FT
if
d
or
pr
in
te
d
80
6.0
63.6
223
6.0
65.8
203
6.5
66.7
183
5.5
68.0
183
6.0
69.0
173
6.5
70.6
163
6.0
74.1
173
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
52.2 56.3 60.0
191
203
213
5.0
5.5
6.0
54.3 58.5 62.3
171
183
193
5.5
6.0
6.5
54.4 58.9 63.1
151
163
173
4.5
5.0
5.5
55.6 60.2 64.4
151
163
173
5.0
5.5
5.5
56.3 61.1 65.3
141
153
163
6.0
6.0
6.5
57.6 62.5 66.8
131
143
153
5.5
5.5
6.0
61.2 66.1 70.2
141
153
163
ad
ed
40
4.5
47.5
177
5.0
49.6
157
5.5
49.3
137
4.5
50.4
137
5.0
50.9
127
6.0
52.1
117
5.0
55.5
127
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FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.3
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = -1000 FT
if
d
U
nc
on
tro
lle
80
6.5
64.4
223
6.0
66.5
203
6.5
67.5
183
5.5
68.8
183
6.0
69.8
173
6.5
71.5
163
6.0
74.9
173
or
pr
in
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d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
52.9 57.0 60.8
191
203
213
5.0
5.5
6.0
55.1 59.3 63.1
171
183
193
5.5
6.0
6.5
55.2 59.7 63.9
151
163
173
4.5
5.0
5.5
56.3 61.0 65.2
151
163
173
5.0
5.5
5.5
57.0 61.9 66.1
141
153
163
6.0
6.0
6.5
58.4 63.3 67.6
131
143
153
5.5
5.5
6.0
62.0 66.9 71.0
141
153
163
ad
ed
40
4.5
48.2
177
5.0
50.2
157
5.5
49.9
137
4.5
51.1
137
5.0
51.6
127
6.0
52.8
117
5.0
56.2
127
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FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.4
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = SEA LEVEL
if
d
or
pr
in
te
d
80
6.5
65.2
223
6.0
67.3
203
6.5
68.3
183
5.5
69.6
183
6.0
70.6
173
6.5
72.4
163
6.0
75.8
173
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
53.5 57.7 61.6
191
203
213
5.0
5.5
6.0
55.8 60.0 63.9
171
183
193
5.5
6.0
6.5
55.9 60.5 64.7
151
163
173
4.5
5.0
5.5
57.1 61.9 66.0
151
163
173
5.5
5.5
5.5
57.8 62.7 66.9
141
153
163
6.0
6.0
6.5
59.2 64.2 68.4
131
143
153
5.5
5.5
6.0
62.8 67.7 71.9
141
153
163
ad
ed
40
4.5
48.9
177
5.0
50.9
157
5.5
50.6
137
4.5
51.8
137
5.0
52.3
127
6.0
53.5
117
5.0
57.0
127
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FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.5
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 1000 FT
if
d
U
nc
on
tro
lle
80
6.5
66.0
223
6.0
68.0
203
6.5
69.1
183
5.5
70.4
183
6.0
71.5
173
6.5
73.2
163
6.0
76.6
173
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
54.3 58.4 62.4
191
203
213
5.0
5.5
6.0
56.5 60.8 64.7
171
183
193
5.5
6.0
6.5
56.6 61.3 65.5
151
163
173
4.5
5.0
5.5
57.9 62.7 66.8
151
163
173
5.5
5.5
5.5
58.6 63.5 67.7
141
153
163
6.0
6.0
6.5
60.0 65.0 69.2
131
143
153
5.5
5.5
6.0
63.6 68.5 72.8
141
153
163
ad
ed
40
4.5
49.7
177
5.0
51.6
157
5.5
51.4
137
4.5
52.6
137
5.0
53.0
127
6.0
54.3
117
5.0
57.7
127
do
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FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.6
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 2000 FT
if
d
or
pr
in
te
d
80
6.5
66.7
223
6.0
68.8
203
6.5
69.9
183
5.5
71.3
183
6.0
72.4
173
6.5
74.1
163
6.0
77.4
173
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
55.0 59.2 63.3
191
203
213
5.0
5.5
6.0
57.3 61.7 65.4
171
183
193
5.5
6.0
6.5
57.4 62.2 66.3
151
163
173
4.5
5.0
5.5
58.6 63.5 67.6
151
163
173
5.5
5.5
5.5
59.4 64.3 68.5
141
153
163
6.0
6.0
6.5
60.8 65.8 70.1
131
143
153
5.5
5.5
6.0
64.4 69.3 73.6
141
153
163
ad
ed
40
4.5
50.4
177
5.0
52.3
157
5.5
52.1
137
4.5
53.3
137
5.0
53.7
127
6.0
55.0
117
5.0
58.5
127
do
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nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.7
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 3000 FT
if
d
U
nc
on
tro
lle
80
6.5
67.4
223
6.0
69.6
203
6.5
70.7
183
5.5
72.1
183
6.0
73.3
173
6.5
74.9
163
6.0
78.2
173
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
55.8 60.0 64.1
191
203
213
5.0
5.5
6.0
58.0 62.5 66.2
171
183
193
5.5
6.0
6.5
58.2 63.0 67.1
151
163
173
4.5
5.0
5.5
59.5 64.3 68.4
151
163
173
5.5
5.5
5.5
60.2 65.2 69.4
141
153
163
6.0
6.0
6.5
61.6 66.5 71.0
131
143
153
5.5
5.5
6.0
65.2 70.2 74.5
141
153
163
ad
ed
40
4.5
51.0
177
5.0
53.1
157
5.5
52.9
137
4.5
54.0
137
5.0
54.5
127
6.0
55.8
117
5.0
59.3
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.8
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 4000 FT
if
d
or
pr
in
te
d
80
6.5
68.2
223
6.0
70.5
203
6.5
71.6
183
5.5
73.0
183
6.0
74.1
173
6.5
75.7
163
6.0
79.1
173
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
56.4 60.8 64.9
191
203
213
5.0
5.5
6.0
58.8 63.3 66.9
171
183
193
5.5
6.0
6.5
59.0 63.8 67.9
151
163
173
4.5
5.0
5.5
60.3 65.1 69.2
151
163
173
5.5
5.5
5.5
61.1 66.0 70.2
141
153
163
6.0
6.0
6.5
62.4 67.4 71.9
131
143
153
5.5
5.5
6.0
66.0 71.1 75.3
141
153
163
ad
ed
40
4.5
51.7
177
5.0
53.9
157
5.5
53.6
137
4.5
54.7
137
5.0
55.2
127
6.0
56.5
117
5.0
60.1
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.9
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 5000 FT
if
d
U
nc
on
tro
lle
80
6.5
69.0
224
6.0
71.4
204
6.5
72.5
184
5.5
73.8
184
6.0
74.9
174
6.5
76.5
164
6.0
80.0
174
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
57.2 61.6 65.6
191
203
213
5.0
5.5
6.0
59.6 64.1 67.7
171
183
193
5.5
6.0
6.5
59.8 64.6 68.7
151
163
173
4.5
5.0
5.5
61.1 65.9 70.0
151
163
173
5.5
5.5
5.5
61.9 66.7 71.1
141
153
163
6.0
6.0
6.5
63.3 68.2 72.7
131
143
153
5.5
5.5
6.0
66.8 71.9 76.1
141
153
163
ad
ed
40
4.5
52.4
177
5.0
54.6
157
5.5
54.3
137
4.5
55.5
137
5.0
56.0
127
6.0
57.3
117
5.0
61.0
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.10
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 6000 FT
if
d
or
pr
in
te
d
80
6.5
69.8
224
6.0
72.2
204
6.5
73.3
184
5.5
74.6
184
6.0
75.7
174
6.5
77.3
164
6.0
80.9
174
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
57.9 62.5 66.3
191
203
213
5.0
5.5
6.0
60.4 64.8 68.5
171
183
193
5.5
6.0
6.5
60.7 65.4 69.5
151
163
173
4.5
5.0
5.5
62.0 66.7 70.9
151
163
173
5.5
5.5
5.5
62.7 67.6 72.0
141
153
163
6.0
6.0
6.5
64.1 69.0 73.6
131
143
153
5.5
5.5
6.0
67.6 72.8 77.0
141
153
163
ad
ed
40
4.5
53.1
177
5.0
55.3
157
5.5
55.1
137
4.5
56.2
137
5.0
56.7
127
6.0
58.1
117
5.0
61.8
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.11
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 7000 FT
if
d
U
nc
on
tro
lle
80
6.5
70.6
224
6.0
73.1
204
6.5
74.1
184
5.5
75.4
184
6.0
76.5
174
6.5
78.2
164
6.0
81.8
174
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
58.7 63.3 67.1
191
203
213
5.0
5.5
6.0
61.3 65.6 69.4
171
183
193
5.5
6.0
6.5
61.5 66.2 70.4
151
163
173
4.5
5.0
5.5
62.8 67.5 71.8
151
163
173
5.5
5.5
5.5
63.5 68.4 72.8
141
153
163
6.0
6.0
6.5
64.9 69.9 74.4
131
143
153
5.5
5.5
6.0
68.5 73.7 77.8
141
153
163
ad
ed
40
4.5
53.8
177
5.0
56.1
157
5.5
55.8
137
4.5
57.0
137
5.0
57.6
127
6.0
58.9
117
5.0
62.6
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.12
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 8000 FT
if
d
or
pr
in
te
d
80
6.0
71.4
225
6.0
73.9
205
6.5
74.9
185
5.5
76.2
185
6.0
77.3
175
6.5
79.1
165
6.0
82.7
175
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
59.5 64.1 67.8
191
203
214
5.0
5.5
6.0
62.1 66.4 70.3
171
183
194
5.5
6.0
6.5
62.4 67.0 71.2
151
163
174
4.5
5.0
5.5
63.6 68.3 72.6
151
163
174
5.5
5.5
5.5
64.3 69.3 73.7
141
153
164
6.0
6.0
6.5
65.7 70.8 75.2
131
143
154
5.5
5.5
6.0
69.4 74.5 78.7
141
153
164
ad
ed
40
4.5
54.5
177
5.0
56.8
157
5.5
56.6
137
4.5
57.8
137
5.0
58.4
127
6.0
59.8
117
5.0
63.5
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.13
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 9000 FT
if
d
U
nc
on
tro
lle
80
6.0
72.2
225
6.0
74.7
205
6.5
75.7
185
5.5
77.1
185
5.5
78.2
175
6.5
80.0
165
6.0
83.6
175
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
60.4 64.9 68.6
191
204
214
5.0
5.5
6.0
62.9 67.2 71.1
171
184
194
5.5
6.0
6.5
63.1 67.8 72.1
151
164
174
4.5
5.0
5.5
64.4 69.2 73.4
151
164
174
5.5
5.5
5.5
65.1 70.2 74.5
141
154
164
6.0
6.0
6.5
66.5 71.7 76.1
131
144
154
5.5
5.5
6.0
70.3 75.3 79.6
141
154
164
ad
ed
40
4.5
55.3
177
5.0
57.6
157
5.5
57.4
137
4.5
58.7
137
5.0
59.2
127
6.0
60.6
117
5.0
64.3
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.14
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 10000 FT
if
d
or
pr
in
te
d
80
6.0
73.0
225
6.0
75.5
205
6.5
76.6
185
5.5
78.0
185
5.5
79.1
175
6.0
80.8
165
6.0
84.5
175
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
61.2 65.6 69.4
191
204
214
5.0
5.5
6.0
63.7 68.0 72.0
171
184
194
5.5
6.0
6.0
64.0 68.7 72.9
151
164
174
4.5
5.0
5.0
65.3 70.1 74.3
151
164
174
5.0
5.5
5.5
65.9 71.1 75.3
141
154
164
6.0
6.0
6.5
67.4 72.6 76.9
131
144
154
5.5
5.5
6.0
71.2 76.2 80.6
141
154
164
ad
ed
40
4.5
56.0
177
5.0
58.4
157
5.5
58.2
137
4.5
59.5
137
5.0
60.1
127
6.0
61.4
117
5.0
65.0
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.15
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 11000 FT
if
d
U
nc
on
tro
lle
80
6.0
73.8
226
6.0
76.3
206
6.5
77.5
186
5.5
79.0
186
5.5
80.1
176
6.0
81.8
166
6.0
85.5
176
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
62.2 66.3 70.3
191
204
215
5.0
5.5
6.0
64.5 69.0 73.0
171
184
195
5.5
6.0
6.0
64.9 69.7 73.8
151
164
175
4.5
5.0
5.0
66.2 71.1 75.1
151
164
175
5.0
5.5
5.5
67.0 72.1 76.2
141
154
165
6.0
6.0
6.5
68.5 73.6 78.0
131
144
155
5.5
5.5
6.0
72.2 77.2 81.6
141
154
165
ad
ed
40
4.5
56.8
177
5.0
59.4
157
5.5
59.4
137
4.5
60.7
137
5.0
61.2
127
6.0
62.6
117
5.0
66.1
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.16
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 12000 FT
if
d
or
pr
in
te
d
80
6.0
74.6
226
6.0
77.2
206
6.5
78.5
186
5.5
79.9
186
5.5
81.1
176
6.0
82.8
166
5.5
86.6
176
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
63.0 67.1 71.2
191
204
215
5.0
5.5
6.0
65.3 69.9 73.7
171
184
195
5.5
6.0
6.0
65.8 70.6 74.7
151
164
175
4.5
5.0
5.0
67.1 72.0 76.0
151
164
175
5.0
5.5
5.5
68.0 73.0 77.2
141
154
165
6.0
6.0
6.0
69.7 74.5 78.9
131
144
155
5.5
5.5
5.5
73.2 78.3 82.6
141
154
165
ad
ed
40
4.5
57.6
178
5.0
60.4
158
5.5
60.4
138
4.5
61.7
138
5.0
62.2
128
6.0
63.6
118
5.0
67.3
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.17
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 13000 FT
if
d
U
nc
on
tro
lle
80
6.0
75.4
227
6.0
78.1
207
6.0
79.4
187
5.0
80.8
187
5.5
82.0
177
6.0
83.7
167
5.5
87.6
177
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
63.7 67.9 72.0
192
205
215
5.0
5.5
6.0
66.2 70.8 74.5
172
185
195
5.5
6.0
6.0
66.7 71.6 75.6
152
165
175
4.5
5.0
5.0
68.1 72.9 77.0
152
165
175
5.0
5.5
5.5
69.1 73.9 78.2
142
155
165
6.0
6.0
6.0
70.7 75.4 79.9
132
145
155
5.5
5.5
5.5
74.2 79.3 83.6
142
155
165
ad
ed
40
4.5
58.5
178
5.0
61.3
158
5.5
61.4
138
4.5
62.6
138
5.0
63.2
128
6.0
64.7
118
5.0
68.4
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.18
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 14000 FT
if
d
or
pr
in
te
d
80
6.0
76.3
227
6.0
79.0
207
6.0
80.3
187
5.5
81.7
187
5.5
82.9
177
6.0
84.7
167
5.5
88.6
177
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
64.4 68.7 72.8
192
205
215
5.0
5.5
6.0
67.1 71.6 75.3
172
185
195
5.5
6.0
6.0
67.7 72.4 76.5
152
165
175
4.5
5.0
5.0
69.1 73.7 77.9
152
165
175
5.0
5.5
5.5
70.1 74.8 79.1
142
155
165
6.0
6.0
6.0
71.7 76.5 80.9
132
145
155
5.5
5.5
5.5
75.1 80.2 84.5
142
155
165
ad
ed
40
4.5
59.4
178
5.0
62.2
158
5.5
62.3
138
4.5
63.5
138
5.0
64.1
128
6.0
65.8
118
5.0
69.5
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.19
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 14500 FT
if
d
U
nc
on
tro
lle
80
6.0
76.7
227
6.0
79.4
207
6.0
80.7
187
5.0
82.1
187
5.5
83.4
177
6.0
85.2
167
5.5
89.2
177
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
64.8 69.2 73.2
192
205
216
5.0
5.5
6.0
67.5 72.1 75.8
172
185
196
5.5
6.0
6.0
68.2 72.9 76.9
152
165
176
4.5
5.0
5.0
69.6 74.2 78.4
152
165
176
5.0
5.5
5.5
70.6 75.2 79.6
142
155
166
6.0
6.0
6.0
72.1 77.0 81.4
132
145
156
5.5
5.5
5.5
75.6 80.7 85.0
142
155
166
ad
ed
40
4.5
59.8
178
5.0
62.6
158
5.5
62.7
138
4.5
63.9
138
5.0
64.6
128
6.0
66.3
118
5.0
70.1
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.20
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = -2000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = -1000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
43.0 46.7
49.9
143
156
167
1.0
1.0
1.5
50.8 55.1
58.6
138
150
161
0.0
0.5
0.5
55.9 60.6
64.4
130
143
153
80
2.5
52.8
178
1.5
62.0
171
0.5
67.9
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
43.6 47.3
50.5
143
156
167
1.0
1.0
1.5
51.5 55.8
59.3
138
150
161
0.0
0.5
0.5
56.6 61.3
65.2
130
143
153
80
2.5
53.5
178
1.5
62.8
171
0.5
68.7
163
or
pr
in
te
d
40
2.0
38.9
128
1.0
46.1
124
0.0
50.5
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
39.5
128
1.0
46.7
124
0.0
51.2
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.21
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = SEA LEVEL
Flap placard speed exceeded in shaded area.
Airport Altitude = 1000 FT
80
2.5
54.2
178
1.5
63.6
171
0.5
69.5
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
44.7
48.7
51.8
143
156
167
1.0
1.0
1.5
52.9
57.2
60.9
138
150
161
0.0
0.5
0.5
58.1 62.9
66.8
131
143
153
80
2.5
54.9
178
1.5
64.4
171
0.5
70.3
163
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
44.1 48.0
51.1
143
156
167
1.0
1.0
1.5
52.2
56.5
60.1
138
150
161
0.0
0.5
0.5
57.3 62.1
66.1
131
143
153
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
40.2
128
1.0
47.3
124
0.0
51.9
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
40.7
128
1.0
47.9
124
0.0
52.6
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.22
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 2000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 3000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
45.4 49.3
52.5
143
156
167
1.0
1.0
1.5
53.6 58.0
61.7
138
150
161
0.0
0.5
0.5
58.9 63.7
67.5
131
143
153
80
2.5
55.6
178
1.5
65.1
171
0.5
71.1
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
46.0 49.9
53.2
143
156
167
1.0
1.0
1.5
54.3 58.7
62.5
138
150
161
0.0
0.5
0.5
59.6 64.5
68.3
131
143
153
80
2.5
56.3
178
1.5
65.9
171
0.5
72.0
163
or
pr
in
te
d
40
2.0
41.2
128
1.0
48.6
124
0.0
53.3
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
41.7
128
1.0
49.2
124
0.0
54.1
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.23
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 4000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 5000 FT
80
2.5
57.0
178
1.5
66.7
171
0.5
72.8
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
47.3
51.2
54.6
143
157
167
1.0
1.0
1.5
55.7
60.3
64.0
138
151
161
0.0
0.5
0.5
61.2 66.1
69.9
131
143
153
80
2.5
57.7
178
1.5
67.5
171
0.5
73.6
163
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
46.7 50.5
53.9
143
157
167
1.0
1.0
1.5
55.0
59.5
63.3
138
150
161
0.0
0.5
0.5
60.4 65.4
69.1
131
143
153
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
42.2
128
1.0
49.9
124
0.0
54.8
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
42.8
129
1.0
50.6
124
0.0
55.6
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.24
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 6000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 7000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
48.0 51.9
55.3
143
157
167
1.0
1.0
1.5
56.4 61.1
64.8
138
151
161
0.0
0.5
0.5
62.0 66.8
70.8
131
143
153
80
2.5
58.4
178
1.5
68.2
171
0.5
74.5
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
48.6 52.6
56.0
143
157
167
1.0
1.0
1.5
57.2 61.9
65.6
138
151
161
0.0
0.5
0.5
62.8 67.6
71.6
131
143
153
80
2.5
59.1
178
1.5
69.0
171
0.5
75.3
163
or
pr
in
te
d
40
2.0
43.4
129
1.0
51.3
124
0.0
56.3
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
44.0
129
1.0
52.0
124
0.0
57.0
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.25
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 8000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 9000 FT
80
2.5
59.8
178
1.5
69.8
171
0.5
76.1
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
49.9
54.1
57.4
143
157
168
1.0
1.5
1.5
58.8
63.4
67.1
138
151
161
0.5
0.5
0.5
64.4 69.3
73.3
131
143
153
80
2.5
60.6
179
1.5
70.6
172
0.5
76.9
163
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
49.2 53.3
56.7
143
157
167
1.0
1.0
1.5
58.0
62.7
66.4
138
151
161
0.0
0.5
0.5
63.6 68.4
72.5
131
143
153
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
44.6
129
1.0
52.7
124
0.0
57.8
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
45.3
129
1.0
53.4
124
0.0
58.6
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.26
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 10000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 11000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
50.6 54.7
58.1
143
157
168
1.0
1.5
1.5
59.6 64.2
67.9
138
151
161
0.5
0.5
0.5
65.2 70.1
74.1
131
143
153
80
2.5
61.4
179
1.5
71.4
172
0.5
77.8
164
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
51.3 55.5
58.8
143
157
168
1.0
1.5
1.5
60.4 65.1
68.7
138
151
161
0.5
0.5
0.5
66.0 71.0
74.9
131
143
153
80
2.5
62.2
179
1.5
72.3
172
0.5
78.7
164
or
pr
in
te
d
40
2.0
45.9
129
1.0
54.2
124
0.0
59.4
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
46.7
129
1.0
54.9
124
0.0
60.2
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.27
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 12000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 13000 FT
80
2.5
62.9
179
1.5
73.0
172
0.5
79.6
164
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
52.8
56.8
60.4
143
157
168
1.0
1.5
1.5
62.0
66.6
70.4
138
151
161
0.5
0.5
0.5
67.6 72.7
76.6
131
143
154
80
2.5
63.6
179
1.5
73.8
172
0.5
80.5
165
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
52.0 56.2
59.6
143
157
168
1.0
1.5
1.5
61.2
65.8
69.5
138
151
161
0.5
0.5
0.5
66.8 71.8
75.7
131
143
153
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
47.3
129
1.0
55.6
124
0.0
61.0
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
47.9
129
1.0
56.4
124
0.0
61.9
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.28
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 14000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 14500 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
53.5 57.6
61.3
143
157
168
1.0
1.5
1.5
62.9 67.5
71.3
138
151
161
0.0
0.5
0.5
68.6 73.6
77.6
131
144
154
80
2.5
64.4
180
1.5
74.6
172
0.5
81.4
165
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
53.9 58.0
61.7
144
157
168
1.0
1.5
1.5
63.4 68.0
71.7
138
151
161
0.0
0.0
0.5
69.2 74.1
78.1
131
144
154
80
2.5
64.7
180
1.5
75.0
172
0.5
81.9
165
or
pr
in
te
d
40
2.0
48.7
129
1.0
57.4
124
0.0
62.9
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
49.1
129
1.0
58.0
124
0.0
63.4
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.29
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
GO-AROUND
Flaps 15, Gear Up, Set Go-Around Thrust
5000
SEA
LEVEL
U
nc
on
tro
lle
d
if
-2000
80
9.0
1400
175
10.5
1700
174
12.5
2200
173
14.0
2600
173
14.5
2500
173
or
pr
in
te
d
10000
WEIGHT (1000 KG)
50
60
70
14.0
11.5
10.5
2700
2200
1700
141
154
164
16.0
13.5
12.0
3200
2600
2100
141
153
163
19.0
16.0
14.0
3800
3100
2600
141
153
163
22.0
18.5
16.0
4300
3600
3000
141
153
163
22.5
18.5
16.0
4200
3500
3000
140
153
163
ad
ed
14500
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
40
17.5
3500
127
20.0
4000
127
24.0
4600
127
28.0
5200
127
28.0
5100
127
do
w
nl
o
PRESSURE ALTITUDE (FT)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.30
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Max Climb %N1
file Highlight
Based on engine bleed for packs on or off and anti-ice off
PRESSURE ALTITUDE (FT)/SPEED (KIAS/MACH)
10000
15000
20000
25000
30000
35000
280
280
280
280
280
.78
90.4
90.6
90.4
92.1
93.8
95.1
91.3
91.4
90.8
91.5
93.1
94.4
92.1
92.2
91.7
91.5
92.4
93.7
92.8
93.0
92.6
92.4
92.4
93.0
93.6
93.8
93.4
93.2
93.2
92.3
94.3
94.5
94.3
94.0
94.0
93.0
95.0
95.2
95.1
94.8
94.7
93.9
95.7
95.9
95.9
95.5
95.4
94.7
96.5
96.7
96.6
96.2
96.1
95.4
95.9
97.5
97.4
96.9
96.7
96.2
95.1
97.8
98.3
97.7
97.4
96.9
94.3
97.0
99.2
98.6
98.1
97.7
93.5
96.2
98.6
99.6
99.1
98.5
92.7
95.4
97.8
99.6
100.0
99.2
91.9
94.6
97.1
98.8
100.3
100.2
91.0
93.8
96.3
98.0
99.6
101.1
90.2
93.0
95.5
97.2
98.7
100.8
89.4
92.2
94.7
96.4
97.9
100.0
88.5
91.3
93.9
95.6
97.1
99.1
87.7
90.5
93.1
94.8
96.3
98.3
86.8
89.6
92.3
93.9
95.4
97.4
37000
.78
95.2
94.5
93.8
93.1
92.4
92.4
93.3
94.1
94.9
95.7
96.5
97.3
98.2
99.0
99.8
100.8
101.3
100.5
99.6
98.8
97.9
41000
.78
93.5
92.8
92.1
91.4
90.7
90.8
91.8
92.8
93.7
94.6
95.6
96.5
97.5
98.4
99.4
100.4
101.0
100.1
99.3
98.4
97.6
or
pr
in
te
d
5000
280
90.5
91.2
92.0
92.6
93.3
94.0
94.8
94.8
94.0
93.2
92.5
91.7
90.9
90.1
89.3
88.5
87.6
86.8
86.0
85.1
84.3
ad
ed
60
55
50
45
40
35
30
25
20
15
10
5
0
-5
-10
-15
-20
-25
-30
-35
-40
0
280
90.2
91.0
91.7
92.4
93.1
93.6
92.9
92.2
91.4
90.6
89.9
89.1
88.3
87.6
86.8
86.0
85.2
84.3
83.5
82.7
81.8
do
w
nl
o
TAT (°C)
%N1 Adjustments for Engine Bleeds
BLEED CONFIGURATION
ENGINE ANTI-ICE
ENGINE & WING ANTI-ICE*
PRESSURE ALTITUDE (1000 FT)
10
20
30
35
-0.8
-0.9
-0.9
-0.8
-2.1
-2.5
-2.7
-3.0
41
-0.8
-3.0
U
nc
on
tro
lle
d
if
*Dual bleed sources
0
-0.6
-1.8
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.31
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Go-around %N1
Based on engine bleed for packs on, engine and wing anti-ice on or off
0
96.2
96.7
97.6
98.4
99.1
99.9
99.8
99.1
98.3
97.5
96.8
96.0
95.2
94.4
93.6
92.8
92.0
91.1
90.3
89.4
88.6
87.7
86.8
1000
96.8
96.6
97.8
98.5
99.2
100.0
100.4
99.7
98.9
98.1
97.4
96.6
95.8
95.0
94.2
93.4
92.6
91.8
90.9
90.1
89.2
88.4
87.5
2000
3000
4000
5000
6000
7000
8000
96.8 97.5
97.8 97.7 97.5 98.2 98.8
98.6 98.7 98.8 98.7 98.5 98.5 99.0
99.3 99.4 99.5 99.6 99.5 99.1 98.9
100.1 100.1 100.3 100.3 100.2 99.9 99.6
100.7 100.7 100.7 100.7 100.7 100.6 100.4
100.2 100.6 100.9 100.9 100.9 100.9 100.9
99.5 99.8 100.2 100.5 100.9 101.0 101.1
98.7 99.1 99.4 99.8 100.1 100.5 100.9
98.0 98.3 98.7 99.0 99.4 99.8 100.2
97.2 97.6 97.9 98.3 98.7 99.0 99.4
96.4 96.8 97.2 97.5 97.9 98.3 98.7
95.6 96.0 96.4 96.8 97.2 97.5 97.9
94.8 95.2 95.6 96.0 96.4 96.8 97.1
94.0 94.4 94.8 95.2 95.6 96.0 96.4
93.2 93.6 94.0 94.4 94.8 95.2 95.6
92.4 92.8 93.2 93.6 94.0 94.4 94.8
91.6 92.0 92.4 92.8 93.3 93.6 94.0
90.7 91.1 91.6 92.0 92.4 92.8 93.2
89.9 90.3 90.7 91.2 91.6 92.0 92.4
89.0 89.4 89.9 90.3 90.8 91.2 91.5
88.2 88.6 89.0 89.5 90.0 90.3 90.7
9000 10000
98.8
99.6
100.4
100.9
101.0
101.3
100.5
99.8
99.0
98.3
97.5
96.7
95.9
95.1
94.3
93.5
92.7
91.9
91.0
99.1
99.5
100.3
100.8
101.0
101.2
100.9
100.2
99.4
98.6
97.9
97.1
96.3
95.5
94.7
93.9
93.0
92.2
91.4
or
pr
in
te
d
60
55
50
45
40
35
30
25
20
15
10
5
0
-5
-10
-15
-20
-25
-30
-35
-40
-45
-50
AIRPORT PRESSURE ALTITUDE (FT)
-2000
95.0
95.9
96.6
97.4
98.0
98.1
97.3
96.6
95.8
95.0
94.2
93.4
92.6
91.8
91.0
90.2
89.3
88.5
87.6
86.8
85.9
85.0
84.1
ad
ed
TAT
(°C)
do
w
nl
o
AIRPORT
OAT
°C
°F
57
134
52
125
47
116
42
108
37
99
32
90
27
81
22
72
17
63
12
54
7
45
2
36
-3
27
-8
18
-13
9
-17
1
-22
-8
-27
-17
-32
-26
-37
-35
-42
-44
-47
-53
-52
-62
%N1 Adjustments for Engine Bleeds
0
0.8
-0.1
1000
0.8
-0.1
2000
0.8
-0.1
if
-2000
0.7
-0.1
PRESSURE ALTITUDE (FT)
3000 4000 5000 6000 7000
0.8
0.9
0.9
0.9
0.9
-0.1 -0.1 -0.1 -0.1 -0.1
8000
0.9
-0.1
9000 10000
0.9
0.9
-0.1 -0.1
U
nc
on
tro
lle
d
BLEED
CONFIGURATION
PACKS OFF
A/C HIGH
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.32
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
VREF
file Highlight
40
159
154
148
143
139
133
127
121
114
107
15
174
169
163
157
153
147
140
133
126
119
U
nc
on
tro
lle
d
if
do
w
nl
o
ad
ed
85
80
75
70
65
60
55
50
45
40
FLAPS
30
167
162
156
151
147
141
134
128
121
114
or
pr
in
te
d
WEIGHT (1000 KG)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.30.33
Performance Inflight - QRH
General
do
w
nl
o
ad
ed
or
pr
in
te
d
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
U
nc
on
tro
lle
d
if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.30.34
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Advisory Information
Section 31
Advisory
file
Highlight
Information
ADVISORY INFORMATION
Runway Surface Condition Correlation
Advisory Information
Advisory Information
5
4
3
Dry
Wet (Smooth, Grooved or PFC) or Frost
3 mm (0.12 inches) or less of: Water, Slush, Dry Snow or Wet Snow
Compacted Snow at or below -15°C OAT
Wet (Slippery), Dry Snow or Wet Snow (any depth) over Compacted Snow
Greater than 3 mm (0.12 inches) of : Dry Snow or Wet Snow
Compacted Snow at OAT warmer than -15°C
Greater than 3 mm (0.12 inches) of: Water or Slush
Ice
Wet Ice, Water on top of Compacted Snow, Dry Snow or Wet Snow over Ice
Good
Good to Medium
Medium
Medium to Poor
Poor
Nil
U
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lle
d
if
do
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o
ad
ed
2
1
0
REPORTED
BRAKING
ACTION
Dry
RUNWAY SURFACE CONDITION DESCRIPTION
or
pr
in
te
d
RUNWAY
CONDITION
CODE
6
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.1
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
1295
1635
2265
2820
3085
85/-70
80/-80
120/-130
175/-185
205/-220
25/35
35/45
60/75
80/110
100/125
-40/140
-50/180
-85/295
-120/405
-140/470
40/50
45/60
60/75
80/110
100/125
-70/230
-70/240
-85/300
-120/405
-140/470
35/-30
35/-30
5/-5
35/-50
80/-90
55/70
60/75
65/85
85/110
100/125
-90/310
-90/315
-100/350
-125/430
-140/485
70/85
70/90
70/90
85/110
100/125
-110/385
-110/390
-115/405
-130/455
-145/495
Good Reported Braking Action
1705
1820
2270
2820
3085
85/-90
90/-100
120/-130
175/-185
205/-220
40
70
115
110
105
25
0
0
90
255
45
5
0
90
385
40/-40
40/-40
60/-60
80/-80
85/-85
50
65
115
110
105
75
85
5
90
255
165
190
10
90
385
65/-50
60/-50
35/-25
55/-60
90/-95
50/-50
50/-50
60/-65
80/-80
85/-85
60
70
115
110
105
145
150
80
110
260
345
360
220
180
415
90/-75
85/-70
70/-45
75/-70
105/-100
60/-60
60/-65
65/-70
80/-80
85/-85
70
80
115
110
105
220
220
150
130
270
525
530
430
265
450
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
10/-10
0/0
0/0
35/-50
80/-90
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF15
25/-25
35/-35
60/-60
80/-80
85/-85
ad
ed
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
2000
2080
2375
2850
3090
110/-115
120/-120
130/-140
175/-185
205/-220
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
2295
2345
2480
2880
3095
140/-140
145/-145
145/-150
180/-190
205/-220
U
nc
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
d
Medium Reported Braking Action
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
APP
SPD
ADJ
REVERSE
THRUST
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
-135/500
-135/505
-140/510
-150/545
-160/575
165/-115
160/-110
145/-95
145/-105
165/-130
70/-70
70/-75
70/-80
85/-85
90/-90
80
85
110
110
105
350
350
315
265
365
895
900
855
685
795
-160/615
-160/615
-165/615
-175/640
-180/655
235/-155
235/-150
225/-145
220/-145
225/-160
80/-85
80/-85
80/-85
85/-90
90/-100
85
90
105
110
105
475
475
485
405
460
1270
1270
1280
1105
1140
2635
2655
2745
3035
3210
170/-170
175/-175
175/-175
195/-205
215/-225
85/110
85/110
85/110
95/125
105/140
Poor Reported Braking Action
2970
2970
3005
3195
3325
200/-200
200/-200
200/-200
215/-220
225/-230
100/130
100/130
100/130
105/145
110/150
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
ad
ed
Medium To Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
PER
5 KTS ONE NO
ABOVE REV REV
VREF15
or
pr
in
te
d
REF
DIST
if
Reference distance is based on sea level, standard day, no wind or slope, VREF15, two-engine detent No. 2
reverse thrust, and auto speedbrakes.
For max manual braking and manual speedbrakes, increase reference landing distance by 70 m.
For autobrake and manual speedbrakes, increase reference landing distance by 60 m.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
All reference distances and adjustments shown have been increased by 15%.
U
nc
on
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lle
d
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.3
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
1250
1555
2130
2615
2850
70/-65
70/-75
115/-120
160/-165
185/-195
25/30
30/40
50/70
75/100
85/115
-40/140
-50/165
-85/280
-115/385
-130/455
40/50
40/50
50/70
75/100
85/115
-65/225
-70/235
-85/290
-115/385
-130/455
35/-30
35/-30
5/-10
35/-45
75/-80
50/65
50/70
60/80
75/100
85/115
-85/300
-85/310
-100/340
-120/410
-135/465
65/80
65/85
65/85
75/105
85/115
-105/375
-105/380
-110/390
-125/435
-140/470
Good Reported Braking Action
1640
1755
2135
2615
2850
80/-85
85/-90
115/-120
160/-165
185/-195
40
65
100
100
90
15
0
0
90
215
40
5
0
90
345
35/-35
40/-40
50/-50
70/-70
80/-80
50
65
100
100
90
70
75
5
90
215
150
165
10
90
345
65/-50
60/-50
35/-30
55/-60
90/-85
45/-45
50/-50
60/-60
70/-70
80/-80
60
70
100
100
90
130
130
70
110
220
300
315
195
170
375
90/-70
85/-70
65/-50
75/-70
105/-85
50/-60
60/-60
65/-65
75/-75
80/-80
70
80
100
100
90
190
190
130
130
225
450
460
380
245
405
do
w
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o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
10/-10
0/0
0/-5
35/-45
75/-80
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF30
25/-25
35/-35
50/-50
70/-70
80/-80
ad
ed
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1910
1995
2240
2645
2860
105/-110
110/-115
125/-130
160/-170
185/-195
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
2175
2235
2345
2675
2865
125/-130
130/-140
130/-140
160/-175
185/-195
U
nc
on
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lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
d
Medium Reported Braking Action
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.4
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
APP
SPD
ADJ
REVERSE
THRUST
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
-130/485
-130/490
-135/495
-145/525
-150/550
155/-105
150/-105
140/-95
140/-105
160/-120
65/-70
65/-70
70/-70
80/-80
85/-85
75
85
95
100
90
300
295
275
245
310
-155/600
-155/600
-160/600
-165/615
-165/635
220/-145
220/-140
215/-140
205/-140
220/-150
75/-80
75/-80
75/-80
80/-85
85/-90
80
90
90
100
90
410 1060
405 1060
415 1070
360 930
390 970
2480
2515
2585
2825
2975
155/-160
160/-160
160/-160
180/-185
195/-200
75/100
80/105
80/105
85/115
90/125
Poor Reported Braking Action
2780
2790
2825
2975
3085
185/-185
185/-185
185/-185
195/-195
200/-205
85/120
90/120
90/120
90/125
100/130
do
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MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
ad
ed
Medium To Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
PER
5 KTS ONE NO
ABOVE REV REV
VREF30
or
pr
in
te
d
REF
DIST
755
760
725
590
685
if
Reference distance is based on sea level, standard day, no wind or slope, VREF30, two-engine detent No. 2
reverse thrust, and auto speedbrakes.
For max manual braking and manual speedbrakes, increase reference landing distance by 70 m.
For autobrake and manual speedbrakes, increase reference landing distance by 60 m.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
All reference distances and adjustments shown have been increased by 15%.
U
nc
on
tro
lle
d
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.5
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
1200
1465
1975
2450
2690
60/-60
65/-70
105/-115
145/-155
175/-180
25/30
30/35
45/65
70/85
80/105
-40/130
-45/160
-80/270
-110/375
-125/435
35/45
40/50
45/65
70/85
80/105
-65/225
-70/230
-80/275
-110/375
-125/435
35/-30
30/-30
10/-5
30/-40
65/-75
45/60
50/65
50/70
70/90
80/105
-85/295
-85/300
-90/330
-115/400
-130/450
60/75
60/80
60/80
70/90
80/110
-105/370
-105/375
-105/380
-120/425
-130/460
Good Reported Braking Action
1580
1680
1980
2450
2690
75/-80
80/-85
105/-115
145/-155
175/-180
40
65
100
105
100
15
0
0
45
165
35
0
0
45
260
35/-35
35/-35
45/-50
65/-65
75/-75
50
65
105
105
100
65
70
5
45
165
140
150
10
45
260
60/-50
55/-45
40/-30
50/-50
80/-80
45/-45
45/-45
50/-55
65/-65
75/-75
60
70
100
105
100
120
120
70
70
175
270
280
195
125
290
85/-70
80/-65
70/-50
70/-65
90/-80
50/-50
50/-50
60/-60
70/-70
75/-75
70
80
100
105
100
175
175
130
90
185
405
410
375
200
315
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
10/-10
0/0
0/-5
30/-40
65/-75
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF40
25/-25
30/-30
45/-45
65/-65
75/-75
ad
ed
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1830
1905
2090
2485
2695
100/-100
105/-105
115/-125
145/-160
175/-180
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
2085
2125
2200
2515
2700
120/-120
125/-125
125/-130
150/-160
175/-180
U
nc
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
d
Medium Reported Braking Action
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.6
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
APP
SPD
ADJ
REVERSE
THRUST
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
-130/475
-130/480
-130/485
-140/515
-150/540
150/-105
150/-100
140/-95
135/-100
150/-110
60/-65
60/-65
65/-65
70/-75
80/-80
75
85
95
100
95
275
275
255
205
265
680
680
670
520
585
-155/585
-155/585
-155/585
-160/605
-165/620
220/-140
220/-140
215/-140
200/-130
205/-145
70/-75
70/-75
70/-75
75/-80
80/-85
80
85
90
100
90
375
375
380
315
350
955
955
965
840
855
2370
2395
2445
2670
2810
145/-145
150/-150
150/-155
165/-175
180/-185
70/95
70/100
70/100
80/105
85/120
Poor Reported Braking Action
2660
2665
2690
2820
2925
175/-175
175/-175
180/-180
185/-185
190/-195
80/115
85/115
85/115
85/120
90/125
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
ad
ed
Medium To Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
PER
5 KTS ONE NO
ABOVE REV REV
VREF40
or
pr
in
te
d
REF
DIST
if
Reference distance is based on sea level, standard day, no wind or slope, VREF40, two-engine detent No. 2
reverse thrust, and auto speedbrakes.
For max manual braking and manual speedbrakes, increase reference landing distance by 65 m.
For autobrake and manual speedbrakes, increase reference landing distance by 50 m.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
All reference distances and adjustments shown have been increased by 15%.
U
nc
on
tro
lle
d
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.7
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
file Highlight
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Airspeed Unreliable (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1185
1540
2600
85/-60
70/-75
160/-170
25/30
35/45
80/105
-35/125
-50/160
-110/360
10/-10
0/0
50/-55
80/-80
85/-90
160/-170
40/50
40/55
80/105
-60/205
-60/215
-110/360
30/-30
30/-20
50/-55
25
0
160
50
5
185
35/-35
40/-40
75/-75
N/A
N/A
N/A
75
85
160
175
195
185
50/65
55/70
80/105
-80/275
-80/280
-115/385
55/-50
55/-40
65/-65
45/-45
50/-50
75/-75
N/A
N/A
N/A
145
155
180
350
365
265
60/80
65/85
65/90
-95/340
-95/345
-100/365
80/-65
75/-60
55/-50
55/-55
55/-55
65/-65
N/A
N/A
N/A
215
220
125
520
535
385
75/100
80/105
80/110
-120/440
-120/440
-125/455
140/-100
135/-95
120/-85
65/-70
65/-70
70/-75
N/A
N/A
N/A
335
335
280
875
880
800
90/120
90/125
90/125
-145/535
-145/535
-145/540
195/-130
195/-125
185/-120
75/-80
75/-80
75/-80
N/A
N/A
N/A
455 1230
450 1225
430 1215
Good To Medium Reported Braking Action
1825
1915
2625
105/-105
105/-110
165/-175
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
25/-25
35/-35
75/-75
ad
ed
1560
1680
2600
REVERSE
THRUST
ADJ
N/A
N/A
N/A
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2085
2145
2335
125/-125
125/-130
130/-140
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
150/-150
155/-155
155/-160
d
2375
2415
2540
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2665
2680
2740
175/-175
180/-180
175/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.8
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Airspeed Unreliable (Flaps 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1145
1465
2415
65/-55
65/-70
145/-155
75/-75
80/-85
145/-155
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/125
-45/155
-105/345
10/-10
0/0
45/-50
20/-20
30/-30
65/-65
N/A
N/A
N/A
20
0
135
45
5
185
35/50
40/50
70/95
-60/200
-60/210
-105/345
30/-25
30/-20
45/-50
35/-35
35/-35
65/-65
N/A
N/A
N/A
70
80
135
155
175
185
-75/265
-80/275
-110/370
55/-45
55/-40
60/-60
45/-45
45/-45
65/-70
N/A
N/A
N/A
130
135
155
305
320
255
-90/330
-95/335
-100/350
80/-60
75/-60
60/-50
50/-50
50/-55
60/-60
N/A
N/A
N/A
185
190
115
450
465
340
70/95
75/95
70/95
-115/425
-120/430
-120/440
135/-95
130/-90
120/-85
60/-60
60/-65
65/-70
N/A
N/A
N/A
290
290
240
740
745
675
80/110
85/110
80/110
-140/520
-140/525
-140/525
185/-125
180/-120
180/-115
65/-70
70/-75
70/-75
N/A
N/A
N/A
390 1025
390 1025
365 1010
ad
ed
1505
1615
2415
REVERSE
THRUST
ADJ
20/30
30/40
70/95
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1745
1830
2440
95/-95
100/-105
150/-155
45/65
50/65
75/95
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
1980
2045
2190
115/-115
120/-120
120/-125
55/75
60/80
60/80
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
140/-140
145/-145
145/-145
d
2245
2290
2380
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2510
2535
2570
160/-160
165/-165
165/-165
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.9
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Airspeed Unreliable (Flaps 40)
VREF40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1105
1375
2280
55/-50
60/-65
135/-145
20/30
30/35
65/85
-35/120
-45/150
-100/335
10/-10
0/0
40/-45
70/-75
75/-80
135/-145
35/45
35/50
65/85
-55/200
-60/210
-100/335
N/A
N/A
N/A
20
0
105
40
0
125
30/-25
30/-25
40/-45
35/-35
35/-35
60/-60
N/A
N/A
N/A
65
70
105
145
160
125
45/60
45/65
70/90
-75/265
-75/270
-105/360
55/-45
55/-45
55/-55
45/-45
45/-45
65/-65
N/A
N/A
N/A
120
125
125
280
290
195
55/70
55/75
55/75
-90/325
-90/330
-95/345
75/-60
75/-60
60/-45
50/-50
50/-50
55/-55
N/A
N/A
N/A
170
175
115
410
420
335
65/90
70/90
65/90
-115/420
-115/425
-115/435
130/-90
130/-90
120/-80
60/-60
60/-60
60/-65
N/A
N/A
N/A
265
265
235
670
675
635
75/105
80/105
75/105
-135/515
-135/515
-135/520
185/-120
185/-115
180/-115
65/-70
65/-70
65/-70
N/A
N/A
N/A
355
355
355
925
925
935
Good To Medium Reported Braking Action
1680
1755
2305
90/-95
95/-100
135/-145
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1455
1550
2280
REVERSE
THRUST
ADJ
20/-20
30/-30
60/-60
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
1905
1960
2060
110/-110
110/-115
110/-120
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
135/-135
135/-135
135/-140
d
2155
2195
2255
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2405
2425
2450
155/-155
155/-155
155/-155
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.10
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
All Flaps Up Landing
VREF40 + 55
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1470
1965
3585
190/-80
90/-85
195/-225
90/-100
90/-100
195/-225
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-45/200
-60/190
-130/435
20/-15
5/0
60/-75
35/-35
50/-50
105/-105
45
75
115
40
5
215
85
15
225
50/70
55/75
115/150
-70/235
-75/245
-130/435
40/-35
30/-25
60/-75
50/-50
55/-55
105/-105
50
75
115
110
95
215
255
250
225
-90/315
-95/320
-135/460
75/-65
70/-55
80/-85
65/-65
65/-70
110/-110
60
80
115
215
210
240
525
530
340
-110/390
-115/395
-120/420
110/-90
105/-85
65/-45
75/-75
75/-80
90/-90
70
80
125
320
325
185
795
805
570
110/145
110/145
110/150
-140/505
-145/505
-145/525
190/-135
190/-130
155/-100
90/-95
90/-95
100/-105
80
90
125
520 1395
520 1390
430 1265
130/175
130/175
130/175
-170/620
-170/615
-170/625
270/-180
270/-175
245/-155
105/-110
105/-110
110/-115
90
95
120
715 1990
710 1975
675 1955
ad
ed
1950
2135
3585
REVERSE
THRUST
ADJ
50/105
45/75
115/150
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
2335
2455
3615
125/-130
125/-130
200/-225
70/95
75/95
115/155
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2720
2775
3080
155/-160
155/-160
150/-165
85/115
90/115
90/120
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
195/-200
195/-200
190/-195
d
3155
3180
3370
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3590
3580
3660
230/-235
230/-235
225/-225
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.11
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
ANTISKID INOPERATIVE (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1860
100/-105
50/65
-80/280
50/-45
Autobrake Inoperative
Autobrake Inoperative
55/75
-95/340
75/-60
Autobrake Inoperative
Autobrake Inoperative
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
2070
120/-120
Good To Medium Reported Braking Action
2345
145/-145
45/-45
60
125
295
50/-50
65
185
460
795
70/95
-120/440 135/-95
Autobrake Inoperative
Autobrake Inoperative
60/-65
70
300
85/115
-140/535 190/-125
Autobrake Inoperative
Autobrake Inoperative
70/-75
75
410 1125
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
Good Reported Braking Action
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2615
170/-170
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
210/-210
d
3035
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
105/145
-190/760 395/-210
Autobrake Inoperative
Autobrake Inoperative
80/-95
85
710 2305
120/175
-235/985 600/-290
Autobrake Inoperative
Autobrake Inoperative
90/-110
90
1005 3480
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3455
250/-245
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.12
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
ANTISKID INOPERATIVE (Flaps 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1785
95/-100
110/-115
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-75/275
50/-40
Autobrake Inoperative
Autobrake Inoperative
40/-40
55
110
260
55/70
-90/335
75/-60
Autobrake Inoperative
Autobrake Inoperative
45/-50
65
165
395
-115/430 130/-90
Autobrake Inoperative
Autobrake Inoperative
55/-60
70
260
670
-135/520 180/-120
Autobrake Inoperative
Autobrake Inoperative
65/-70
75
355
940
ad
ed
1975
REVERSE
THRUST
ADJ
45/60
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
2225
135/-135
65/90
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2470
155/-155
75/105
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
190/-190
d
2855
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
95/135
-185/740 370/-195
Autobrake Inoperative
Autobrake Inoperative
75/-90
80
610 1895
110/160
-230/960 560/-270
Autobrake Inoperative
Autobrake Inoperative
85/-105
85
860 2845
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3235
225/-225
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.13
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
ANTISKID INOPERATIVE (Flaps 40)
VREF40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1715
90/-95
40/55
-75/270
50/-40
Autobrake Inoperative
Autobrake Inoperative
50/65
-90/330
75/-60
Autobrake Inoperative
Autobrake Inoperative
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1900
105/-110
Good To Medium Reported Braking Action
2135
130/-130
40/-40
60
100
235
45/-45
65
150
360
60/85
-115/420 130/-90
Autobrake Inoperative
Autobrake Inoperative
55/-55
70
240
605
70/100
-135/510 180/-115
Autobrake Inoperative
Autobrake Inoperative
60/-65
75
325
850
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
Good Reported Braking Action
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2370
150/-150
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
185/-185
d
2740
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
90/125
-180/730 365/-190
Autobrake Inoperative
Autobrake Inoperative
70/-85
80
560 1720
105/150
-225/945 550/-265
Autobrake Inoperative
Autobrake Inoperative
80/-100
85
795 2590
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3105
215/-215
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.14
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Jammed or Restricted Flight Controls (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1120
1420
2420
75/-60
70/-70
150/-160
75/-75
80/-85
150/-160
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/120
-45/155
-105/350
10/-10
0/0
35/-45
20/-20
30/-30
65/-65
35
60
90
20
0
105
45
5
105
35/45
40/50
70/95
-55/200
-60/210
-105/350
30/-25
30/-20
35/-45
35/-35
35/-35
65/-65
45
55
90
70
80
105
160
175
105
-75/265
-80/275
-110/370
55/-45
55/-40
55/-55
45/-45
45/-45
70/-70
55
65
90
135
140
125
325
335
180
-90/330
-95/335
-95/350
80/-65
75/-60
55/-40
50/-50
50/-55
55/-60
60
70
100
195
200
125
485
490
390
70/95
75/100
75/100
-115/430
-120/430
-120/440
140/-95
135/-95
120/-80
60/-65
60/-65
65/-70
70
75
95
310
315
275
825
825
780
85/115
85/115
85/115
-140/525
-140/525
-140/530
195/-125
195/-125
185/-115
70/-75
70/-75
70/-75
75
75
90
425 1165
425 1160
425 1165
ad
ed
1470
1570
2420
REVERSE
THRUST
ADJ
20/30
30/40
70/95
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1720
1790
2445
100/-100
100/-105
155/-165
45/60
50/65
75/95
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
1965
2010
2140
120/-120
120/-125
125/-130
55/75
60/80
60/80
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
145/-145
145/-150
150/-150
d
2245
2270
2350
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2525
2525
2555
170/-170
170/-170
170/-170
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.15
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LEADING EDGE FLAPS TRANSIT (Flaps 15)
VREF15 + 15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1230
1600
2725
80/-65
75/-75
170/-180
25/35
35/45
85/110
-40/130
-50/165
-110/370
15/-10
0/0
50/-60
80/-85
85/-90
170/-180
40/55
45/60
85/110
-60/210
-65/220
-110/370
35
65
90
25
0
175
55
5
210
35/-30
30/-20
50/-60
40/-40
40/-40
75/-75
45
65
90
85
95
175
195
215
210
55/75
60/75
85/115
-80/280
-85/290
-115/395
60/-50
55/-45
70/-70
50/-50
50/-50
80/-80
55
70
90
160
170
195
385
405
295
65/90
70/90
70/95
-100/350
-100/355
-105/370
85/-70
80/-65
60/-50
55/-60
60/-60
65/-70
60
70
95
235
240
140
575
590
430
80/110
85/110
85/115
-125/450
-125/455
-130/465
145/-105
145/-100
125/-90
65/-70
70/-75
75/-80
70
80
95
365
365
305
960
965
880
95/130
95/130
95/130
-145/545
-145/550
-150/555
205/-140
205/-130
190/-125
75/-80
80/-85
80/-85
75
85
90
490 1340
490 1340
465 1325
Good To Medium Reported Braking Action
1905
2000
2750
105/-110
110/-115
170/-180
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1630
1755
2725
REVERSE
THRUST
ADJ
25/-25
35/-35
75/-75
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2180
2245
2445
130/-130
135/-135
135/-145
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
160/-160
160/-160
160/-165
d
2485
2525
2655
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2785
2805
2865
185/-185
185/-185
185/-185
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.16
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM A (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1235
1425
2545
70/-60
65/-70
150/-165
90/-95
95/-100
150/-165
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-40/130
-45/150
-105/360
15/-15
5/0
0/-10
25/-25
30/-30
70/-70
45
60
140
30
0
0
50
5
0
45/60
45/60
70/90
-65/230
-70/230
-105/360
45/-40
40/-35
5/-10
40/-40
40/-45
70/-70
70
75
140
120
125
0
245
255
0
-85/305
-90/305
-115/385
80/-65
80/-65
30/-25
50/-55
50/-55
75/-75
80
85
140
225
225
50
510
515
250
-105/375
-105/375
-105/375
110/-90
115/-90
115/-80
60/-65
60/-65
60/-65
90
90
90
325
325
325
775
775
775
90/120
90/125
90/125
-135/480
-135/480
-135/480
185/-130
190/-135
190/-130
70/-80
75/-80
75/-80
100
100
100
500 1340
500 1345
500 1345
105/145
105/145
105/145
-160/580
-160/580
-160/580
255/-170
260/-175
260/-175
80/-90
85/-90
85/-90
105
105
105
675 1905
675 1910
675 1910
ad
ed
1720
1755
2545
REVERSE
THRUST
ADJ
25/35
30/40
70/90
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
2020
2035
2585
120/-125
125/-125
155/-170
60/80
60/80
75/95
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2315
2315
2315
145/-150
150/-150
150/-150
70/95
70/100
70/100
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
180/-180
185/-180
185/-180
d
2645
2645
2645
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2970
2970
2970
210/-210
215/-210
215/-210
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.17
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM A (Flaps 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1185
1350
2380
65/-55
60/-65
140/-150
25/30
25/35
65/85
-40/125
-45/145
-105/345
15/-15
0/0
0/-10
85/-90
90/-95
140/-150
40/55
40/55
65/85
-65/220
-65/225
-105/345
45
55
130
25
0
0
45
5
0
45/-40
40/-35
0/-10
40/-40
40/-40
65/-65
65
70
130
105
105
0
210
215
0
55/75
55/75
70/90
-85/290
-85/295
-110/370
75/-65
75/-60
25/-25
50/-50
50/-50
65/-70
75
80
130
190
190
45
430
430
200
65/90
65/90
65/90
-100/360
-100/360
-100/360
105/-85
110/-85
105/-75
55/-60
55/-60
55/-60
85
85
90
275
275
275
645
640
645
80/110
80/110
80/110
-125/465
-125/465
-125/465
175/-120
180/-125
175/-120
65/-70
65/-70
65/-70
90
90
95
420 1090
420 1085
420 1090
95/130
95/130
95/130
-150/565
-150/565
-150/565
240/-155
245/-160
245/-160
75/-80
75/-80
75/-80
95
95
95
565 1530
565 1530
565 1530
Good To Medium Reported Braking Action
1915
1920
2415
110/-115
115/-115
140/-155
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1640
1665
2380
REVERSE
THRUST
ADJ
25/-25
30/-30
65/-65
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2185
2175
2180
135/-135
135/-135
135/-135
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
165/-165
165/-165
165/-165
d
2480
2475
2480
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2775
2775
2775
190/-190
195/-190
195/-190
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.18
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM A (Flaps 40)
VREF40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1140
1270
2185
60/-50
55/-60
125/-140
80/-85
80/-90
125/-140
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/125
-40/140
-95/330
15/-15
0/0
0/-5
20/-20
25/-25
60/-60
45
55
125
25
5
0
35
10
0
40/50
40/50
60/75
-65/220
-65/220
-95/330
45/-35
35/-30
0/-5
35/-35
35/-35
60/-60
70
70
125
95
95
0
190
185
0
-85/290
-85/290
-100/355
75/-60
70/-55
30/-15
45/-45
45/-45
60/-65
80
80
125
170
170
45
375
370
190
-100/355
-100/355
-100/355
100/-80
105/-80
105/-75
55/-55
55/-55
55/-55
85
85
90
245
240
240
560
555
555
75/105
75/105
75/105
-125/455
-125/455
-125/455
165/-115
170/-120
170/-115
65/-65
65/-65
65/-65
90
90
95
370
370
370
935
930
930
85/120
90/120
90/120
-150/550
-145/550
-145/550
230/-150
235/-155
235/-155
70/-75
70/-75
70/-75
95
95
95
495 1305
495 1305
495 1305
ad
ed
1570
1570
2185
REVERSE
THRUST
ADJ
20/30
25/30
60/75
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1820
1815
2220
105/-110
105/-110
130/-140
50/70
50/70
60/80
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2070
2055
2060
125/-130
125/-130
125/-130
60/85
60/85
60/85
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
155/-155
155/-155
155/-155
d
2345
2335
2340
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2620
2615
2615
180/-180
180/-180
180/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.19
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM A AND SYSTEM B (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1685
80/-85
40/50
-60/195
35/-30
Autobrake Inoperative
Autobrake Inoperative
65/90
-100/335 100/-80
Autobrake Inoperative
Autobrake Inoperative
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
2390
135/-140
Good To Medium Reported Braking Action
2760
170/-175
40/-40
75
-5
60
60/-60
105
90
425
905
85/115
-125/430 160/-120
Autobrake Inoperative
Autobrake Inoperative
75/-75
115
225
100/135
-145/520 215/-160
Autobrake Inoperative
Autobrake Inoperative
85/-85
125
355 1385
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
Good Reported Braking Action
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
3130
200/-205
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
240/-240
d
3495
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
120/165
-180/650 345/-215
Autobrake Inoperative
Autobrake Inoperative
95/-100
130
580 2370
140/195
-210/780 475/-270
Autobrake Inoperative
Autobrake Inoperative
105/-115
135
805 3355
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3860
275/-270
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.20
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
LOSS OF SYSTEM B (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1245
55/-60
95/-95
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-40/145
15/-15
Autobrake Inoperative
Autobrake Inoperative
25/-25
40
35
55
45/60
-70/245
45/-40
Autobrake Inoperative
Autobrake Inoperative
40/-40
55
120
250
-90/325
80/-65
Autobrake Inoperative
Autobrake Inoperative
50/-50
65
215
490
-110/400 115/-90
Autobrake Inoperative
Autobrake Inoperative
60/-60
75
305
730
ad
ed
1715
REVERSE
THRUST
ADJ
25/35
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1995
120/-120
60/80
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2275
145/-145
70/95
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
175/-175
d
2575
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
85/120
-140/515 200/-130
Autobrake Inoperative
Autobrake Inoperative
70/-75
80
460 1215
100/140
-165/625 285/-170
Autobrake Inoperative
Autobrake Inoperative
80/-85
85
610 1695
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2875
200/-200
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.21
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
MANUAL REVERSION (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1685
80/-85
40/50
-60/195
35/-30
Autobrake Inoperative
Autobrake Inoperative
65/90
-100/335 100/-80
Autobrake Inoperative
Autobrake Inoperative
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
2390
135/-140
Good To Medium Reported Braking Action
2760
170/-175
40/-40
75
-5
60
60/-60
105
90
425
905
85/115
-125/430 160/-120
Autobrake Inoperative
Autobrake Inoperative
75/-75
115
225
100/135
-145/520 215/-160
Autobrake Inoperative
Autobrake Inoperative
85/-85
125
355 1385
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
Good Reported Braking Action
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
3130
200/-205
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
240/-240
d
3495
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
120/165
-180/650 345/-215
Autobrake Inoperative
Autobrake Inoperative
95/-100
130
580 2370
140/195
-210/780 475/-270
Autobrake Inoperative
Autobrake Inoperative
105/-115
135
805 3355
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3860
275/-270
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.22
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
One Engine Inoperative Landing (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1130
1420
2520
80/-60
70/-70
150/-160
75/-80
85/-90
150/-160
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/125
-45/155
-105/355
10/-10
0/0
10/-30
20/-20
30/-30
70/-70
35
60
115
0
0
0
20
0
5
35/50
40/50
70/90
-60/210
-65/220
-105/355
35/-30
35/-25
10/-30
35/-35
40/-40
70/-70
50
60
115
0
0
0
85
95
5
-80/285
-85/295
-115/385
70/-55
65/-50
35/-40
45/-45
50/-50
75/-75
60
70
115
0
0
0
180
185
55
-100/360
-100/365
-105/370
100/-80
95/-75
80/-60
55/-55
60/-60
60/-60
70
80
95
0
0
0
270
275
245
75/100
75/105
80/105
-130/475
-130/480
-135/480
185/-125
185/-120
175/-115
70/-70
70/-75
70/-75
80
90
95
0
0
0
475
480
465
90/120
90/125
95/125
-160/590
-160/590
-160/590
270/-170
270/-165
265/-170
80/-85
80/-85
80/-85
85
95
90
0
0
0
675
680
685
ad
ed
1520
1635
2520
REVERSE
THRUST
ADJ
20/30
30/40
70/90
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1820
1905
2555
100/-105
110/-115
155/-165
50/65
50/65
75/95
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2115
2175
2235
125/-130
130/-135
135/-140
60/80
60/80
65/85
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
160/-165
165/-165
165/-170
d
2485
2515
2565
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2850
2855
2890
190/-195
195/-195
195/-200
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.23
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
One Engine Inoperative Landing (Flaps 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1090
1350
2335
60/-55
60/-65
140/-145
20/25
25/35
65/85
-35/120
-45/145
-100/340
10/-10
0/0
15/-35
75/-75
80/-85
140/-145
35/45
35/50
65/85
-60/205
-60/215
-100/340
35
55
100
0
0
0
20
0
10
35/-30
30/-25
15/-35
35/-35
35/-35
65/-65
50
60
100
0
0
0
75
85
10
45/60
45/65
65/90
-80/280
-80/285
-105/370
65/-55
60/-50
40/-45
45/-45
45/-45
65/-65
60
70
100
0
0
0
155
160
55
55/75
55/75
60/75
-95/350
-100/355
-100/360
95/-75
90/-70
80/-65
50/-55
55/-55
55/-55
65
75
85
0
0
0
230
235
210
70/95
70/95
75/95
-125/460
-125/460
-130/465
170/-115
170/-110
165/-115
65/-65
65/-70
65/-70
75
85
85
0
0
0
395
395
390
85/110
85/110
85/110
-150/565
-150/565
-155/570
245/-155
245/-150
245/-160
75/-75
75/-80
75/-80
80
90
80
0
0
0
555
555
565
Good To Medium Reported Braking Action
1730
1815
2370
95/-100
100/-105
145/-150
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1460
1570
2335
REVERSE
THRUST
ADJ
20/-20
30/-30
65/-65
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2000
2055
2105
115/-120
120/-125
120/-130
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
145/-150
150/-155
150/-155
d
2325
2355
2395
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2650
2655
2685
175/-175
175/-180
175/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.24
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Stabilizer Trim Inoperative (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1120
1420
2420
75/-60
70/-70
150/-160
75/-75
80/-85
150/-160
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/120
-45/155
-105/350
10/-10
0/0
35/-45
20/-20
30/-30
65/-65
35
60
90
20
0
105
45
5
105
35/45
40/50
70/95
-55/200
-60/210
-105/350
30/-25
30/-20
35/-45
35/-35
35/-35
65/-65
45
55
90
70
80
105
160
175
105
-75/265
-80/275
-110/370
55/-45
55/-40
55/-55
45/-45
45/-45
70/-70
55
65
90
135
140
125
325
335
180
-90/330
-95/335
-95/350
80/-65
75/-60
55/-40
50/-50
50/-55
55/-60
60
70
100
195
200
125
485
490
390
70/95
75/100
75/100
-115/430
-120/430
-120/440
140/-95
135/-95
120/-80
60/-65
60/-65
65/-70
70
75
95
310
315
275
825
825
780
85/115
85/115
85/115
-140/525
-140/525
-140/530
195/-125
195/-125
185/-115
70/-75
70/-75
70/-75
75
75
90
425 1165
425 1160
425 1165
ad
ed
1470
1570
2420
REVERSE
THRUST
ADJ
20/30
30/40
70/95
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1720
1790
2445
100/-100
100/-105
155/-165
45/60
50/65
75/95
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
1965
2010
2140
120/-120
120/-125
125/-130
55/75
60/80
60/80
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
145/-145
145/-150
150/-150
d
2245
2270
2350
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2525
2525
2555
170/-170
170/-170
170/-170
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.25
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Asymmetry (1 ≤ Flap Lever <15)
VREF40 + 30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1225
1625
2765
95/-60
70/-75
160/-175
25/40
35/45
85/110
-40/130
-50/170
-110/375
15/-10
0/0
55/-60
75/-80
80/-85
160/-175
40/55
45/55
85/110
-60/210
-65/220
-110/375
40
65
90
25
0
180
55
5
220
30/-30
25/-20
55/-60
35/-40
40/-40
80/-80
45
65
90
80
70
180
175
175
220
55/70
55/75
85/115
-80/280
-85/285
-115/400
60/-50
55/-45
70/-70
45/-50
50/-50
80/-80
55
70
90
150
150
200
355
365
295
65/85
65/90
70/95
-95/345
-100/350
-105/375
85/-65
80/-65
55/-50
55/-60
60/-60
70/-70
60
70
95
220
225
125
535
550
375
80/110
80/110
85/115
-120/445
-125/450
-130/465
145/-100
140/-100
125/-90
70/-75
70/-75
75/-80
70
75
95
350
350
280
915
920
820
95/130
95/130
95/130
-145/545
-145/550
-150/555
205/-135
200/-130
190/-125
80/-85
80/-85
80/-85
75
80
95
480 1290
475 1290
435 1260
Good To Medium Reported Braking Action
1885
2000
2790
100/-105
105/-110
165/-180
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1600
1760
2765
REVERSE
THRUST
ADJ
25/-25
35/-35
80/-80
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2165
2240
2475
120/-125
125/-130
125/-135
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
150/-155
155/-155
150/-160
d
2485
2530
2685
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2800
2820
2890
180/-180
180/-180
175/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.26
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Asymmetry (Flap Lever 15 or 25)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1120
1420
2420
75/-60
70/-70
150/-160
75/-75
80/-85
150/-160
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/120
-45/155
-105/350
10/-10
0/0
35/-45
20/-20
30/-30
65/-65
35
60
90
20
0
105
45
5
105
35/45
40/50
70/95
-55/200
-60/210
-105/350
30/-25
30/-20
35/-45
35/-35
35/-35
65/-65
45
55
90
70
80
105
160
175
105
-75/265
-80/275
-110/370
55/-45
55/-40
55/-55
45/-45
45/-45
70/-70
55
65
90
135
140
125
325
335
180
-90/330
-95/335
-95/350
80/-65
75/-60
55/-40
50/-50
50/-55
55/-60
60
70
100
195
200
125
485
490
390
70/95
75/100
75/100
-115/430
-120/430
-120/440
140/-95
135/-95
120/-80
60/-65
60/-65
65/-70
70
75
95
310
315
275
825
825
780
85/115
85/115
85/115
-140/525
-140/525
-140/530
195/-125
195/-125
185/-115
70/-75
70/-75
70/-75
75
75
90
425 1165
425 1160
425 1165
ad
ed
1470
1570
2420
REVERSE
THRUST
ADJ
20/30
30/40
70/95
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1720
1790
2445
100/-100
100/-105
155/-165
45/60
50/65
75/95
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
1965
2010
2140
120/-120
120/-125
125/-130
55/75
60/80
60/80
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
145/-145
145/-150
150/-150
d
2245
2270
2350
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2525
2525
2555
170/-170
170/-170
170/-170
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.27
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Asymmetry (Flap Lever 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1080
1350
2250
60/-55
60/-65
140/-145
20/25
25/35
65/85
-35/120
-45/145
-100/335
10/-10
0/0
35/-45
70/-70
75/-80
140/-145
35/45
35/45
65/85
-55/195
-60/205
-100/335
35
55
85
20
0
95
35
5
100
30/-25
25/-20
35/-45
30/-30
35/-35
60/-60
45
55
85
65
70
95
140
155
100
45/60
45/60
65/90
-75/260
-75/265
-105/355
55/-45
50/-40
50/-55
40/-40
45/-45
60/-65
55
65
85
120
125
115
280
290
170
55/70
55/70
55/75
-90/325
-90/325
-95/340
75/-60
70/-55
55/-45
45/-50
50/-50
50/-55
60
70
85
170
175
115
415
425
340
65/90
65/90
65/90
-115/420
-115/420
-115/430
130/-90
130/-85
115/-80
55/-60
60/-60
60/-65
65
75
85
270
270
240
695
695
660
75/105
75/105
75/105
-135/510
-135/510
-135/515
180/-120
185/-115
175/-115
65/-70
65/-70
65/-70
70
80
80
365
365
365
970
965
975
Good To Medium Reported Braking Action
1640
1710
2275
90/-90
95/-100
140/-150
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1415
1505
2250
REVERSE
THRUST
ADJ
20/-20
30/-30
60/-60
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
1865
1910
2020
110/-110
115/-115
115/-120
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
135/-135
135/-135
140/-140
d
2120
2145
2215
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2370
2380
2410
155/-155
155/-155
160/-160
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.28
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Disagree (1 ≤ Indicated Flaps <15)
VREF40 + 30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1225
1625
2765
95/-60
70/-75
160/-175
75/-80
80/-85
160/-175
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-40/130
-50/170
-110/375
15/-10
0/0
55/-60
25/-25
35/-35
80/-80
40
65
90
25
0
180
55
5
220
40/55
45/55
85/110
-60/210
-65/220
-110/375
30/-30
25/-20
55/-60
35/-40
40/-40
80/-80
45
65
90
80
70
180
175
175
220
-80/280
-85/285
-115/400
60/-50
55/-45
70/-70
45/-50
50/-50
80/-80
55
70
90
150
150
200
355
365
295
-95/345
-100/350
-105/375
85/-65
80/-65
55/-50
55/-60
60/-60
70/-70
60
70
95
220
225
125
535
550
375
80/110
80/110
85/115
-120/445
-125/450
-130/465
145/-100
140/-100
125/-90
70/-75
70/-75
75/-80
70
75
95
350
350
280
915
920
820
95/130
95/130
95/130
-145/545
-145/550
-150/555
205/-135
200/-130
190/-125
80/-85
80/-85
80/-85
75
80
95
480 1290
475 1290
435 1260
ad
ed
1600
1760
2765
REVERSE
THRUST
ADJ
25/40
35/45
85/110
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1885
2000
2790
100/-105
105/-110
165/-180
55/70
55/75
85/115
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2165
2240
2475
120/-125
125/-130
125/-135
65/85
65/90
70/95
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
150/-155
155/-155
150/-160
d
2485
2530
2685
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2800
2820
2890
180/-180
180/-180
175/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.29
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Disagree (15 ≤ Indicated Flaps <30)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1120
1420
2420
75/-60
70/-70
150/-160
20/30
30/40
70/95
-35/120
-45/155
-105/350
10/-10
0/0
35/-45
75/-75
80/-85
150/-160
35/45
40/50
70/95
-55/200
-60/210
-105/350
35
60
90
20
0
105
45
5
105
30/-25
30/-20
35/-45
35/-35
35/-35
65/-65
45
55
90
70
80
105
160
175
105
45/60
50/65
75/95
-75/265
-80/275
-110/370
55/-45
55/-40
55/-55
45/-45
45/-45
70/-70
55
65
90
135
140
125
325
335
180
55/75
60/80
60/80
-90/330
-95/335
-95/350
80/-65
75/-60
55/-40
50/-50
50/-55
55/-60
60
70
100
195
200
125
485
490
390
70/95
75/100
75/100
-115/430
-120/430
-120/440
140/-95
135/-95
120/-80
60/-65
60/-65
65/-70
70
75
95
310
315
275
825
825
780
85/115
85/115
85/115
-140/525
-140/525
-140/530
195/-125
195/-125
185/-115
70/-75
70/-75
70/-75
75
75
90
425 1165
425 1160
425 1165
Good To Medium Reported Braking Action
1720
1790
2445
100/-100
100/-105
155/-165
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1470
1570
2420
REVERSE
THRUST
ADJ
20/-20
30/-30
65/-65
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
1965
2010
2140
120/-120
120/-125
125/-130
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
145/-145
145/-150
150/-150
d
2245
2270
2350
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2525
2525
2555
170/-170
170/-170
170/-170
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.30
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flap Disagree (30 ≤ Indicated Flaps <40)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1080
1350
2250
60/-55
60/-65
140/-145
70/-70
75/-80
140/-145
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/120
-45/145
-100/335
10/-10
0/0
35/-45
20/-20
30/-30
60/-60
35
55
85
20
0
95
35
5
100
35/45
35/45
65/85
-55/195
-60/205
-100/335
30/-25
25/-20
35/-45
30/-30
35/-35
60/-60
45
55
85
65
70
95
140
155
100
-75/260
-75/265
-105/355
55/-45
50/-40
50/-55
40/-40
45/-45
60/-65
55
65
85
120
125
115
280
290
170
-90/325
-90/325
-95/340
75/-60
70/-55
55/-45
45/-50
50/-50
50/-55
60
70
85
170
175
115
415
425
340
65/90
65/90
65/90
-115/420
-115/420
-115/430
130/-90
130/-85
115/-80
55/-60
60/-60
60/-65
65
75
85
270
270
240
695
695
660
75/105
75/105
75/105
-135/510
-135/510
-135/515
180/-120
185/-115
175/-115
65/-70
65/-70
65/-70
70
80
80
365
365
365
970
965
975
ad
ed
1415
1505
2250
REVERSE
THRUST
ADJ
20/25
25/35
65/85
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1640
1710
2275
90/-90
95/-100
140/-150
45/60
45/60
65/90
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
1865
1910
2020
110/-110
115/-115
115/-120
55/70
55/70
55/75
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
135/-135
135/-135
140/-140
d
2120
2145
2215
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2370
2380
2410
155/-155
155/-155
160/-160
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.31
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Trailing Edge Flaps Up Landing
VREF40 + 40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1325
1755
3130
110/-70
75/-75
175/-195
30/70
40/50
100/125
-40/140
-55/175
-120/400
15/-15
0/0
55/-65
85/-90
85/-95
175/-195
45/60
50/65
100/125
-65/225
-70/235
-120/400
40
70
105
30
0
170
65
10
180
40/-35
30/-20
55/-65
45/-45
45/-50
90/-90
50
70
105
95
90
170
210
220
180
60/80
65/85
100/130
-85/300
-90/305
-125/425
70/-60
65/-50
70/-75
55/-60
55/-60
90/-95
60
75
105
185
180
195
435
445
280
75/100
75/100
80/105
-105/370
-105/375
-115/395
100/-80
95/-75
60/-45
65/-70
65/-70
75/-80
65
75
115
270
270
160
655
665
485
95/125
95/125
95/130
-135/480
-135/480
-140/495
170/-120
170/-115
145/-95
80/-85
80/-85
85/-90
75
85
115
430 1135
430 1135
365 1040
110/150
110/150
110/150
-160/585
-160/585
-160/590
240/-160
240/-155
225/-140
90/-95
90/-95
95/-100
85
90
110
590 1610
585 1600
565 1595
Good To Medium Reported Braking Action
2105
2205
3160
110/-120
115/-120
180/-200
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1770
1920
3130
REVERSE
THRUST
ADJ
30/-30
40/-40
90/-90
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2435
2485
2715
135/-145
140/-145
135/-150
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
170/-180
175/-180
170/-180
d
2810
2830
2980
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3185
3175
3240
205/-210
205/-210
200/-205
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.32
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
Advisory
file
Highlight
Information
ADVISORY INFORMATION
Recommended Brake Cooling Schedule
Reference Brake Energy Per Brake (Millions of Foot Pounds)
180
10
67.3
69.5
70.5
71.4
73.2
74.8
76.3
59.7
61.6
62.5
63.4
64.9
66.2
67.4
51.8
53.6
54.4
55.1
56.5
57.5
58.3
44.1
45.5
46.2
46.8
48.0
48.8
49.3
36.4
37.6
38.2
38.7
39.7
40.2
40.6
0
60.8
62.8
63.7
64.6
66.2
67.5
68.7
54.9
56.7
57.5
58.3
59.8
60.9
61.8
48.1
49.7
50.4
51.1
52.3
53.2
53.9
40.9
42.2
42.8
43.4
44.5
45.2
45.7
33.7
34.8
35.3
35.8
36.7
37.2
37.5
5
69.6
71.9
72.9
73.9
75.7
77.4
79.0
62.7
64.8
65.7
66.5
68.2
69.6
70.9
54.8
56.6
57.4
58.2
59.6
60.7
61.7
46.4
48.0
48.7
49.3
50.6
51.4
52.1
38.2
39.5
40.0
40.6
41.6
42.2
42.6
10
81.2
83.9
85.1
86.2
88.4
90.5
92.9
72.9
75.4
76.4
77.4
79.4
81.2
83.0
63.5
65.6
66.5
67.4
69.1
70.5
71.9
53.6
55.4
56.2
56.9
58.4
59.4
60.3
43.9
45.4
46.0
46.6
47.8
48.6
49.1
or
pr
in
te
d
0
22.4
23.1
23.5
23.8
24.4
24.7
24.8
20.2
20.8
21.1
21.4
22.0
22.2
22.3
18.0
18.5
18.8
19.1
19.6
19.8
19.8
15.7
16.3
16.5
16.7
17.2
17.3
17.3
13.5
14.0
14.2
14.4
14.8
14.9
14.9
do
w
nl
o
10
19.3
20.0
20.2
20.5
21.1
21.3
21.3
17.5
18.1
18.4
18.6
19.1
19.3
19.3
15.7
16.3
16.5
16.7
17.2
17.3
17.3
14.0
14.4
14.7
14.9
15.2
15.4
15.4
12.3
12.7
12.9
13.1
13.4
13.5
13.5
if
5
17.0
17.6
17.8
18.1
18.5
18.7
18.7
15.4
15.9
16.2
16.4
16.8
17.0
17.0
13.9
14.3
14.6
14.8
15.1
15.3
15.3
12.3
12.7
12.9
13.1
13.4
13.6
13.6
10.8
11.2
11.4
11.5
11.8
11.9
11.9
d
0
15.1
15.6
15.8
16.0
16.4
16.6
16.6
13.7
14.2
14.4
14.6
14.9
15.1
15.1
12.3
12.7
12.9
13.1
13.4
13.6
13.5
11.0
11.3
11.5
11.6
11.9
12.1
12.0
9.6
10.0
10.1
10.2
10.5
10.6
10.6
nc
on
tro
lle
WEIGHT OAT
(1000 KG) (°C)
0
10
15
80
20
30
40
50
0
10
15
70
20
30
40
50
0
10
15
60
20
30
40
50
0
10
15
50
20
30
40
50
0
10
15
40
20
30
40
50
WIND CORRECTED BRAKES ON SPEED (KIAS)*
100
120
140
160
PRESSURE ALTITUDE (1000 FT)
5 10 0
5 10 0
5 10 0
5
25.3 28.9 30.9 35.0 40.2 40.4 45.9 53.0 50.8 57.9
26.1 29.8 31.9 36.2 41.5 41.8 47.5 54.8 52.5 59.9
26.5 30.3 32.4 36.7 42.1 42.4 48.2 55.6 53.3 60.7
26.9 30.7 32.8 37.2 42.7 42.9 48.8 56.3 54.0 61.5
27.6 31.5 33.7 38.2 43.8 44.0 50.0 57.7 55.3 63.1
27.9 31.9 34.1 38.7 44.4 44.7 50.9 58.8 56.3 64.3
28.0 32.1 34.3 39.0 44.9 45.2 51.5 59.7 57.1 65.4
22.8 26.0 27.7 31.3 35.9 36.1 41.0 47.2 45.3 51.6
23.5 26.8 28.6 32.4 37.1 37.3 42.3 48.7 46.8 53.3
23.9 27.2 29.0 32.8 37.6 37.8 43.0 49.4 47.5 54.0
24.2 27.6 29.4 33.3 38.1 38.4 43.5 50.1 48.1 54.8
24.8 28.3 30.2 34.1 39.1 39.3 44.6 51.4 49.3 56.1
25.1 28.6 30.5 34.6 39.6 39.9 45.3 52.2 50.1 57.1
25.2 28.8 30.7 34.8 40.0 40.2 45.8 52.9 50.7 58.0
20.3 23.1 24.4 27.6 31.6 31.7 35.9 41.2 39.6 45.0
20.9 23.8 25.2 28.5 32.6 32.7 37.1 42.6 40.9 46.5
21.2 24.2 25.6 29.0 33.1 33.2 37.6 43.2 41.5 47.1
21.5 24.5 26.0 29.4 33.5 33.6 38.1 43.8 42.0 47.8
22.1 25.1 26.6 30.1 34.4 34.5 39.1 44.9 43.1 49.0
22.3 25.4 26.9 30.5 34.9 35.0 39.7 45.6 43.8 49.8
22.4 25.5 27.0 30.6 35.1 35.2 40.0 46.0 44.2 50.4
17.7 20.2 21.2 23.9 27.3 27.2 30.8 35.3 33.8 38.3
18.3 20.8 21.9 24.7 28.2 28.1 31.8 36.5 34.9 39.6
18.6 21.1 22.2 25.1 28.6 28.6 32.3 37.0 35.4 40.2
18.9 21.4 22.5 25.4 29.0 28.9 32.8 37.5 35.9 40.7
19.3 22.0 23.1 26.1 29.7 29.7 33.6 38.4 36.8 41.8
19.5 22.2 23.4 26.4 30.1 30.1 34.0 39.0 37.4 42.4
19.6 22.3 23.4 26.5 30.3 30.2 34.2 39.3 37.6 42.8
15.2 17.3 17.9 20.2 23.0 22.8 25.8 29.4 28.1 31.8
15.8 17.9 18.5 20.9 23.8 23.6 26.6 30.4 29.0 32.8
16.0 18.1 18.8 21.2 24.1 23.9 27.0 30.8 29.4 33.3
16.2 18.4 19.1 21.5 24.5 24.2 27.4 31.3 29.8 33.8
16.6 18.9 19.6 22.1 25.1 24.9 28.1 32.1 30.6 34.6
16.8 19.1 19.8 22.3 25.4 25.2 28.4 32.5 31.0 35.1
16.8 19.1 19.8 22.3 25.5 25.2 28.6 32.7 31.1 35.3
ad
ed
80
U
*To correct for wind, enter table with the brakes on speed minus one half the headwind or plus 1.5 times the
tailwind. If ground speed is used for brakes on speed, ignore wind and enter table with sea level, 15°C.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.31.33
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Recommended Brake Cooling Schedule
Adjusted Brake Energy Per Brake (Millions of Foot Pounds)
No Reverse Thrust
REFERENCE BRAKE ENERGY PER BRAKE (MILLIONS OF FOOT POUNDS)
10
20
30
40
50
60
70
80
90
10
20
30
40
50
60
70
80
90
7.8
16.3
25.3
34.7
44.7
55.0
65.7
76.6
87.9
7.5
15.4
23.6
32.4
41.8
51.8
62.5
74.1
86.5
7.3
14.7
22.3
30.2
38.6
47.6
57.4
68.1
80.0
7.0
13.8
20.5
27.4
34.8
42.7
51.5
61.3
72.4
6.7
13.1
19.2
25.3
31.8
38.8
46.6
55.4
65.5
or
pr
in
te
d
LANDING
EVENT
RTO MAX MAN
MAX MAN
MAX AUTO
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
Two Engine Detent Reverse Thrust
REFERENCE BRAKE ENERGY PER BRAKE (MILLIONS OF FOOT POUNDS)
10
20
30
40
50
60
70
80
90
10
20
30
40
50
60
70
80
90
7.0
14.6
22.8
31.4
40.5
49.9
59.7
69.8
80.0
5.8
12.3
19.5
27.2
35.6
44.5
53.9
63.7
74.1
4.3
9.2
14.7
20.7
27.2
34.4
42.0
50.2
59.0
2.5
5.6
9.1
13.1
17.8
23.0
28.8
35.2
42.3
1.8
3.8
6.1
8.8
11.9
15.5
19.6
24.4
29.8
ad
ed
LANDING
EVENT
RTO MAX MAN
MAX MAN
MAX AUTO
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
EVENT ADJUSTED BRAKE ENERGY (MILLIONS OF FOOT POUNDS)
16 & BELOW
17
20
23
25
28
32
33 TO 48
49 & ABOVE
BRAKE TEMPERATURE MONITOR SYSTEM INDICATION ON CDS
UP TO 2.4
2.6
3.1
3.5
3.9
4.4
4.9
5.0 TO 7.5
7.5 & ABOVE
NO SPECIAL
1
2
3
4
5
6
FUSE PLUG
PROCEDURE
CAUTION
MELT ZONE
REQUIRED
10
20
30
40
50
60
if
INFLIGHT
GEAR DOWN
GROUND
do
w
nl
o
Cooling Time (Minutes) - Category C Steel Brakes
Cooling Time (Minutes) - Category N Carbon Brakes
on
tro
lle
d
EVENT ADJUSTED BRAKE ENERGY (MILLIONS OF FOOT POUNDS)
16 & BELOW
17
19
20.9 23.5 26.9 29.4
30 TO 41
41 & ABOVE
BRAKE TEMPERATURE MONITOR SYSTEM INDICATION ON CDS
UP TO 2.5
2.6
3
3.3
3.8
4.5
4.9
5.0 TO 7.1
7.1 & ABOVE
NO SPECIAL
1
4
5
6
7
7.6
FUSE PLUG
PROCEDURE
CAUTION
MELT ZONE
REQUIRED
6.7
16.0 24.1 34.2 45.9 53.3
INFLIGHT
GEAR DOWN
GROUND
U
nc
Observe maximum quick turnaround limit.
Table shows energy per brake added by a single stop with all brakes operating. Energy is assumed to be
equally distributed among the operating brakes. Total energy is the sum of residual energy plus energy
added.
Add 1.0 million foot pounds per brake for each taxi mile.
When in caution zone, wheel fuse plugs may melt. Delay takeoff and inspect after one hour. If overheat occurs
after takeoff, extend gear soon for at least 7 minutes.
When in fuse plug melt zone, clear runway immediately. Unless required, do not set parking brake. Do not
approach gear or attempt to taxi for one hour. Tire, wheel and brake replacement may be required. If
overheat occurs after takeoff, extend gear soon for at least 12 minutes.
Brake temperature monitor system (BTMS) indication on CDS systems page may be used 10 to 15 minutes
after airplane has come to a complete stop or inflight with gear retracted to determine recommended cooling
schedule.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.31.34
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Engine Inoperative
Section 32
Engine
file
Highlight
Inoperative
ENGINE INOP
Engine Inoperative
Engine Inoperative
Initial Max Continuous %N1
Based on .79M, A/C high and anti-ice off
27
96.6
97.2
97.8
98.6
98.7
98.0
97.2
96.4
95.6
94.9
94.1
93.2
92.4
29
96.3
96.9
97.5
98.3
99.2
99.1
98.4
97.6
96.8
96.0
95.2
94.4
93.5
PRESSURE ALTITUDE (1000 FT)
31
33
35
37
96.1
95.9
95.4
95.0
96.8
96.6
96.2
95.7
97.4
97.4
96.9
96.5
98.1
98.1
97.7
97.3
99.0
98.9
98.5
98.2
99.8
99.7
99.3
98.9
99.6
100.5
100.2
99.8
98.8
100.1
101.0
100.8
98.0
99.3
100.5
101.1
97.2
98.5
99.7
100.2
96.4
97.7
98.8
99.4
95.6
96.8
98.0
98.5
94.7
96.0
97.1
97.6
25
-1.2
-4.2
41
93.9
94.8
95.7
96.6
97.5
98.4
99.4
100.3
100.6
99.8
99.0
98.1
97.2
27
-1.1
-4.4
PRESSURE ALTITUDE (1000 FT)
29
31
33
35
37
-1.0
-0.9
-0.8
-0.8
-0.8
-4.5
-4.7
-5.0
-4.8
-4.8
39
-0.8
-4.8
41
-0.8
-4.8
U
nc
on
tro
lle
d
if
ENGINE ANTI-ICE
ENGINE & WING ANTI-ICE
do
w
nl
o
%N1 Adjustments for Engine Bleeds
BLEED CONFIGURATION
39
94.7
95.5
96.3
97.1
98.0
98.7
99.6
100.6
100.8
100.0
99.2
98.3
97.4
or
pr
in
te
d
20
15
10
5
0
-5
-10
-15
-20
-25
-30
-35
-40
25
96.8
97.4
98.0
98.3
97.5
96.7
96.0
95.2
94.4
93.6
92.8
92.0
91.2
ad
ed
TAT (°C)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.32.1
Performance Inflight - QRH
Engine Inoperative
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
Max Continuous %N1
37000 FT to 29000 FT Pressure Altitudes
-40
99.4
98.7
97.7
97.0
-35
100.2
99.6
98.6
97.8
-30
99.6
100.4
99.4
98.7
-50
97.4
97.0
95.9
94.6
-45
98.3
97.9
96.8
95.5
-40
99.2
98.8
97.7
96.4
-35
100.1
99.7
98.6
97.3
-30
99.8
100.6
99.4
98.1
-45
98.3
97.9
96.8
95.1
94.5
-40
99.2
98.8
97.7
96.0
95.4
-35
100.0
99.7
98.5
96.8
96.2
-30
100.8
100.6
99.4
97.7
97.1
-25
100.0
101.4
100.2
98.5
97.9
-45
98.2
98.0
96.5
94.7
93.2
-40
99.1
98.9
97.4
95.5
94.1
-35
100.0
99.7
98.3
96.4
94.9
-30
100.9
100.6
99.1
97.2
95.7
-25
101.1
101.5
100.0
98.0
96.5
-40
99.0
98.4
97.1
95.0
92.9
92.9
-35
99.9
99.3
98.0
95.9
93.7
93.7
-30
100.8
100.2
98.9
96.7
94.5
94.5
-25
101.6
101.0
99.7
97.5
95.3
95.3
-20
101.2
101.9
100.5
98.3
96.1
96.1
TAT (°C)
-25
98.8
100.1
100.3
99.5
TAT (°C)
-25
99.0
100.5
100.3
98.9
TAT (°C)
-20
99.1
100.6
101.1
99.3
98.7
TAT (°C)
-20
100.2
101.6
100.8
98.8
97.4
TAT (°C)
-15
100.2
101.3
101.4
99.1
96.9
96.9
do
w
nl
o
if
d
-20
97.6
99.3
100.7
100.4
-15
96.3
98.4
100.0
101.2
-10
94.7
97.5
99.2
100.9
-5
93.2
96.3
98.4
100.0
0
91.8
95.2
97.5
99.1
-15
96.8
98.6
100.2
100.6
-10
95.4
97.6
99.5
100.3
-5
94.0
96.5
98.6
99.5
0
92.7
95.4
97.7
98.8
-10
96.7
98.6
100.2
100.5
100.3
-5
95.3
97.5
99.4
99.7
101.1
0
93.9
96.3
98.4
98.9
100.7
5
92.6
95.1
97.4
98.1
99.8
-15
99.2
100.7
101.3
99.7
98.2
-10
98.0
99.7
100.5
100.5
98.9
-5
96.6
98.6
99.8
99.8
99.7
0
95.2
97.4
98.8
98.9
99.9
5
93.9
96.2
97.8
98.0
99.1
-10
99.1
100.4
101.1
99.9
97.7
97.7
-5
97.9
99.3
100.2
100.1
98.5
98.5
0
96.4
98.2
99.2
99.1
99.2
99.2
5
95.1
96.9
98.3
98.2
98.5
100.0
10
93.8
95.8
97.2
97.5
97.6
100.1
-20
98.0
99.6
100.8
99.8
-15
97.9
99.6
100.9
100.2
99.5
or
pr
in
te
d
-45
98.5
97.8
96.8
96.1
ad
ed
-50
97.6
96.9
96.0
95.2
on
tro
lle
37000 FT PRESS ALT
KIAS M
-55
160
.51
96.6
200
.63
96.0
240
.74
95.1
280
.86
94.3
35000 FT PRESS ALT
KIAS M
-55
160
.49
96.5
200
.60
96.1
240
.71
95.0
280
.82
93.8
33000 FT PRESS ALT
KIAS M
-50
160
.47
97.4
200
.58
97.0
240
.68
95.9
280
.79
94.3
320
.89
93.6
31000 FT PRESS ALT
KIAS M
-50
160
.45
97.3
200
.55
97.1
240
.66
95.6
280
.76
93.8
320
.85
92.4
29000 FT PRESS ALT
KIAS M
-45
160
.43
98.1
200
.53
97.5
240
.63
96.3
280
.73
94.2
320
.82
92.1
360
.91
92.1
%N1 Adjustments for Engine Bleeds
BLEED CONFIGURATION
PRESSURE ALTITUDE (1000 FT)
31
33
35
-0.9
-0.8
-0.8
-4.3
-4.5
-4.7
37
-0.8
-4.7
U
nc
ENGINE ANTI-ICE ON
ENGINE & WING ANTI-ICE ON
29
-0.9
-4.1
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.32.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Engine Inoperative
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
Max Continuous %N1
27000 FT to 20000 FT Pressure Altitudes
-30
100.6
99.6
98.2
96.1
94.0
93.4
-25
101.4
100.4
99.1
96.9
94.8
94.2
-20
102.2
101.2
99.9
97.7
95.6
95.0
-35
99.7
98.3
96.5
94.7
92.6
91.2
-30
100.5
99.2
97.4
95.5
93.4
92.1
-25
101.4
100.0
98.2
96.3
94.2
92.9
-20
102.2
100.9
99.0
97.1
95.0
93.7
-15
102.4
101.7
99.9
97.9
95.8
94.5
-35
99.5
98.4
96.8
95.1
93.0
91.4
-30
100.4
99.2
97.6
95.9
93.8
92.2
-25
101.2
100.1
98.5
96.7
94.6
93.1
-20
102.1
100.9
99.3
97.5
95.4
93.9
-30
100.0
99.3
98.1
96.5
94.7
93.0
-25
100.9
100.1
98.9
97.4
95.5
93.8
-20
101.7
101.0
99.7
98.2
96.3
94.6
-15
102.5
101.8
100.5
99.0
97.1
95.4
-10
102.8
102.6
101.3
99.8
97.9
96.1
-30
99.5
99.2
98.4
97.0
95.5
93.8
-25
100.4
100.0
99.2
97.8
96.3
94.6
-20
101.2
100.9
100.0
98.7
97.1
95.4
-15
102.0
101.7
100.8
99.5
97.9
96.2
-10
102.8
102.5
101.7
100.3
98.7
97.0
nc
TAT (°C)
-15
101.2
101.8
100.7
98.5
96.4
95.8
TAT (°C)
-10
101.4
101.5
100.7
98.7
96.5
95.3
TAT (°C)
-10
101.9
102.2
100.9
99.1
96.9
95.5
TAT (°C)
-5
101.8
102.3
102.1
100.6
98.6
96.9
TAT (°C)
-5
102.5
103.3
102.5
101.1
99.5
97.7
-15
102.9
101.8
100.1
98.3
96.2
94.7
do
w
nl
o
if
d
-10
100.2
100.8
101.3
99.3
97.2
96.6
-5
99.0
99.9
100.4
100.1
98.0
97.3
0
97.8
98.8
99.4
99.4
98.7
98.1
5
96.4
97.6
98.5
98.4
98.6
98.8
10
95.1
96.4
97.5
97.6
97.8
99.4
-5
100.3
100.6
100.5
99.5
97.3
96.1
0
99.1
99.5
99.5
99.5
98.0
96.9
5
97.7
98.4
98.6
98.6
98.6
97.6
10
96.5
97.3
97.6
97.6
97.8
98.4
15
95.2
96.2
96.7
96.9
97.2
98.2
-5
100.8
101.1
101.2
99.9
97.7
96.2
0
99.6
100.1
100.2
100.4
98.5
97.0
5
98.4
99.0
99.2
99.4
99.2
97.8
10
97.1
97.8
98.2
98.3
98.6
98.5
15
95.8
96.7
97.3
97.5
97.8
98.6
0
100.7
101.2
101.6
101.3
99.4
97.7
5
99.5
100.0
100.5
101.0
100.1
98.4
10
98.2
98.9
99.4
99.8
100.2
99.2
15
97.0
97.8
98.5
98.9
99.3
99.7
20
95.8
96.8
97.5
98.1
98.6
99.1
0
101.5
102.3
103.1
101.8
100.2
98.5
5
100.4
101.1
101.8
102.5
101.0
99.2
10
99.2
100.0
100.5
101.3
101.7
100.0
15
98.0
98.9
99.5
100.1
100.9
100.7
20
96.8
97.8
98.6
99.3
99.9
100.4
or
pr
in
te
d
-35
99.7
98.7
97.4
95.3
93.2
92.6
ad
ed
-40
98.8
97.8
96.5
94.4
92.4
91.8
on
tro
lle
27000 FT PRESS ALT
KIAS M
-45
160
.41
98.0
200
.51
96.9
240
.60
95.6
280
.70
93.6
320
.79
91.6
360
.88
91.0
25000 FT PRESS ALT
KIAS M
-40
160
.39
98.8
200
.49
97.5
240
.58
95.7
280
.67
93.9
320
.76
91.7
360
.85
90.4
24000 FT PRESS ALT
KIAS M
-40
160
.38
98.6
200
.48
97.5
240
.57
95.9
280
.66
94.2
320
.75
92.1
360
.83
90.6
22000 FT PRESS ALT
KIAS M
-35
160
.37
99.1
200
.46
98.4
240
.55
97.2
280
.63
95.7
320
.72
93.9
360
.80
92.2
20000 FT PRESS ALT
KIAS M
-35
160
.35
98.7
200
.44
98.3
240
.53
97.5
280
.61
96.2
320
.69
94.7
360
.77
93.0
U
%N1 Adjustments for Engine Bleeds
BLEED CONFIGURATION
ENGINE ANTI-ICE ON
ENGINE & WING ANTI-ICE ON
20
-0.9
-3.6
PRESSURE ALTITUDE (1000 FT)
22
24
25
-0.9
-1.0
-1.0
-3.8
-3.8
-3.9
27
-1.0
-4.0
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.32.3
Performance Inflight - QRH
Engine Inoperative
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
Max Continuous %N1
18000 FT to 12000 FT Pressure Altitudes
-15
101.0
101.2
100.3
98.7
97.2
95.3
-10
101.8
102.0
101.1
99.5
97.9
96.1
-5
102.6
102.8
101.9
100.3
98.7
96.9
-25
98.0
98.8
97.9
96.4
94.8
92.9
-20
98.8
99.6
98.7
97.2
95.6
93.7
-15
99.6
100.4
99.5
98.0
96.4
94.5
-10
100.4
101.2
100.3
98.8
97.2
95.3
-5
101.2
102.0
101.1
99.6
97.9
96.1
-20
97.4
97.9
97.4
96.3
94.9
93.1
-15
98.2
98.7
98.2
97.1
95.7
93.9
-10
99.0
99.5
99.0
97.8
96.5
94.7
-5
99.8
100.3
99.8
98.6
97.2
95.5
0
100.6
101.1
100.6
99.4
98.0
96.3
-15
97.0
97.9
97.3
96.3
94.8
93.2
-10
97.8
98.7
98.0
97.0
95.6
94.0
-5
98.6
99.5
98.8
97.8
96.4
94.8
0
99.4
100.3
99.6
98.6
97.2
95.6
5
100.1
101.0
100.3
99.3
97.9
96.4
TAT (°C)
0
101.6
103.1
102.7
101.0
99.5
97.6
TAT (°C)
0
101.6
102.8
101.9
100.3
98.7
96.9
TAT (°C)
5
100.4
101.8
101.3
100.1
98.7
97.0
TAT (°C)
10
99.3
101.5
101.1
100.0
98.7
97.1
do
w
nl
o
if
d
5
100.3
101.7
102.5
101.8
100.2
98.4
10
99.2
100.4
101.1
101.6
101.0
99.1
15
98.1
99.3
99.9
100.5
100.9
99.9
20
97.0
98.3
99.0
99.6
100.0
100.2
25
95.9
97.3
98.1
98.8
99.2
99.6
10
99.1
101.3
101.8
101.8
100.2
98.4
15
98.1
100.2
100.5
100.9
100.9
99.2
20
97.1
99.3
99.6
99.8
100.2
99.9
25
96.1
98.3
98.7
99.0
99.4
99.6
10
99.1
101.5
101.8
100.9
99.5
97.8
15
98.0
101.0
101.1
101.0
100.2
98.6
20
97.1
100.1
100.3
100.1
100.3
99.3
25
96.2
99.3
99.5
99.2
99.5
99.6
30
95.3
98.4
98.7
98.5
98.8
99.0
15
98.1
100.8
101.0
100.8
99.4
97.9
20
97.1
99.8
100.1
100.3
100.2
98.7
25
96.3
99.0
99.4
99.4
99.7
99.4
30
95.4
98.2
98.6
98.6
98.9
99.1
35
94.5
97.3
97.9
98.0
98.2
98.5
5
100.3
102.5
102.7
101.1
99.4
97.7
or
pr
in
te
d
-20
100.2
100.4
99.5
97.9
96.4
94.6
ad
ed
-25
99.3
99.6
98.7
97.1
95.6
93.8
on
tro
lle
18000 FT PRESS ALT
KIAS M
-30
160
.34
98.5
200
.42
98.7
240
.51
97.8
280
.59
96.3
320
.67
94.8
360
.75
93.0
16000 FT PRESS ALT
KIAS M
-30
160
.33
97.1
200
.41
98.0
240
.49
97.1
280
.57
95.6
320
.64
94.0
360
.72
92.1
14000 FT PRESS ALT
KIAS M
-25
160
.31
96.6
200
.39
97.1
240
.47
96.6
280
.54
95.5
320
.62
94.1
360
.69
92.2
12000 FT PRESS ALT
KIAS M
-20
160
.30
96.3
200
.38
97.1
240
.45
96.5
280
.52
95.5
320
.60
94.0
360
.67
92.3
%N1 Adjustments for Engine Bleeds
12
-0.9
-3.2
PRESSURE ALTITUDE (1000 FT)
14
16
-0.9
-0.9
-3.4
-3.4
18
-0.9
-3.5
U
nc
BLEED
CONFIGURATION
ENGINE ANTI-ICE ON
ENGINE & WING ANTI-ICE ON
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.32.4
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Engine Inoperative
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
Max Continuous %N1
10000 FT to 1000 FT Pressure Altitudes
-5
97.6
98.3
97.9
96.9
95.5
94.0
0
98.3
99.0
98.7
97.6
96.2
94.8
5
99.1
99.8
99.4
98.4
97.0
95.6
-5
95.7
95.5
94.8
94.1
93.3
92.3
0
96.4
96.3
95.6
94.9
94.1
93.1
5
97.2
97.1
96.4
95.7
94.9
93.9
10
98.0
97.8
97.2
96.5
95.7
94.7
15
98.8
98.6
97.9
97.3
96.5
95.5
0
95.6
95.3
94.9
94.0
93.3
92.4
5
96.4
96.1
95.6
94.8
94.1
93.2
10
97.2
96.9
96.4
95.6
94.9
94.0
15
98.0
97.6
97.2
96.4
95.7
94.7
0
94.7
94.3
93.8
93.2
92.4
91.5
5
95.4
95.1
94.6
93.9
93.2
92.3
10
96.2
95.9
95.4
94.7
94.0
93.1
15
97.0
96.7
96.1
95.5
94.8
93.9
TAT (°C)
10
99.8
100.5
100.2
99.1
97.8
96.4
TAT (°C)
20
99.2
99.4
98.7
98.1
97.2
96.2
TAT (°C)
25
98.8
99.2
98.7
97.9
97.2
96.3
TAT (°C)
25
98.5
98.2
97.7
97.1
96.3
95.4
20
98.7
98.4
98.0
97.2
96.4
95.5
do
w
nl
o
if
d
15
98.6
100.5
100.9
99.9
98.6
97.2
20
97.4
99.4
100.1
100.4
99.3
98.0
25
96.6
98.5
99.2
99.5
99.7
98.7
30
95.8
97.8
98.4
98.7
99.0
99.1
35
94.9
97.0
97.7
98.0
98.2
98.5
25
98.3
98.9
99.5
98.8
98.0
97.0
30
97.4
98.0
98.7
98.9
98.7
97.8
35
96.6
97.3
97.9
98.2
98.4
98.5
40
95.9
96.6
97.2
97.5
97.7
98.0
45
95.1
95.8
96.5
96.8
97.1
97.3
30
97.9
98.3
98.8
98.7
98.0
97.1
35
97.1
97.5
98.0
98.3
98.5
97.8
40
96.4
96.8
97.2
97.5
97.8
98.1
45
95.6
96.1
96.6
96.9
97.1
97.4
50
94.8
95.3
95.9
96.2
96.5
96.8
30
98.2
98.5
98.4
97.8
97.1
96.2
35
97.4
97.8
98.1
98.3
97.9
96.9
40
96.7
97.0
97.3
97.6
97.9
97.7
45
96.0
96.3
96.6
96.9
97.2
97.3
50
95.2
95.6
95.9
96.2
96.5
96.6
or
pr
in
te
d
-10
96.8
97.5
97.2
96.1
94.7
93.2
ad
ed
-15
96.0
96.7
96.4
95.3
93.9
92.4
on
tro
lle
10000 FT PRESS ALT
KIAS M
-20
160
.29
95.2
200
.36
96.0
240
.43
95.6
280
.51
94.5
320
.58
93.0
360
.65
91.6
5000 FT PRESS ALT
KIAS M
-10
160
.26
94.9
200
.33
94.7
240
.40
94.0
280
.46
93.3
320
.53
92.5
360
.59
91.5
3000 FT PRESS ALT
KIAS M
-5
160
.26
94.8
200
.32
94.5
240
.38
94.1
280
.45
93.2
320
.51
92.5
360
.57
91.6
1000 FT PRESS ALT
KIAS M
-5
160
.25
93.9
200
.31
93.5
240
.37
93.0
280
.43
92.3
320
.49
91.6
360
.55
90.7
20
97.8
97.4
96.9
96.3
95.6
94.7
%N1 Adjustments for Engine Bleeds
1
-0.6
-2.9
PRESSURE ALTITUDE (1000 FT)
3
5
-0.8
-0.8
-3.0
-2.7
10
-0.8
-3.2
U
nc
BLEED
CONFIGURATION
ENGINE ANTI-ICE ON
ENGINE & WING ANTI-ICE ON
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.32.5
Performance Inflight - QRH
Engine Inoperative
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
MAX CONTINUOUS THRUST
Driftdown Speed/Level Off Altitude
100 ft/min residual rate of climb
OPTIMUM
DRIFTDOWN
SPEED (KIAS)
271
263
255
247
238
229
219
209
199
187
U
nc
on
tro
lle
d
if
do
w
nl
o
ad
ed
Includes APU fuel burn.
LEVEL OFF ALTITUDE (FT)
ISA + 10°C
ISA + 15°C
ISA + 20°C
& BELOW
18500
17300
15900
20200
19000
17700
21600
20600
19400
23100
22200
21100
24700
23800
22800
26800
25800
24700
29100
28100
27000
31200
30400
29400
33300
32600
31700
35600
34900
34000
or
pr
in
te
d
WEIGHT (1000 KG)
START
LEVEL OFF
DRIFTDOWN
85
82
80
77
75
72
70
67
65
62
60
57
55
53
50
48
45
43
40
38
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.32.6
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Engine Inoperative
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
MAX CONTINUOUS THRUST
Driftdown/LRC Cruise Range Capability
Ground to Air Miles Conversion
or
pr
in
te
d
AIR DISTANCE (NM)
TAILWIND COMPONENT (KTS)
20
40
60
80
100
95
90
86
82
78
190
180
172
164
157
284
270
258
246
235
379
360
344
328
314
474
451
429
410
392
569
541
515
492
471
664
631
601
574
549
758
721
687
656
628
853
811
773
738
706
948
901
859
820
785
1043
991
945
902
863
1138
1081
1030
984
942
1232
1171
1116
1066
1020
1327
1261
1202
1148
1098
1422
1351
1288
1230
1177
1517
1441
1373
1312
1255
1611
1531
1459
1393
1333
1706
1621
1545
1475
1411
ad
ed
GROUND
DISTANCE
(NM)
100
200
300
400
500
600
700
800
900
1000
1100
1200
1300
1400
1500
1600
1700
1800
do
w
nl
o
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
100
80
60
40
20
138
128
120
112
106
275
256
239
225
212
413
384
359
337
317
551
512
479
449
423
689
640
598
562
529
826
768
718
674
635
964
896
838
786
741
1102
1025
957
898
846
1240
1153
1077
1011
952
1377
1281
1197
1123
1058
1515
1409
1317
1235
1164
1653
1537
1436
1348
1270
1792
1666
1556
1460
1375
1930
1794
1676
1573
1481
2068
1922
1796
1685
1587
2207
2051
1916
1798
1693
2345
2180
2036
1910
1799
2484
2309
2156
2023
1905
Driftdown/Cruise Fuel and Time
45
0.4
0.8
1.3
1.8
2.2
2.7
3.1
3.6
4.0
4.4
4.8
5.3
5.7
6.1
6.5
6.9
7.3
7.7
if
40
0.4
0.8
1.2
1.6
2.0
2.4
2.8
3.2
3.6
4.0
4.4
4.8
5.2
5.5
5.9
6.3
6.6
7.0
U
nc
on
tro
lle
100
200
300
400
500
600
700
800
900
1000
1100
1200
1300
1400
1500
1600
1700
1800
FUEL REQUIRED (1000 KG)
WEIGHT AT START OF DRIFTDOWN (1000 KG)
50
55
60
65
70
75
0.4
0.4
0.4
0.5
0.5
0.5
0.9
0.9
1.0
1.0
1.1
1.1
1.4
1.5
1.6
1.7
1.8
1.9
1.9
2.0
2.2
2.3
2.5
2.6
2.4
2.6
2.8
3.0
3.2
3.3
2.9
3.1
3.3
3.6
3.8
4.0
3.4
3.6
3.9
4.2
4.5
4.7
3.9
4.2
4.5
4.8
5.1
5.4
4.3
4.7
5.0
5.4
5.7
6.1
4.8
5.2
5.6
6.0
6.4
6.7
5.3
5.7
6.1
6.6
7.0
7.4
5.7
6.2
6.7
7.1
7.6
8.1
6.2
6.7
7.2
7.7
8.2
8.7
6.6
7.2
7.7
8.3
8.8
9.4
7.1
7.7
8.3
8.9
9.4
10.0
7.5
8.2
8.8
9.4
10.0
10.7
8.0
8.6
9.3
10.0
10.6
11.3
8.4
9.1
9.8
10.5
11.2
11.9
d
AIR DIST
(NM)
80
0.5
1.2
2.0
2.8
3.5
4.3
5.0
5.7
6.4
7.1
7.9
8.6
9.2
9.9
10.6
11.3
12.0
12.6
85
0.5
1.3
2.1
2.9
3.7
4.5
5.3
6.1
6.8
7.6
8.3
9.0
9.8
10.5
11.2
12.0
12.7
13.4
TIME
(HR:MIN)
0:16
0:33
0:49
1:06
1:22
1:39
1:55
2:11
2:28
2:44
3:01
3:17
3:34
3:51
4:07
4:24
4:41
4:57
Includes APU fuel burn.
Driftdown at optimum driftdown speed and cruise at long range cruise speed.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.32.7
Performance Inflight - QRH
Engine Inoperative
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Altitude Capability
100 ft/min residual rate of climb
85
80
75
70
65
60
55
50
45
40
ISA + 10°C & BELOW
15200
17200
19200
20900
22500
24100
26300
29000
31400
33800
PRESSURE ALTITUDE (FT)
ISA + 15°C
12600
15300
17400
19700
21300
23000
24800
27700
30500
33000
U
nc
on
tro
lle
d
if
do
w
nl
o
ad
ed
With engine anti-ice on, decrease altitude capability by 1200 ft.
With engine and wing anti-ice on, decrease altitude capability by 5500 ft.
ISA + 20°C
9900
12500
15000
17300
19800
21600
23500
25800
29200
31800
or
pr
in
te
d
WEIGHT (1000 KG)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.32.8
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Engine Inoperative
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
Long Range Cruise Control
96.2
.610
274
2487
93.9
.596
268
2295
91.9
.585
263
2143
89.5
.563
253
1953
87.0
.538
241
1764
84.1
.511
228
1577
81.0
.480
214
1392
if
29
31
ad
ed
98.5
.621
291
2886
96.1
.607
284
2662
94.0
.595
278
2481
92.2
.584
273
2330
90.0
.564
263
2140
87.7
.541
252
1950
85.2
.516
240
1762
82.3
.489
227
1575
79.4
.462
214
1402
27
or
pr
in
te
d
PRESSURE ALTITUDE (1000 FT)
19
21
23
25
96.4
.612
265
2317
93.7
.597
258
2114
91.4
.585
252
1958
88.7
.561
241
1767
85.9
.533
229
1580
82.8
.502
215
1394
96.4
.614
254
2146
93.3
.597
247
1938
90.7
.583
241
1777
87.7
.556
229
1586
84.6
.525
216
1400
96.2
.614
244
1971
92.7
.596
236
1765
89.7
.578
229
1600
86.4
.548
216
1410
95.7
.613
233
1793
91.8
.593
225
1593
88.3
.571
216
1421
94.8
.610
222
1613
90.7
.589
214
1424
U
nc
17
97.9
.616
300
3052
95.9
.603
294
2846
94.0
.593
288
2674
92.3
.582
283
2520
90.4
.563
274
2330
88.3
.543
263
2139
85.9
.520
252
1950
83.4
.495
239
1762
80.6
.469
227
1582
77.8
.445
215
1416
do
w
nl
o
15
95.5
.600
303
3033
94.0
.590
299
2870
92.5
.579
293
2709
90.7
.562
284
2518
88.7
.542
274
2327
86.5
.521
263
2137
84.2
.498
251
1948
81.6
.475
239
1764
79.1
.452
227
1594
76.2
.429
215
1434
d
10
91.8
.561
311
3067
90.1
.545
302
2875
88.4
.528
293
2684
86.5
.510
282
2494
84.5
.491
271
2306
82.3
.471
261
2124
80.2
.453
250
1954
77.8
.434
240
1791
75.5
.415
229
1636
73.0
.395
218
1485
on
tro
lle
WEIGHT
(1000 KG)
%N1
MACH
85
KIAS
FF/ENG
%N1
MACH
80
KIAS
FF/ENG
%N1
MACH
75
KIAS
FF/ENG
%N1
MACH
70
KIAS
FF/ENG
%N1
MACH
65
KIAS
FF/ENG
%N1
MACH
60
KIAS
FF/ENG
%N1
MACH
55
KIAS
FF/ENG
%N1
MACH
50
KIAS
FF/ENG
%N1
MACH
45
KIAS
FF/ENG
%N1
MACH
40
KIAS
FF/ENG
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.32.9
Performance Inflight - QRH
Engine Inoperative
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Diversion Fuel and Time
Ground to Air Miles Conversion
GROUND
DISTANCE
(NM)
200
400
600
800
1000
1200
1400
1600
1800
2000
AIR DISTANCE (NM)
TAILWIND COMPONENT (KTS)
20
40
60
80
100
190
180
172
164
158
379
361
344
328
315
570
542
517
494
473
759
721
687
657
630
949
902
859
820
786
1139
1082
1031
984
943
1328
1262
1202
1147
1099
1518
1442
1373
1311
1256
1707
1622
1544
1474
1412
1896
1801
1715
1637
1568
or
pr
in
te
d
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
100
80
60
40
20
298
272
249
230
214
600
547
501
462
429
903
823
753
694
644
1209
1100
1005
926
859
1516
1379
1259
1159
1075
1825
1659
1513
1393
1290
2137
1940
1768
1626
1506
2450
2222
2024
1860
1722
2766
2507
2281
2095
1938
3083
2792
2539
2331
2155
ad
ed
Reference Fuel and Time Required at Check Point
PRESSURE ALTITUDE (1000 FT)
18
22
26
FUEL
TIME
FUEL
TIME
FUEL
TIME
FUEL
TIME
FUEL
TIME
(1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN)
200
1.4
0:43
1.2
0:41
1.1
0:39
1.0
0:38
0.9
0:37
400
2.8
1:23
2.6
1:19
2.4
1:14
2.2
1:11
2.1
1:09
600
4.3
2:04
3.9
1:57
3.6
1:50
3.4
1:45
3.2
1:42
800
5.7
2:46
5.2
2:36
4.9
2:26
4.5
2:19
4.4
2:14
1000
7.1
3:28
6.6
3:15
6.1
3:03
5.7
2:53
5.5
2:47
1200
8.5
4:10
7.9
3:55
7.3
3:40
6.8
3:28
6.6
3:21
1400
9.8
4:53
9.1
4:36
8.5
4:18
8.0
4:02
7.7
3:54
1600
11.2
5:36
10.4
5:16
9.7
4:55
9.1
4:38
8.7
4:28
1800
12.5
6:20
11.7
5:58
10.9
5:34
10.2
5:13
9.8
5:02
2000
13.9
7:05
12.9
6:39
12.0
6:13
11.3
5:49
10.8
5:36
AIR
DIST
(NM)
14
on
tro
lle
d
if
do
w
nl
o
10
Fuel Required Adjustments (1000 KG)
U
nc
REFERENCE FUEL REQUIRED
(1000 KG)
1
2
3
4
5
6
7
8
9
10
11
12
13
14
40
-0.1
-0.3
-0.4
-0.6
-0.7
-0.8
-1.0
-1.1
-1.3
-1.4
-1.6
-1.7
-1.9
-2.0
45
-0.1
-0.2
-0.3
-0.4
-0.5
-0.6
-0.8
-0.9
-1.0
-1.1
-1.2
-1.3
-1.4
-1.5
WEIGHT AT CHECK POINT (1000 KG)
50
55
60
65
70
-0.1
0.0
0.0
0.1
0.1
-0.1
-0.1
0.0
0.2
0.3
-0.2
-0.1
0.0
0.3
0.5
-0.3
-0.1
0.0
0.3
0.7
-0.4
-0.2
0.0
0.4
0.9
-0.4
-0.2
0.0
0.5
1.1
-0.5
-0.3
0.0
0.6
1.2
-0.6
-0.3
0.0
0.6
1.4
-0.7
-0.3
0.0
0.7
1.5
-0.7
-0.4
0.0
0.7
1.6
-0.8
-0.4
0.0
0.8
1.7
-0.9
-0.4
0.0
0.8
1.9
-0.9
-0.5
0.0
0.9
2.0
-1.0
-0.5
0.0
0.9
2.0
75
0.2
0.6
0.9
1.2
1.4
1.7
2.0
2.2
2.4
2.6
2.8
3.0
3.2
3.4
80
0.3
0.8
1.2
1.6
2.0
2.4
2.8
3.2
3.5
3.8
4.1
4.4
4.7
4.9
Includes APU fuel burn.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.32.10
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Engine Inoperative
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
MAX CONTINUOUS THRUST
Holding
Flaps Up
30000
35000
ad
ed
or
pr
in
te
d
PRESSURE ALTITUDE (FT)
10000
15000
20000
25000
88.3
92.8
252
253
2750
2800
86.5
91.0
98.3
244
245
247
2570
2610
2740
84.7
89.1
95.0
236
238
239
2400
2420
2490
82.8
87.1
92.1
228
229
231
2230
2250
2270
80.8
85.0
89.7
97.7
220
221
222
224
2070
2070
2080
2230
78.5
82.8
87.4
93.7
211
212
213
214
1910
1910
1910
1970
76.3
80.5
84.9
90.0
202
203
204
205
1750
1740
1730
1760
73.8
77.8
82.3
87.0
192
193
194
195
1600
1580
1570
1570
71.0
75.0
79.4
84.0
184
184
184
185
1440
1430
1400
1400
67.8
72.0
76.2
80.7
177
177
177
177
1300
1270
1250
1240
if
do
w
nl
o
5000
84.1
251
2730
82.4
243
2570
80.5
236
2400
78.6
227
2240
76.7
219
2090
74.6
210
1930
72.3
201
1770
69.7
191
1620
66.9
184
1470
64.0
177
1330
d
1500
81.1
250
2740
79.5
242
2580
77.8
235
2420
76.0
227
2260
74.0
219
2100
71.7
210
1950
69.4
200
1800
67.0
191
1650
64.3
184
1500
61.1
177
1350
on
tro
lle
WEIGHT
(1000 KG)
%N1
85
KIAS
FF/ENG
%N1
80
KIAS
FF/ENG
%N1
75
KIAS
FF/ENG
%N1
70
KIAS
FF/ENG
%N1
65
KIAS
FF/ENG
%N1
60
KIAS
FF/ENG
%N1
55
KIAS
FF/ENG
%N1
50
KIAS
FF/ENG
%N1
45
KIAS
FF/ENG
%N1
40
KIAS
FF/ENG
94.9
196
1680
89.6
186
1450
85.4
177
1260
94.1
177
1360
U
nc
This table includes 5% additional fuel for holding in a racetrack pattern.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.32.11
Performance Inflight - QRH
Engine Inoperative
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
ENGINE INOP
ADVISORY INFORMATION
Gear Down Landing Rate of Climb Available
Flaps 15
0
-10
20
50
70
100
130
160
190
220
250
270
270
280
290
300
320
340
6000
8000
-250
-220
-190
-160
-140
-120
-100
-70
-60
-20
-10
-10
0
0
-320
-300
-280
-250
-230
-210
-190
-130
-120
-120
-120
-120
6000
8000
-570
-540
-510
-490
-470
-450
-430
-410
-390
-350
-360
-360
-370
-380
-650
-630
-610
-580
-560
-540
-520
-470
-470
-470
-490
-500
ad
ed
-2000
50
80
110
140
170
200
220
250
270
270
270
280
290
300
310
330
350
do
w
nl
o
52
50
48
46
44
42
40
38
36
34
32
30
20
10
0
-20
-40
or
pr
in
te
d
RATE OF CLIMB (FT/MIN)
PRESSURE ALTITUDE (FT)
2000
4000
-120
-80
-200
-50
-160
-30
-130
0
-100
30
-80
50
-50
80
-20
110
0
140
20
160
40
180
60
200
90
210
100
210
100
230
110
240
120
TAT (°C)
Rate of climb capability shown is valid for 60000 kg, gear down at VREF15+5.
Decrease rate of climb 120 ft/min per 5000 kg greater than 60000 kg.
Increase rate of climb 160 ft/min per 5000 kg less than 60000 kg.
-2000
-250
-220
-190
-170
-140
-110
-90
-60
-40
-40
-40
-40
-30
-20
-20
-10
-10
0
-310
-290
-260
-240
-210
-180
-160
-130
-100
-70
-50
-50
-50
-40
-40
-30
-30
U
nc
on
tro
lle
52
50
48
46
44
42
40
38
36
34
32
30
20
10
0
-20
-40
d
TAT (°C)
RATE OF CLIMB (FT/MIN)
PRESSURE ALTITUDE (FT)
2000
4000
-420
-390
-510
-360
-480
-340
-450
-320
-420
-290
-400
-260
-370
-240
-350
-210
-320
-180
-300
-160
-290
-150
-270
-130
-240
-130
-240
-130
-240
-130
-250
-130
-250
if
Flaps 30
Rate of climb capability shown is valid for 60000 kg, gear down at VREF30+5.
Decrease rate of climb 120 ft/min per 5000 kg greater than 60000 kg.
Increase rate of climb 170 ft/min per 5000 kg less than 60000 kg.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.32.12
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Gear Down
Section 33
GearHighlight
file
Down
GEAR DOWN
Gear Down
Gear Down
Long Range Cruise Altitude Capability
Max Cruise Thrust, 100 ft/min residual rate of climb
ISA + 20°C
9400
12600
15700
18600
21800
25300
28100
30700
33000
35400
or
pr
in
te
d
PRESSURE ALTITUDE (FT)
ISA + 15°C
12500
15500
18500
21400
24400
27100
29600
31900
34100
36500
U
nc
on
tro
lle
d
if
do
w
nl
o
85
80
75
70
65
60
55
50
45
40
ISA + 10°C & BELOW
15600
18400
21100
23600
26100
28600
30800
32900
35100
37500
ad
ed
WEIGHT (1000 KG)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.33.1
Performance Inflight - QRH
Gear Down
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
GEAR DOWN
Gear Down
Long Range Cruise Control
91.7
.557
240
1950
89.5
.543
233
1806
87.4
.525
225
1661
85.0
.504
216
1512
82.5
.482
206
1367
79.7
.458
196
1224
76.6
.434
185
1085
if
33
35
91.6
.560
231
1805
89.1
.544
224
1658
86.8
.525
216
1515
84.2
.502
206
1368
81.4
.477
196
1224
78.3
.452
185
1083
94.5
.578
229
1836
91.3
.562
222
1664
88.5
.545
215
1517
86.0
.523
206
1374
83.1
.498
196
1230
80.0
.471
185
1089
94.5
.580
220
1696
90.9
.562
213
1523
87.8
.544
205
1377
85.0
.520
196
1235
81.8
.491
185
1092
94.1
.581
211
1555
90.2
.561
203
1381
86.8
.541
195
1237
83.6
.513
185
1094
93.5
.580
201
1411
89.1
.559
193
1239
85.5
.535
185
1096
92.5
.578
191
1265
87.7
.554
183
1097
U
nc
31
or
pr
in
te
d
91.7
.554
248
2101
89.8
.541
242
1960
87.9
.524
234
1812
85.6
.504
225
1661
83.3
.484
216
1515
80.7
.463
206
1371
78.0
.441
196
1231
74.9
.417
185
1098
PRESSURE ALTITUDE (1000 FT)
25
27
29
ad
ed
23
do
w
nl
o
21
on
tro
lle
10
85.9
.482
267
2421
84.2
.468
259
2271
82.5
.454
251
2123
80.6
.440
243
1977
78.6
.425
235
1835
76.5
.409
226
1696
74.4
.393
217
1559
71.9
.376
207
1424
69.1
.358
197
1294
66.2
.340
187
1170
d
WEIGHT
(1000 KG)
%N1
85
MACH
KIAS
FF/ENG
%N1
80
MACH
KIAS
FF/ENG
%N1
75
MACH
KIAS
FF/ENG
%N1
70
MACH
KIAS
FF/ENG
%N1
65
MACH
KIAS
FF/ENG
%N1
60
MACH
KIAS
FF/ENG
%N1
55
MACH
KIAS
FF/ENG
%N1
50
MACH
KIAS
FF/ENG
%N1
45
MACH
KIAS
FF/ENG
%N1
40
MACH
KIAS
FF/ENG
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.33.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Gear Down
Category C/N Brakes
737 Flight Crew Operations Manual
GEAR DOWN
Long Range Cruise Enroute Fuel and Time
Ground to Air Miles Conversion
GROUND
DISTANCE
(NM)
200
400
600
800
1000
1200
1400
1600
1800
AIR DISTANCE (NM)
TAILWIND COMPONENT (KTS)
20
40
60
80
100
188
178
168
160
153
377
357
338
321
307
566
535
507
483
461
754
713
676
643
614
943
891
844
803
766
1131
1069
1013
962
918
1320
1247
1181
1122
1070
1508
1424
1348
1280
1221
1695
1600
1514
1438
1371
Reference Fuel and Time Required at Check Point
or
pr
in
te
d
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
100
80
60
40
20
324
290
260
236
217
654
583
523
474
435
989
880
787
713
653
1329
1181
1054
953
871
1674
1484
1322
1194
1090
2024
1791
1593
1436
1310
2381
2103
1865
1680
1530
2743
2417
2140
1924
1751
3113
2737
2418
2171
1972
PRESSURE ALTITUDE (1000 FT)
20
24
28
FUEL
TIME
FUEL
TIME
FUEL
TIME
FUEL
TIME
FUEL
TIME
(1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN) (1000 KG) (HR:MIN)
200
2.4
0:49
2.2
0:47
1.9
0:44
1.7
0:42
1.6
0:41
400
4.9
1:36
4.5
1:31
4.0
1:25
3.7
1:20
3.5
1:17
600
7.4
2:25
6.8
2:17
6.1
2:06
5.7
1:59
5.4
1:54
800
9.8
3:14
9.1
3:03
8.1
2:48
7.6
2:38
7.2
2:31
1000
12.1
4:04
11.3
3:50
10.1
3:30
9.5
3:18
9.0
3:08
1200
14.4
4:56
13.5
4:39
12.1
4:14
11.3
3:58
10.7
3:46
1400
16.7
5:49
15.6
5:28
14.0
4:58
13.1
4:40
12.4
4:24
1600
18.9
6:43
17.7
6:18
15.9
5:44
14.9
5:22
14.1
5:03
1800
21.1
7:38
19.7
7:10
17.7
6:30
16.6
6:05
15.7
5:43
14
ad
ed
10
do
w
nl
o
AIR
DIST
(NM)
if
Fuel Required Adjustments (1000 KG)
U
nc
on
tro
lle
d
REFERENCE FUEL REQUIRED
(1000 KG)
2
4
6
8
10
12
14
16
18
20
22
40
-0.3
-0.7
-1.0
-1.3
-1.7
-2.0
-2.4
-2.7
-3.0
-3.4
-3.7
WEIGHT AT CHECK POINT (1000 KG)
50
60
70
-0.2
0.0
0.3
-0.3
0.0
0.6
-0.5
0.0
0.9
-0.7
0.0
1.2
-0.8
0.0
1.4
-1.0
0.0
1.6
-1.2
0.0
1.8
-1.3
0.0
2.0
-1.5
0.0
2.2
-1.7
0.0
2.4
-1.8
0.0
2.5
80
0.7
1.3
2.0
2.6
3.2
3.7
4.2
4.6
5.0
5.3
5.6
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.33.3
Performance Inflight - QRH
Gear Down
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
GEAR DOWN
Descent
VREF40 + 70 KIAS
FUEL (KG)
DISTANCE (NM)
21
20
19
19
18
17
17
16
15
14
13
13
12
11
8
6
4
280
270
270
260
260
250
250
240
230
230
220
210
200
190
170
140
110
91
86
81
77
72
68
64
60
56
52
48
44
40
36
26
16
9
U
nc
on
tro
lle
d
if
do
w
nl
o
Allowances for a straight-in approach are included.
or
pr
in
te
d
TIME (MIN)
ad
ed
PRESSURE ALTITUDE
(FT)
41000
39000
37000
35000
33000
31000
29000
27000
25000
23000
21000
19000
17000
15000
10000
5000
1500
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.33.4
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Gear Down
Category C/N Brakes
737 Flight Crew Operations Manual
GEAR DOWN
Holding
Flaps Up
30000
35000
ad
ed
or
pr
in
te
d
PRESSURE ALTITUDE (FT)
10000
15000
20000
25000
82.7
86.9
91.9
229
229
229
2220
2230
2250
81.0
85.3
89.9
224
224
224
2090
2090
2100
79.2
83.6
88.1
218
218
218
1960
1960
1960
77.5
81.8
86.2
91.7
213
213
213
213
1840
1830
1830
1860
75.8
80.0
84.4
89.1
209
209
209
209
1720
1710
1700
1720
73.9
77.9
82.3
86.9
203
203
203
203
1600
1590
1580
1580
71.8
75.8
80.2
84.7
197
197
197
197
1490
1470
1450
1450
69.4
73.6
77.8
82.3
191
191
191
191
1370
1350
1330
1320
67.0
71.2
75.3
79.8
184
184
184
184
1260
1240
1210
1200
64.5
68.5
72.8
77.1
177
177
177
177
1150
1130
1100
1080
if
do
w
nl
o
5000
78.4
229
2220
76.9
224
2100
75.3
218
1970
73.5
213
1850
71.7
209
1740
69.7
203
1620
67.6
197
1510
65.5
191
1400
63.1
184
1290
60.4
177
1170
d
1500
75.7
229
2240
74.1
224
2110
72.3
218
1990
70.6
213
1870
68.8
209
1760
66.9
203
1650
65.0
197
1530
62.7
191
1420
60.2
184
1310
57.7
177
1200
on
tro
lle
WEIGHT
(1000 KG)
%N1
85
KIAS
FF/ENG
%N1
80
KIAS
FF/ENG
%N1
75
KIAS
FF/ENG
%N1
70
KIAS
FF/ENG
%N1
65
KIAS
FF/ENG
%N1
60
KIAS
FF/ENG
%N1
55
KIAS
FF/ENG
%N1
50
KIAS
FF/ENG
%N1
45
KIAS
FF/ENG
%N1
40
KIAS
FF/ENG
94.1
203
1660
90.2
197
1490
87.0
191
1350
84.4
184
1220
81.5
177
1090
91.3
184
1260
86.6
177
1110
U
nc
This table includes 5% additional fuel for holding in a racetrack pattern.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.33.5
Performance Inflight - QRH
Gear Down
do
w
nl
o
ad
ed
or
pr
in
te
d
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
U
nc
on
tro
lle
d
if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.33.6
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Gear Down, Engine Inop
GearHighlight
file
Down, Engine Inop
Section 34
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Driftdown Speed/Level Off Altitude
or
pr
in
te
d
Gear Down, Engine Inop
Gear Down, Engine Inoperative
100 ft/min residual rate of climb
LEVEL OFF ALTITUDE (FT)
ISA + 10°C
ISA + 15°C
ISA + 20°C
& BELOW
1700
4000
2300
200
6300
4900
2800
8600
7300
5300
10900
9800
8000
13200
12300
10900
15600
14800
13900
18100
17300
16500
20600
19800
18900
23100
22300
21400
ad
ed
OPTIMUM
DRIFTDOWN
SPEED (KIAS)
227
223
218
213
208
202
196
190
183
176
do
w
nl
o
WEIGHT (1000 KG)
START
LEVEL OFF
DRIFTDOWN
85
80
80
76
75
71
70
66
65
62
60
57
55
52
50
47
45
43
40
38
Includes APU fuel burn.
Long Range Cruise Altitude Capability
100 ft/min residual rate of climb
d
PRESSURE ALTITUDE (FT)
ISA + 15°C
ISA + 20°C
2500
5900
9200
12300
15400
18300
21400
3400
6900
10600
14500
17500
20500
U
nc
on
tro
lle
75
70
65
60
55
50
45
40
ISA + 10°C & BELOW
1500
4500
7500
10600
13300
16200
19300
22200
if
WEIGHT (1000 KG)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.34.1
Performance Inflight - QRH
Gear Down, Engine Inop
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Control
96.9
.402
226
3527
93.7
.388
218
3198
91.0
.374
210
2906
88.2
.359
202
2630
85.4
.344
193
2374
82.5
.329
184
2133
96.3
.402
218
3240
92.8
.387
209
2913
89.9
.371
201
2626
86.9
.355
192
2356
83.9
.339
183
2107
if
19
21
23
or
pr
in
te
d
94.3
.389
227
3485
91.9
.375
219
3191
89.3
.362
211
2909
86.7
.348
203
2647
84.0
.334
195
2400
81.1
.320
186
2166
PRESSURE ALTITUDE (1000 FT)
11
13
15
17
ad
ed
9
95.4
.400
209
2951
91.7
.384
200
2633
88.6
.367
191
2351
85.4
.349
182
2088
do
w
nl
o
7
94.2
.398
199
2657
90.4
.380
190
2352
87.0
.361
181
2076
98.2
.412
198
2737
92.7
.393
189
2359
88.8
.374
180
2069
96.6
.408
189
2417
90.8
.387
179
2065
94.1
.402
179
2101
98.4
.418
178
2201
U
nc
on
tro
lle
5
94.8
.389
235
3774
92.6
.376
228
3477
90.2
.364
220
3192
87.8
.351
212
2924
85.3
.338
204
2672
82.7
.325
196
2432
79.8
.311
188
2206
d
WEIGHT
(1000 KG)
%N1
MACH
70
KIAS
FF/ENG
%N1
MACH
65
KIAS
FF/ENG
%N1
MACH
60
KIAS
FF/ENG
%N1
MACH
55
KIAS
FF/ENG
%N1
MACH
50
KIAS
FF/ENG
%N1
MACH
45
KIAS
FF/ENG
%N1
MACH
40
KIAS
FF/ENG
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.34.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Gear Down, Engine Inop
Category C/N Brakes
737 Flight Crew Operations Manual
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Diversion Fuel and Time
Ground to Air Miles Conversion
AIR DISTANCE (NM)
TAILWIND COMPONENT (KTS)
20
40
60
80
100
93
88
83
78
75
187
175
165
156
148
280
262
246
232
220
373
349
328
309
293
466
436
409
385
365
559
523
490
462
438
652
610
572
538
510
745
696
652
614
581
838
782
733
690
653
931
868
813
765
724
or
pr
in
te
d
GROUND
DISTANCE
(NM)
100
200
300
400
500
600
700
800
900
1000
ad
ed
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS)
100
80
60
40
20
172
151
134
120
109
352
308
270
242
219
533
465
408
364
330
716
623
545
486
440
900
783
684
609
551
1086
943
823
733
661
1273
1105
964
856
772
1462
1267
1103
980
883
1653
1431
1245
1104
994
1845
1595
1386
1228
1105
Reference Fuel and Time Required at Check Point
PRESSURE ALTITUDE (1000 FT)
10
14
FUEL
TIME
FUEL
TIME
(1000 KG)
(HR:MIN)
(1000 KG)
(HR:MIN)
1.1
0:26
1.0
0:26
2.4
0:50
2.3
0:48
3.7
1:15
3.6
1:11
4.9
1:39
4.8
1:35
6.1
2:04
6.0
1:58
7.3
2:29
7.1
2:22
8.5
2:55
8.3
2:46
9.7
3:20
9.4
3:10
10.9
3:46
10.5
3:35
12.0
4:12
11.6
3:59
do
w
nl
o
TIME
(HR:MIN)
0:27
0:53
1:18
1:44
2:10
2:37
3:03
3:30
3:58
4:25
if
FUEL
(1000 KG)
1.3
2.6
3.9
5.2
6.5
7.8
9.1
10.3
11.6
12.8
on
tro
lle
100
200
300
400
500
600
700
800
900
1000
6
d
AIR DIST
(NM)
Fuel Required Adjustments (1000 KG)
U
nc
REFERENCE FUEL REQUIRED
(1000 KG)
1
2
3
4
5
6
7
8
9
10
11
12
13
14
40
-0.2
-0.3
-0.5
-0.6
-0.8
-1.0
-1.1
-1.3
-1.5
-1.6
-1.8
-1.9
-2.1
-2.3
WEIGHT AT CHECK POINT (1000 KG)
50
60
70
-0.1
0.0
0.1
-0.2
0.0
0.3
-0.3
0.0
0.5
-0.3
0.0
0.7
-0.4
0.0
0.9
-0.5
0.0
1.0
-0.6
0.0
1.2
-0.7
0.0
1.4
-0.7
0.0
1.6
-0.8
0.0
1.8
-0.9
0.0
1.9
-1.0
0.0
2.1
-1.1
0.0
2.3
-1.1
0.0
2.5
80
0.3
0.6
1.0
1.3
1.7
2.0
2.4
2.7
3.1
3.5
3.8
4.2
4.5
4.9
Includes APU fuel burn.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.34.3
Performance Inflight - QRH
Gear Down, Engine Inop
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Holding
Flaps Up
15000
94.5
218
3890
92.4
213
3610
90.3
209
3360
88.1
203
3090
85.7
197
2840
83.2
191
2600
80.5
184
2370
77.7
177
2140
97.0
197
2990
92.6
191
2650
89.5
184
2380
86.4
177
2130
or
pr
in
te
d
PRESSURE ALTITUDE (FT)
5000
10000
95.7
209
3430
92.7
203
3130
90.2
197
2860
87.6
191
2610
84.9
184
2360
82.0
177
2120
ad
ed
do
w
nl
o
on
tro
lle
d
1500
93.2
224
4120
91.2
218
3840
89.2
213
3580
87.3
209
3340
85.1
203
3090
82.8
197
2850
80.2
191
2610
77.7
184
2390
75.0
177
2170
if
WEIGHT
(1000 KG)
%N1
80
KIAS
FF/ENG
%N1
75
KIAS
FF/ENG
%N1
70
KIAS
FF/ENG
%N1
65
KIAS
FF/ENG
%N1
60
KIAS
FF/ENG
%N1
55
KIAS
FF/ENG
%N1
50
KIAS
FF/ENG
%N1
45
KIAS
FF/ENG
%N1
40
KIAS
FF/ENG
U
nc
This table includes 5% additional fuel for holding in a racetrack pattern.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.34.4
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Text
Section 35
TextHighlight
File
Introduction
or
pr
in
te
d
This chapter contains information to supplement performance data from
the Flight Management Computer (FMC). In addition, sufficient inflight
data is provided to complete a flight with the FMC inoperative. In the event
of conflict between data presented in this chapter and that contained in the
approved Airplane Flight Manual, the Flight Manual shall always take
precedence.
General
ad
ed
Flight with Unreliable Airspeed / Turbulent Air Penetration
do
w
nl
o
Pitch attitude and average %N1 information is provided for use in all
phases of flight in the event of unreliable airspeed/Mach indications
resulting from blocking or freezing of the pitot system. Loss of radome or
turbulent air may also cause unreliable airspeed/Mach indications. The
cruise table in this section may also be used for turbulent air penetration.
Pitch attitude is shown in bold type for emphasis since altitude and/or
vertical speed indications may also be unreliable.
if
Max Climb %N1
on
tro
lle
d
This table shows Max Climb %N1 for a 280/.78 climb speed schedule,
normal engine bleed for packs on or off and anti-ice off. Enter the table
with airport pressure altitude and TAT and read %N1. %N1 adjustments are
shown for anti-ice operation.
Go-around %N1
U
nc
To find Max Go-around %N1 based on normal engine bleed for packs on
(AUTO) and anti-ice on or off, enter the Go-around %N1 table with airport
pressure altitude and reported OAT or TAT and read %N1. For packs OFF
or HIGH operation, apply the %N1 adjustment shown below the table.
VREF
This table contains flaps 40, 30 and 15 reference speeds for a given weight.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.35.1
Performance Inflight - QRH
Text
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Advisory Information
Runway Surface Condition Correlation
Normal Configuration Landing Distance
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When landing on slippery runways or runways contaminated with ice,
snow, slush, or standing water, the reported braking action must be
considered. A table is provided that correlates runway condition code to
runway surface condition description and reported braking action that can
then be used to determine the appropriate Normal Configuration Landing
Distance or Non-Normal Configuration Landing Distance.
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Tables are provided as advisory information for normal configuration
landing distances on dry runways and runways with good,
good-to-medium, medium, medium-to-poor, and poor reported braking
action. Landing distances (reference distances plus adjustments) are 115%
of the actual landing distance. The Normal Configuration Landing
Distance tables should be used enroute to make a landing distance
assessment for time of arrival.
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The reference landing distance is the distance from threshold to complete
stop. It includes an air distance allowance of 1500 ft from threshold to
touchdown. The reference distance is based on a reference landing weight
and speed at sea level, standard day, zero wind, zero slope, two-engine
detent No. 2 reverse thrust, and auto speedbrakes.
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To use these tables, determine the reference landing distance for the
selected braking configuration and reported braking action. Adjust this
reference distance for landing weight, altitude, wind, slope, temperature,
approach speed, and the number of operative thrust reversers. Each
correction is applied independently to the reference landing distance. A
correction for use of manual speedbrakes is provided in the table notes.
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Use of the autobrake system commands the airplane to a constant
deceleration rate. In some conditions, such as a runway with "poor"
reported braking action, the airplane may not be able to achieve these
deceleration rates. In these cases, runway slope and inoperative reversers
influence the stopping distance. Since it cannot be determined quickly
when this becomes a factor, it is appropriate to add the effects of slope and
inoperative reversers when using the autobrake system.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.35.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Text
Category C/N Brakes
737 Flight Crew Operations Manual
Non-normal Configuration Landing Distance
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Advisory information is provided to support non-normal configurations
that affect landing. Landing distances and adjustments are provided for dry
runways and runways with good, good-to-medium, medium,
medium-to-poor, and poor reported braking action. Landing distances
(reference distances plus adjustments) are representative of the actual
landing distance, and are not factored. The Non-Normal Configuration
Landing Distance tables should be used enroute to make a landing distance
assessment for time of arrival.
The reference landing distance is the distance from threshold to complete
stop. It includes an air distance allowance of 1500 ft from threshold to
touchdown. The reference distance is based on a reference landing weight
and speed at sea level, standard day, zero wind, zero slope, and maximum
available reverse thrust.
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Tables for Non-Normal Configuration Landing Distance in this section are
similar in format and used in the same manner as tables for the Normal
Configuration Landing Distance previously described.
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Recommended Brake Cooling Schedule
Advisory information is provided to assist in avoiding the problems
associated with hot brakes. For normal operation, most landings are at
weights below the AFM quick turnaround limit weight.
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Use of the recommended cooling schedule will help avoid brake overheat
and fuse plug problems that could result from repeated landings at short
time intervals or a rejected takeoff.
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Enter the Recommended Brake Cooling Schedule table with the airplane
weight and brakes on speed, adjusted for wind at the appropriate
temperature and altitude condition. Instructions for applying wind
adjustments are included below the table. Linear interpolation may be used
to obtain intermediate values. The resulting number is the reference brake
energy per brake in millions of foot-pounds, and represents the amount of
energy absorbed by each brake during a rejected takeoff. Notes providing
adjustments for wind are included below the table.
To determine the energy per brake absorbed during landing, enter the
appropriate Adjusted Brake Energy Per Brake table (No Reverse Thrust or
2 Engine Reverse) with the reference brake energy per brake and the type
of braking used during landing (Max Manual, Max Auto, or Autobrake).
The resulting number is the adjusted brake energy per brake and represents
the energy absorbed in each brake during the landing.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.35.3
Performance Inflight - QRH
Text
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
The recommended cooling time is found in the appropriate (steel or carbon
brakes) final table by entering with the adjusted brake energy per brake.
Times are provided for ground cooling and inflight gear down cooling.
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Brake Temperature Monitor System (BTMS) indications are also shown. If
brake cooling is determined from the BTMS, use the hottest brake
indication 10 to 15 minutes after the airplane has come to a complete stop,
or inflight with gear retracted to determine recommended cooling
schedule.
Engine Inoperative
Initial Max Continuous %N1
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Max Continuous %N1
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The Initial Max Continuous %N1 setting for use following an engine
failure is shown. The table is based on the typical all engine cruise speed
of.79M to provide a target %N1 setting at the start of driftdown. Once
driftdown is established, the Max Continuous %N1 table should be used to
determine %N1 for the given conditions.
Power setting is based on one engine operating with one A/C pack
operating and all anti-ice bleeds off. Enter the table with pressure altitude,
TAT, and IAS or Mach to read %N1.
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It is desirable to maintain engine thrust level within the limits of the Max
Cruise thrust rating. However, where thrust level in excess of Max Cruise
rating is required, such as for meeting terrain clearance, ATC altitude
assignments, or to attain maximum range capability, it is permissible to use
the thrust needed up to the Max Continuous thrust rating. The Max
Continuous thrust rating is intended primarily for emergency use at the
discretion of the pilot and is the maximum thrust that may be used
continuously.
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Driftdown Speed/Level Off Altitude
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The table shows optimum driftdown speed as a function of cruise weight
at start of driftdown. Also shown are the approximate weight and pressure
altitude at which the airplane will level off considering 100 ft/min residual
rate of climb.
The level off altitude is dependent on air temperature (ISA deviation).
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.35.4
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
FAA
Text
Category C/N Brakes
737 Flight Crew Operations Manual
Driftdown/LRC Range Capability
This table shows the range capability from the start of driftdown.
Driftdown is continued to level off altitude. As weight decreases due to
fuel burn, the airplane is accelerated to Long Range Cruise speed. Cruise
is continued at level off altitude and Long Range Cruise speed.
Long Range Cruise Altitude Capability
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To determine fuel required, enter the Ground to Air Miles Conversion table
with the desired ground distance and adjust for anticipated winds to obtain
air distance to destination. Then enter the Driftdown/Cruise Fuel and Time
table with air distance and weight at start of driftdown to determine fuel
and time required. If altitudes other than the level off altitude is used, fuel
and time required may be obtained by using the Engine Inoperative Long
Range Cruise Enroute Fuel and Time table.
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Long Range Cruise Control
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The table shows the maximum altitude that can be maintained at a given
weight and air temperature (ISA deviation), based on Long Range Cruise
speed, Max Continuous thrust, and 100 ft/min residual rate of climb.
The table provides target %N1, engine inoperative Long Range Cruise
Mach number, IAS and fuel flow for the airplane weight and pressure
altitude. The fuel flow values in this table reflect single engine fuel burn.
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APU Operation During Flight
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For APU operation during flight, increase fuel flow according to the
following table. These increments include the APU fuel flow and the effect
of increased drag from the APU door.
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PRESSURE ALTITUDE (1000 FT)
39
35
31
25
20
15
10
5
APU FUEL FLOW (KG/HR)
45
45
50
60
65
75
85
95
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.35.5
Performance Inflight - QRH
Text
737-800WSFP1/CFM56-7B26
FAA
Category C/N Brakes
737 Flight Crew Operations Manual
Long Range Cruise Diversion Fuel and Time
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Tables are provided for crews to determine the fuel and time required to
proceed to an alternate airfield with one engine inoperative. The data is
based on single engine Long Range Cruise speed and .78/280/250 descent.
Enter with Air Distance as determined from the Ground to Air Miles
Conversion table and read Fuel and Time required at the cruise pressure
altitude. Adjust the fuel obtained for deviation from the reference weight
at checkpoint as required by entering the off reference fuel adjustments
table with the fuel required for the reference weight and the actual weight
at checkpoint. Read fuel required and time for the actual weight.
Holding
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Target %N1, indicated airspeed and fuel flow per engine information is
tabulated for holding with flaps up based on the FMC optimum holding
speed schedule. This is the higher of the maximum endurance speed and
the maneuvering speed. Small variations in airspeed will not appreciably
affect the overall endurance time. Enter the table with weight and pressure
altitude to read %N1, IAS and fuel flow per engine.
Gear Down Landing Rate of Climb Available
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Rate of climb data is provided as guidance information in the event an
engine inoperative landing (manual or autoland) is planned. The tables
show gear down rate of climb available for Flaps 15 and Flaps 30. Enter
the table with TAT and pressure altitude to read rate of climb available.
Apply adjustments shown to correct for weight.
Gear Down
This section contains performance for airplane operation with the landing
gear extended. The data is based on engine bleeds for normal air
conditioning.
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Note: The Flight Management Computer System (FMCS) does not
contain special provisions for operation with landing gear extended.
As a result, the FMCS may generate inappropriate enroute speed
schedules, display non-conservative predictions of fuel burn,
estimated time of arrival (ETA), maximum altitude, and compute
overly shallow descent path. An accurate estimated time of arrival
(ETA) is available if current speed or Mach is entered into the
VNAV cruise page.
Tables for gear down performance in this section are identical in format
and used in the same manner as tables for the gear up configuration
previously described.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.35.6
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1
Section
737-800WSFP1
CFM56-7B26
CFM56-7B26
C M KGCJAA
M KG
CATC/N
JAA CATC/N
TALPA TALPA
(FMC Model
(FMC737-800W.1)
Model 737-800W.1)
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Table of Contents
Section 40
737-800WSFP1 CFM56-7B26 C M KG JAA CATC/N TALPA (FMC
Model 737-800W.1)
Pkg Model Identification . . . . . . . . . . . . . . . . . . . PI-QRH.ModID.40.1
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General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.40.1
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Flight With Unreliable Airspeed/
Turbulent Air Penetration . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.40.1
CLIMB (280/.76) . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.40.1
CRUISE (.76/280) . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.40.1
DESCENT (.76/280) . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.40.2
HOLDING (VREF40 + 70). . . . . . . . . . . . . . . . . . . PI-QRH.40.2
TERMINAL AREA (5000 FT) . . . . . . . . . . . . . . . . PI-QRH.40.3
Airport Altitude = -2000 FT . . . . . . . . . . . . . . . . PI-QRH.40.3
Airport Altitude = -1000 FT . . . . . . . . . . . . . . . . PI-QRH.40.4
Airport Altitude = SEA LEVEL . . . . . . . . . . . . . PI-QRH.40.5
Airport Altitude = 1000 FT . . . . . . . . . . . . . . . . PI-QRH.40.6
Airport Altitude = 2000 FT . . . . . . . . . . . . . . . . PI-QRH.40.7
Airport Altitude = 3000 FT . . . . . . . . . . . . . . . . PI-QRH.40.8
Airport Altitude = 4000 FT . . . . . . . . . . . . . . . . PI-QRH.40.9
Airport Altitude = 5000 FT . . . . . . . . . . . . . . . PI-QRH.40.10
Airport Altitude = 6000 FT . . . . . . . . . . . . . . . .PI-QRH.40.11
Airport Altitude = 7000 FT . . . . . . . . . . . . . . . PI-QRH.40.12
Airport Altitude = 8000 FT . . . . . . . . . . . . . . . PI-QRH.40.13
Airport Altitude = 9000 FT . . . . . . . . . . . . . . . PI-QRH.40.14
Airport Altitude = 10000 FT . . . . . . . . . . . . . . PI-QRH.40.15
Airport Altitude = 11000 FT. . . . . . . . . . . . . . . PI-QRH.40.16
Airport Altitude = 12000 FT . . . . . . . . . . . . . . PI-QRH.40.17
Airport Altitude = 13000 FT . . . . . . . . . . . . . . PI-QRH.40.18
Airport Altitude = 14000 FT . . . . . . . . . . . . . . PI-QRH.40.19
Airport Altitude = 14500 FT . . . . . . . . . . . . . . PI-QRH.40.20
FINAL APPROACH (1500 FT) . . . . . . . . . . . . . . PI-QRH.40.21
Airport Altitude = -2000 FT . . . . . . . . . . . . . . . PI-QRH.40.21
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
4
D6-27370-8AS-NOK
PI-QRH.TOC.40.1
Performance Inflight - QRH Table of Contents
737 Flight Crew Operations Manual
PI-QRH.40.21
PI-QRH.40.22
PI-QRH.40.22
PI-QRH.40.23
PI-QRH.40.23
PI-QRH.40.24
PI-QRH.40.24
PI-QRH.40.25
PI-QRH.40.25
PI-QRH.40.26
PI-QRH.40.26
PI-QRH.40.27
PI-QRH.40.27
PI-QRH.40.28
PI-QRH.40.28
PI-QRH.40.29
PI-QRH.40.29
PI-QRH.40.30
PI-QRH.40.31
PI-QRH.40.32
PI-QRH.40.33
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Airport Altitude = -1000 FT . . . . . . . . . . . . . . .
Airport Altitude = SEA LEVEL . . . . . . . . . . . .
Airport Altitude = 1000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 2000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 3000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 4000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 5000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 6000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 7000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 8000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 9000 FT. . . . . . . . . . . . . . . .
Airport Altitude = 10000 FT. . . . . . . . . . . . . . .
Airport Altitude = 11000 FT. . . . . . . . . . . . . . .
Airport Altitude = 12000 FT. . . . . . . . . . . . . . .
Airport Altitude = 13000 FT. . . . . . . . . . . . . . .
Airport Altitude = 14000 FT. . . . . . . . . . . . . . .
Airport Altitude = 14500 FT. . . . . . . . . . . . . . .
GO-AROUND . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Max Climb %N1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Go-around %N1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
VREF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Advisory Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.41.1
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Runway Surface Condition Correlation . . . . . . . . . . . . PI-QRH.41.1
Normal Configuration Landing Distance . . . . . . . . . . . PI-QRH.41.2
Non-Normal Configuration Landing Distance . . . . . . . PI-QRH.41.6
Airspeed Unreliable (Flaps 15) . . . . . . . . . . . . . . . . PI-QRH.41.6
Airspeed Unreliable (Flaps 30) . . . . . . . . . . . . . . . . PI-QRH.41.7
Airspeed Unreliable (Flaps 40) . . . . . . . . . . . . . . . . PI-QRH.41.8
All Flaps Up Landing. . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.41.9
ANTISKID INOPERATIVE (Flaps 15) . . . . . . . . PI-QRH.41.10
ANTISKID INOPERATIVE (Flaps 30) . . . . . . . . PI-QRH.41.11
ANTISKID INOPERATIVE (Flaps 40) . . . . . . . . PI-QRH.41.12
Jammed or Restricted Flight Controls (Flaps 15) . PI-QRH.41.13
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.TOC.40.2
D6-27370-8AS-NOK
September 30, 2022
Performance Inflight - QRH Table of Contents
737 Flight Crew Operations Manual
PI-QRH.41.14
PI-QRH.41.15
PI-QRH.41.16
PI-QRH.41.17
PI-QRH.41.18
PI-QRH.41.19
PI-QRH.41.20
PI-QRH.41.21
PI-QRH.41.22
PI-QRH.41.23
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LEADING EDGE FLAPS TRANSIT (Flaps 15) .
LOSS OF SYSTEM A (Flaps 15) . . . . . . . . . . . . .
LOSS OF SYSTEM A (Flaps 30) . . . . . . . . . . . . .
LOSS OF SYSTEM A (Flaps 40) . . . . . . . . . . . . .
LOSS OF SYSTEM A AND SYSTEM B
(Flaps 15). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
LOSS OF SYSTEM B (Flaps 15) . . . . . . . . . . . . .
MANUAL REVERSION (Flaps 15). . . . . . . . . . .
One Engine Inoperative Landing (Flaps 15) . . . . .
One Engine Inoperative Landing (Flaps 30) . . . . .
Stabilizer Trim Inoperative (Flaps 15) . . . . . . . . .
Trailing Edge Flap Asymmetry (1 ≤ Flap
Lever <15) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flap Asymmetry (Flap Lever
15 or 25) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flap Asymmetry (Flap Lever 30) . .
Trailing Edge Flap Disagree (1 ≤ Indicated
Flaps <15) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flap Disagree (15 ≤ Indicated
Flaps <30) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flap Disagree (30 ≤ Indicated
Flaps <40) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Trailing Edge Flaps Up Landing . . . . . . . . . . . . . .
Recommended Brake Cooling Schedule . . . . . . . . . .
PI-QRH.41.24
PI-QRH.41.25
PI-QRH.41.26
PI-QRH.41.27
PI-QRH.41.28
PI-QRH.41.29
PI-QRH.41.30
PI-QRH.41.31
Engine Inoperative . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.42.1
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Initial Max Continuous %N1 . . . . . . . . . . . . . . . . . . . . PI-QRH.42.1
Max Continuous %N1 . . . . . . . . . . . . . . . . . . . . . . . . . PI-QRH.42.2
Driftdown Speed/Level Off Altitude . . . . . . . . . . . . . . PI-QRH.42.6
Driftdown/LRC Cruise Range Capability . . . . . . . . . . PI-QRH.42.7
Long Range Cruise Altitude Capability . . . . . . . . . . . . PI-QRH.42.8
Long Range Cruise Control . . . . . . . . . . . . . . . . . . . . . PI-QRH.42.9
Long Range Cruise Diversion Fuel and Time . . . . . . PI-QRH.42.10
Holding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.42.11
Gear Down Landing Rate of Climb Available . . . . . . PI-QRH.42.12
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.TOC.40.3
Performance Inflight - QRH Table of Contents
737 Flight Crew Operations Manual
Gear Down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.43.1
PI-QRH.43.1
PI-QRH.43.2
PI-QRH.43.3
PI-QRH.43.4
PI-QRH.43.5
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Long Range Cruise Altitude Capability . . . . . . . . . . . .
Long Range Cruise Control . . . . . . . . . . . . . . . . . . . . .
Long Range Cruise Enroute Fuel and Time . . . . . . . . .
Descent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Holding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Gear Down, Engine Inoperative . . . . . . . . . . . . . . . . . . . .PI-QRH.44.1
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Driftdown Speed/Level Off Altitude. . . . . . . . . . . . . . .
Long Range Cruise Altitude Capability . . . . . . . . . . . .
Long Range Cruise Control . . . . . . . . . . . . . . . . . . . . .
Long Range Cruise Diversion Fuel and Time. . . . . . . .
Holding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
PI-QRH.44.1
PI-QRH.44.1
PI-QRH.44.2
PI-QRH.44.3
PI-QRH.44.4
Text. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PI-QRH.45.1
PI-QRH.45.1
PI-QRH.45.1
PI-QRH.45.2
PI-QRH.45.4
PI-QRH.45.6
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Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Advisory Information . . . . . . . . . . . . . . . . . . . . . . . . . .
Engine Inoperative . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Gear Down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.TOC.40.4
D6-27370-8AS-NOK
September 30, 2022
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Pkg Model Identification
Section 40
Pkg Model Identification
File Model
Pkg
highlight
Identification
General
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The table below shows the airplanes that have been identified with the following
performance package. Note, some airplanes may be identified with more than one
performance package. This configuration table information reflects the Boeing
delivered configuration updated for service bulletin incorporations in
conformance with the policy stated in the introduction section of the FCOM. The
performance data is prepared for the owner/operator named on the title page. The
intent of this information is to assist flight crews and airlines in knowing which
performance package is applicable to a given airplane. The performance package
model identification information is based on Boeing's knowledge of the airline's
fleet at a point in time approximately three months prior to the page date. Notice
of Errata (NOE) will not be provided to airlines to identify airplanes that are
moved between performance packages within this manual or airplanes added to
the airline's fleet whose performance packages are already represented in this
manual. These types of changes will be updated in the next block revision.
Owners/operators are responsible for ensuring the operational documentation they
are using is complete and matches the current configuration of their airplanes, and
the accuracy and validity of all information furnished by the owner/operator or
any other party. Owners/operators receiving active revision service are
responsible to ensure that any modifications to the listed airplanes are properly
reflected in this manual.
d
Serial and tabulation number are supplied by Boeing.
Serial Number
Tabulation
Number
HS-DBG
35094
YL061
U
nc
on
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Registry Number
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September 30, 2022
2
D6-27370-8AS-NOK
PI-QRH.ModID.40.1
Performance Inflight - QRH Pkg Model Identification
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ed
or
pr
in
te
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737 Flight Crew Operations Manual
U
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if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.ModID.40.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
General
Section 40
General
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
file Highlight
General
40
2.0
82.9
1.0
81.2
1.0
80.7
1.0
77.2
1.0
73.6
1.0
69.8
or
pr
in
te
d
CRUISE (.76/280)
Flaps Up, %N1 for Level Flight
PRESSURE
ALTITUDE (FT)
PITCH ATT
40000
%N1
PITCH ATT
35000
%N1
PITCH ATT
30000
%N1
PITCH ATT
25000
%N1
PITCH ATT
20000
%N1
PITCH ATT
15000
%N1
WEIGHT (1000 KG)
50
60
70
4.0
4.0
1100
600
4.0
3.5
4.0
1900
1500
1100
6.5
6.0
6.0
3300
2600
2100
9.5
8.5
8.0
4400
3600
3000
12.5
11.0
10.0
5300
4400
3700
ad
ed
40
4.0
1700
4.0
2500
7.0
4200
11.0
5600
14.5
6700
U
nc
on
tro
lle
d
if
do
w
nl
o
CLIMB (280/.76)
Flaps Up, Set Max Climb Thrust
PRESSURE
ALTITUDE (FT)
PITCH ATT
40000
V/S (FT/MIN)
PITCH ATT
30000
V/S (FT/MIN)
PITCH ATT
20000
V/S (FT/MIN)
PITCH ATT
10000
V/S (FT/MIN)
SEA
PITCH ATT
V/S (FT/MIN)
LEVEL
WEIGHT (1000 KG)
50
60
70
2.5
3.5
85.4
88.9
2.0
2.5
3.0
82.6
84.4
86.8
1.5
2.0
2.5
81.5
82.7
84.2
1.5
2.0
2.5
77.9
79.0
80.5
1.5
2.0
2.5
74.2
75.3
76.6
1.5
2.0
3.0
70.6
71.6
72.9
80
4.0
800
6.0
1700
8.0
2500
9.5
3100
80
3.5
90.4
3.0
86.1
3.0
82.3
3.5
78.2
3.5
74.4
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.1
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
do
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o
HOLDING (VREF40 + 70)
Flaps Up, %N1 for Level Flight
PRESSURE ALTITUDE (FT)
PITCH ATT
%N1
KIAS
PITCH ATT
%N1
KIAS
PITCH ATT
%N1
KIAS
40
5.0
56
177
5.0
52
177
5.0
49
177
if
15000
on
tro
lle
d
10000
80
1.5
-2700
0.5
-2000
0.5
-1700
0.5
-1500
0.5
-1400
WEIGHT (1000 KG)
50
60
70
5.0
5.0
5.0
62
66
70
193
212
229
5.0
5.0
5.0
58
62
66
192
211
228
5.5
5.0
5.0
54
58
62
191
210
227
80
5.0
73
246
5.0
69
244
5.0
66
243
U
nc
5000
WEIGHT (1000 KG)
50
60
70
-0.5
0.5
1.0
-2400
-2300
-2500
-2.0
-1.0
-0.5
-2600
-2300
-2100
-2.0
-1.0
0.0
-2300
-2000
-1900
-2.0
-1.0
0.0
-2100
-1800
-1700
-2.5
-1.0
-0.5
-1900
-1700
-1500
or
pr
in
te
d
40
-1.5
-2700
-3.5
-3100
-3.5
-2800
-3.5
-2500
-3.5
-2300
ad
ed
DESCENT (.76/280)
Flaps Up, Set Idle Thrust
PRESSURE
ALTITUDE (FT)
PITCH ATT
40000
V/S (FT/MIN)
PITCH ATT
30000
V/S (FT/MIN)
PITCH ATT
20000
V/S (FT/MIN)
PITCH ATT
10000
V/S (FT/MIN)
SEA
PITCH ATT
V/S (FT/MIN)
LEVEL
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = -2000 FT
if
d
or
pr
in
te
d
80
6.0
63.6
223
6.0
65.8
203
6.5
66.7
183
5.5
68.0
183
6.0
69.0
173
6.5
70.6
163
6.0
74.1
173
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
52.2 56.3 60.0
191
203
213
5.0
5.5
6.0
54.3 58.5 62.3
171
183
193
5.5
6.0
6.5
54.4 58.9 63.1
151
163
173
4.5
5.0
5.5
55.6 60.2 64.4
151
163
173
5.0
5.5
5.5
56.3 61.1 65.3
141
153
163
6.0
6.0
6.5
57.6 62.5 66.8
131
143
153
5.5
5.5
6.0
61.2 66.1 70.2
141
153
163
ad
ed
40
4.5
47.5
177
5.0
49.6
157
5.5
49.3
137
4.5
50.4
137
5.0
50.9
127
6.0
52.1
117
5.0
55.5
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.3
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = -1000 FT
if
d
U
nc
on
tro
lle
80
6.5
64.4
223
6.0
66.5
203
6.5
67.5
183
5.5
68.8
183
6.0
69.8
173
6.5
71.5
163
6.0
74.9
173
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
52.9 57.0 60.8
191
203
213
5.0
5.5
6.0
55.1 59.3 63.1
171
183
193
5.5
6.0
6.5
55.2 59.7 63.9
151
163
173
4.5
5.0
5.5
56.3 61.0 65.2
151
163
173
5.0
5.5
5.5
57.0 61.9 66.1
141
153
163
6.0
6.0
6.5
58.4 63.3 67.6
131
143
153
5.5
5.5
6.0
62.0 66.9 71.0
141
153
163
ad
ed
40
4.5
48.2
177
5.0
50.2
157
5.5
49.9
137
4.5
51.1
137
5.0
51.6
127
6.0
52.8
117
5.0
56.2
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.4
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = SEA LEVEL
if
d
or
pr
in
te
d
80
6.5
65.2
223
6.0
67.3
203
6.5
68.3
183
5.5
69.6
183
6.0
70.6
173
6.5
72.4
163
6.0
75.8
173
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
53.5 57.7 61.6
191
203
213
5.0
5.5
6.0
55.8 60.0 63.9
171
183
193
5.5
6.0
6.5
55.9 60.5 64.7
151
163
173
4.5
5.0
5.5
57.1 61.9 66.0
151
163
173
5.5
5.5
5.5
57.8 62.7 66.9
141
153
163
6.0
6.0
6.5
59.2 64.2 68.4
131
143
153
5.5
5.5
6.0
62.8 67.7 71.9
141
153
163
ad
ed
40
4.5
48.9
177
5.0
50.9
157
5.5
50.6
137
4.5
51.8
137
5.0
52.3
127
6.0
53.5
117
5.0
57.0
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.5
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 1000 FT
if
d
U
nc
on
tro
lle
80
6.5
66.0
223
6.0
68.0
203
6.5
69.1
183
5.5
70.4
183
6.0
71.5
173
6.5
73.2
163
6.0
76.6
173
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
54.3 58.4 62.4
191
203
213
5.0
5.5
6.0
56.5 60.8 64.7
171
183
193
5.5
6.0
6.5
56.6 61.3 65.5
151
163
173
4.5
5.0
5.5
57.9 62.7 66.8
151
163
173
5.5
5.5
5.5
58.6 63.5 67.7
141
153
163
6.0
6.0
6.5
60.0 65.0 69.2
131
143
153
5.5
5.5
6.0
63.6 68.5 72.8
141
153
163
ad
ed
40
4.5
49.7
177
5.0
51.6
157
5.5
51.4
137
4.5
52.6
137
5.0
53.0
127
6.0
54.3
117
5.0
57.7
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.6
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 2000 FT
if
d
or
pr
in
te
d
80
6.5
66.7
223
6.0
68.8
203
6.5
69.9
183
5.5
71.3
183
6.0
72.4
173
6.5
74.1
163
6.0
77.4
173
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
55.0 59.2 63.3
191
203
213
5.0
5.5
6.0
57.3 61.7 65.4
171
183
193
5.5
6.0
6.5
57.4 62.2 66.3
151
163
173
4.5
5.0
5.5
58.6 63.5 67.6
151
163
173
5.5
5.5
5.5
59.4 64.3 68.5
141
153
163
6.0
6.0
6.5
60.8 65.8 70.1
131
143
153
5.5
5.5
6.0
64.4 69.3 73.6
141
153
163
ad
ed
40
4.5
50.4
177
5.0
52.3
157
5.5
52.1
137
4.5
53.3
137
5.0
53.7
127
6.0
55.0
117
5.0
58.5
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.7
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 3000 FT
if
d
U
nc
on
tro
lle
80
6.5
67.4
223
6.0
69.6
203
6.5
70.7
183
5.5
72.1
183
6.0
73.3
173
6.5
74.9
163
6.0
78.2
173
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
55.8 60.0 64.1
191
203
213
5.0
5.5
6.0
58.0 62.5 66.2
171
183
193
5.5
6.0
6.5
58.2 63.0 67.1
151
163
173
4.5
5.0
5.5
59.5 64.3 68.4
151
163
173
5.5
5.5
5.5
60.2 65.2 69.4
141
153
163
6.0
6.0
6.5
61.6 66.5 71.0
131
143
153
5.5
5.5
6.0
65.2 70.2 74.5
141
153
163
ad
ed
40
4.5
51.0
177
5.0
53.1
157
5.5
52.9
137
4.5
54.0
137
5.0
54.5
127
6.0
55.8
117
5.0
59.3
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.8
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 4000 FT
if
d
or
pr
in
te
d
80
6.5
68.2
223
6.0
70.5
203
6.5
71.6
183
5.5
73.0
183
6.0
74.1
173
6.5
75.7
163
6.0
79.1
173
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
56.4 60.8 64.9
191
203
213
5.0
5.5
6.0
58.8 63.3 66.9
171
183
193
5.5
6.0
6.5
59.0 63.8 67.9
151
163
173
4.5
5.0
5.5
60.3 65.1 69.2
151
163
173
5.5
5.5
5.5
61.1 66.0 70.2
141
153
163
6.0
6.0
6.5
62.4 67.4 71.9
131
143
153
5.5
5.5
6.0
66.0 71.1 75.3
141
153
163
ad
ed
40
4.5
51.7
177
5.0
53.9
157
5.5
53.6
137
4.5
54.7
137
5.0
55.2
127
6.0
56.5
117
5.0
60.1
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.9
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 5000 FT
if
d
U
nc
on
tro
lle
80
6.5
69.0
224
6.0
71.4
204
6.5
72.5
184
5.5
73.8
184
6.0
74.9
174
6.5
76.5
164
6.0
80.0
174
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
57.2 61.6 65.6
191
203
213
5.0
5.5
6.0
59.6 64.1 67.7
171
183
193
5.5
6.0
6.5
59.8 64.6 68.7
151
163
173
4.5
5.0
5.5
61.1 65.9 70.0
151
163
173
5.5
5.5
5.5
61.9 66.7 71.1
141
153
163
6.0
6.0
6.5
63.3 68.2 72.7
131
143
153
5.5
5.5
6.0
66.8 71.9 76.1
141
153
163
ad
ed
40
4.5
52.4
177
5.0
54.6
157
5.5
54.3
137
4.5
55.5
137
5.0
56.0
127
6.0
57.3
117
5.0
61.0
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.10
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 6000 FT
if
d
or
pr
in
te
d
80
6.5
69.8
224
6.0
72.2
204
6.5
73.3
184
5.5
74.6
184
6.0
75.7
174
6.5
77.3
164
6.0
80.9
174
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
57.9 62.5 66.3
191
203
213
5.0
5.5
6.0
60.4 64.8 68.5
171
183
193
5.5
6.0
6.5
60.7 65.4 69.5
151
163
173
4.5
5.0
5.5
62.0 66.7 70.9
151
163
173
5.5
5.5
5.5
62.7 67.6 72.0
141
153
163
6.0
6.0
6.5
64.1 69.0 73.6
131
143
153
5.5
5.5
6.0
67.6 72.8 77.0
141
153
163
ad
ed
40
4.5
53.1
177
5.0
55.3
157
5.5
55.1
137
4.5
56.2
137
5.0
56.7
127
6.0
58.1
117
5.0
61.8
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.11
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 7000 FT
if
d
U
nc
on
tro
lle
80
6.5
70.6
224
6.0
73.1
204
6.5
74.1
184
5.5
75.4
184
6.0
76.5
174
6.5
78.2
164
6.0
81.8
174
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
58.7 63.3 67.1
191
203
213
5.0
5.5
6.0
61.3 65.6 69.4
171
183
193
5.5
6.0
6.5
61.5 66.2 70.4
151
163
173
4.5
5.0
5.5
62.8 67.5 71.8
151
163
173
5.5
5.5
5.5
63.5 68.4 72.8
141
153
163
6.0
6.0
6.5
64.9 69.9 74.4
131
143
153
5.5
5.5
6.0
68.5 73.7 77.8
141
153
163
ad
ed
40
4.5
53.8
177
5.0
56.1
157
5.5
55.8
137
4.5
57.0
137
5.0
57.6
127
6.0
58.9
117
5.0
62.6
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.12
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 8000 FT
if
d
or
pr
in
te
d
80
6.0
71.4
225
6.0
73.9
205
6.5
74.9
185
5.5
76.2
185
6.0
77.3
175
6.5
79.1
165
6.0
82.7
175
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
59.5 64.1 67.8
191
203
214
5.0
5.5
6.0
62.1 66.4 70.3
171
183
194
5.5
6.0
6.5
62.4 67.0 71.2
151
163
174
4.5
5.0
5.5
63.6 68.3 72.6
151
163
174
5.5
5.5
5.5
64.3 69.3 73.7
141
153
164
6.0
6.0
6.5
65.7 70.8 75.2
131
143
154
5.5
5.5
6.0
69.4 74.5 78.7
141
153
164
ad
ed
40
4.5
54.5
177
5.0
56.8
157
5.5
56.6
137
4.5
57.8
137
5.0
58.4
127
6.0
59.8
117
5.0
63.5
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.13
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 9000 FT
if
d
U
nc
on
tro
lle
80
6.0
72.2
225
6.0
74.7
205
6.5
75.7
185
5.5
77.1
185
5.5
78.2
175
6.5
80.0
165
6.0
83.6
175
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
60.4 64.9 68.6
191
204
214
5.0
5.5
6.0
62.9 67.2 71.1
171
184
194
5.5
6.0
6.5
63.1 67.8 72.1
151
164
174
4.5
5.0
5.5
64.4 69.2 73.4
151
164
174
5.5
5.5
5.5
65.1 70.2 74.5
141
154
164
6.0
6.0
6.5
66.5 71.7 76.1
131
144
154
5.5
5.5
6.0
70.3 75.3 79.6
141
154
164
ad
ed
40
4.5
55.3
177
5.0
57.6
157
5.5
57.4
137
4.5
58.7
137
5.0
59.2
127
6.0
60.6
117
5.0
64.3
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.14
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 10000 FT
if
d
or
pr
in
te
d
80
6.0
73.0
225
6.0
75.5
205
6.5
76.6
185
5.5
78.0
185
5.5
79.1
175
6.0
80.8
165
6.0
84.5
175
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
61.2 65.6 69.4
191
204
214
5.0
5.5
6.0
63.7 68.0 72.0
171
184
194
5.5
6.0
6.0
64.0 68.7 72.9
151
164
174
4.5
5.0
5.0
65.3 70.1 74.3
151
164
174
5.0
5.5
5.5
65.9 71.1 75.3
141
154
164
6.0
6.0
6.5
67.4 72.6 76.9
131
144
154
5.5
5.5
6.0
71.2 76.2 80.6
141
154
164
ad
ed
40
4.5
56.0
177
5.0
58.4
157
5.5
58.2
137
4.5
59.5
137
5.0
60.1
127
6.0
61.4
117
5.0
65.0
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.15
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 11000 FT
if
d
U
nc
on
tro
lle
80
6.0
73.8
226
6.0
76.3
206
6.5
77.5
186
5.5
79.0
186
5.5
80.1
176
6.0
81.8
166
6.0
85.5
176
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
62.2 66.3 70.3
191
204
215
5.0
5.5
6.0
64.5 69.0 73.0
171
184
195
5.5
6.0
6.0
64.9 69.7 73.8
151
164
175
4.5
5.0
5.0
66.2 71.1 75.1
151
164
175
5.0
5.5
5.5
67.0 72.1 76.2
141
154
165
6.0
6.0
6.5
68.5 73.6 78.0
131
144
155
5.5
5.5
6.0
72.2 77.2 81.6
141
154
165
ad
ed
40
4.5
56.8
177
5.0
59.4
157
5.5
59.4
137
4.5
60.7
137
5.0
61.2
127
6.0
62.6
117
5.0
66.1
127
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.16
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 12000 FT
if
d
or
pr
in
te
d
80
6.0
74.6
226
6.0
77.2
206
6.5
78.5
186
5.5
79.9
186
5.5
81.1
176
6.0
82.8
166
5.5
86.6
176
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
63.0 67.1 71.2
191
204
215
5.0
5.5
6.0
65.3 69.9 73.7
171
184
195
5.5
6.0
6.0
65.8 70.6 74.7
151
164
175
4.5
5.0
5.0
67.1 72.0 76.0
151
164
175
5.0
5.5
5.5
68.0 73.0 77.2
141
154
165
6.0
6.0
6.0
69.7 74.5 78.9
131
144
155
5.5
5.5
5.5
73.2 78.3 82.6
141
154
165
ad
ed
40
4.5
57.6
178
5.0
60.4
158
5.5
60.4
138
4.5
61.7
138
5.0
62.2
128
6.0
63.6
118
5.0
67.3
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.17
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 13000 FT
if
d
U
nc
on
tro
lle
80
6.0
75.4
227
6.0
78.1
207
6.0
79.4
187
5.0
80.8
187
5.5
82.0
177
6.0
83.7
167
5.5
87.6
177
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
63.7 67.9 72.0
192
205
215
5.0
5.5
6.0
66.2 70.8 74.5
172
185
195
5.5
6.0
6.0
66.7 71.6 75.6
152
165
175
4.5
5.0
5.0
68.1 72.9 77.0
152
165
175
5.0
5.5
5.5
69.1 73.9 78.2
142
155
165
6.0
6.0
6.0
70.7 75.4 79.9
132
145
155
5.5
5.5
5.5
74.2 79.3 83.6
142
155
165
ad
ed
40
4.5
58.5
178
5.0
61.3
158
5.5
61.4
138
4.5
62.6
138
5.0
63.2
128
6.0
64.7
118
5.0
68.4
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.18
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 14000 FT
if
d
or
pr
in
te
d
80
6.0
76.3
227
6.0
79.0
207
6.0
80.3
187
5.5
81.7
187
5.5
82.9
177
6.0
84.7
167
5.5
88.6
177
U
nc
on
tro
lle
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
64.4 68.7 72.8
192
205
215
5.0
5.5
6.0
67.1 71.6 75.3
172
185
195
5.5
6.0
6.0
67.7 72.4 76.5
152
165
175
4.5
5.0
5.0
69.1 73.7 77.9
152
165
175
5.0
5.5
5.5
70.1 74.8 79.1
142
155
165
6.0
6.0
6.0
71.7 76.5 80.9
132
145
155
5.5
5.5
5.5
75.1 80.2 84.5
142
155
165
ad
ed
40
4.5
59.4
178
5.0
62.2
158
5.5
62.3
138
4.5
63.5
138
5.0
64.1
128
6.0
65.8
118
5.0
69.5
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.19
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
TERMINAL AREA (5000 FT)
%N1 for Level Flight
Airport Altitude = 14500 FT
if
d
U
nc
on
tro
lle
80
6.0
76.7
227
6.0
79.4
207
6.0
80.7
187
5.0
82.1
187
5.5
83.4
177
6.0
85.2
167
5.5
89.2
177
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
5.0
5.5
6.0
64.8 69.2 73.2
192
205
216
5.0
5.5
6.0
67.5 72.1 75.8
172
185
196
5.5
6.0
6.0
68.2 72.9 76.9
152
165
176
4.5
5.0
5.0
69.6 74.2 78.4
152
165
176
5.0
5.5
5.5
70.6 75.2 79.6
142
155
166
6.0
6.0
6.0
72.1 77.0 81.4
132
145
156
5.5
5.5
5.5
75.6 80.7 85.0
142
155
166
ad
ed
40
4.5
59.8
178
5.0
62.6
158
5.5
62.7
138
4.5
63.9
138
5.0
64.6
128
6.0
66.3
118
5.0
70.1
128
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
FLAPS UP
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+70
FLAPS 1
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+50
FLAPS 5
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 10
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+30
FLAPS 15
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+20
FLAPS 25
PITCH ATT
%N1
(GEAR UP)
KIAS
VREF40+10
FLAPS 15
PITCH ATT
%N1
(GEAR DOWN)
KIAS
VREF40+20
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.20
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = -2000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = -1000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
43.0 46.7
49.9
143
156
167
1.0
1.0
1.5
50.8 55.1
58.6
138
150
161
0.0
0.5
0.5
55.9 60.6
64.4
130
143
153
80
2.5
52.8
178
1.5
62.0
171
0.5
67.9
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
43.6 47.3
50.5
143
156
167
1.0
1.0
1.5
51.5 55.8
59.3
138
150
161
0.0
0.5
0.5
56.6 61.3
65.2
130
143
153
80
2.5
53.5
178
1.5
62.8
171
0.5
68.7
163
or
pr
in
te
d
40
2.0
38.9
128
1.0
46.1
124
0.0
50.5
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
39.5
128
1.0
46.7
124
0.0
51.2
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.21
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = SEA LEVEL
Flap placard speed exceeded in shaded area.
Airport Altitude = 1000 FT
80
2.5
54.2
178
1.5
63.6
171
0.5
69.5
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
44.7
48.7
51.8
143
156
167
1.0
1.0
1.5
52.9
57.2
60.9
138
150
161
0.0
0.5
0.5
58.1 62.9
66.8
131
143
153
80
2.5
54.9
178
1.5
64.4
171
0.5
70.3
163
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
44.1 48.0
51.1
143
156
167
1.0
1.0
1.5
52.2
56.5
60.1
138
150
161
0.0
0.5
0.5
57.3 62.1
66.1
131
143
153
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
40.2
128
1.0
47.3
124
0.0
51.9
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
40.7
128
1.0
47.9
124
0.0
52.6
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.22
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 2000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 3000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
45.4 49.3
52.5
143
156
167
1.0
1.0
1.5
53.6 58.0
61.7
138
150
161
0.0
0.5
0.5
58.9 63.7
67.5
131
143
153
80
2.5
55.6
178
1.5
65.1
171
0.5
71.1
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
46.0 49.9
53.2
143
156
167
1.0
1.0
1.5
54.3 58.7
62.5
138
150
161
0.0
0.5
0.5
59.6 64.5
68.3
131
143
153
80
2.5
56.3
178
1.5
65.9
171
0.5
72.0
163
or
pr
in
te
d
40
2.0
41.2
128
1.0
48.6
124
0.0
53.3
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
41.7
128
1.0
49.2
124
0.0
54.1
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.23
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 4000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 5000 FT
80
2.5
57.0
178
1.5
66.7
171
0.5
72.8
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
47.3
51.2
54.6
143
157
167
1.0
1.0
1.5
55.7
60.3
64.0
138
151
161
0.0
0.5
0.5
61.2 66.1
69.9
131
143
153
80
2.5
57.7
178
1.5
67.5
171
0.5
73.6
163
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
46.7 50.5
53.9
143
157
167
1.0
1.0
1.5
55.0
59.5
63.3
138
150
161
0.0
0.5
0.5
60.4 65.4
69.1
131
143
153
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
42.2
128
1.0
49.9
124
0.0
54.8
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
42.8
129
1.0
50.6
124
0.0
55.6
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.24
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 6000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 7000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
48.0 51.9
55.3
143
157
167
1.0
1.0
1.5
56.4 61.1
64.8
138
151
161
0.0
0.5
0.5
62.0 66.8
70.8
131
143
153
80
2.5
58.4
178
1.5
68.2
171
0.5
74.5
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
48.6 52.6
56.0
143
157
167
1.0
1.0
1.5
57.2 61.9
65.6
138
151
161
0.0
0.5
0.5
62.8 67.6
71.6
131
143
153
80
2.5
59.1
178
1.5
69.0
171
0.5
75.3
163
or
pr
in
te
d
40
2.0
43.4
129
1.0
51.3
124
0.0
56.3
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
44.0
129
1.0
52.0
124
0.0
57.0
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.25
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 8000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 9000 FT
80
2.5
59.8
178
1.5
69.8
171
0.5
76.1
163
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
49.9
54.1
57.4
143
157
168
1.0
1.5
1.5
58.8
63.4
67.1
138
151
161
0.5
0.5
0.5
64.4 69.3
73.3
131
143
153
80
2.5
60.6
179
1.5
70.6
172
0.5
76.9
163
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
49.2 53.3
56.7
143
157
167
1.0
1.0
1.5
58.0
62.7
66.4
138
151
161
0.0
0.5
0.5
63.6 68.4
72.5
131
143
153
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
44.6
129
1.0
52.7
124
0.0
57.8
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
45.3
129
1.0
53.4
124
0.0
58.6
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.26
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 10000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 11000 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
50.6 54.7
58.1
143
157
168
1.0
1.5
1.5
59.6 64.2
67.9
138
151
161
0.5
0.5
0.5
65.2 70.1
74.1
131
143
153
80
2.5
61.4
179
1.5
71.4
172
0.5
77.8
164
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
51.3 55.5
58.8
143
157
168
1.0
1.5
1.5
60.4 65.1
68.7
138
151
161
0.5
0.5
0.5
66.0 71.0
74.9
131
143
153
80
2.5
62.2
179
1.5
72.3
172
0.5
78.7
164
or
pr
in
te
d
40
2.0
45.9
129
1.0
54.2
124
0.0
59.4
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
46.7
129
1.0
54.9
124
0.0
60.2
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.27
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 12000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 13000 FT
80
2.5
62.9
179
1.5
73.0
172
0.5
79.6
164
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
52.8
56.8
60.4
143
157
168
1.0
1.5
1.5
62.0
66.6
70.4
138
151
161
0.5
0.5
0.5
67.6 72.7
76.6
131
143
154
80
2.5
63.6
179
1.5
73.8
172
0.5
80.5
165
or
pr
in
te
d
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
52.0 56.2
59.6
143
157
168
1.0
1.5
1.5
61.2
65.8
69.5
138
151
161
0.5
0.5
0.5
66.8 71.8
75.7
131
143
153
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
47.3
129
1.0
55.6
124
0.0
61.0
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
47.9
129
1.0
56.4
124
0.0
61.9
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.28
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
FINAL APPROACH (1500 FT)
Gear Down, %N1 for 3° Glideslope
Airport Altitude = 14000 FT
Flap placard speed exceeded in shaded area.
Airport Altitude = 14500 FT
on
tro
lle
d
if
do
w
nl
o
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
53.5 57.6
61.3
143
157
168
1.0
1.5
1.5
62.9 67.5
71.3
138
151
161
0.0
0.5
0.5
68.6 73.6
77.6
131
144
154
80
2.5
64.4
180
1.5
74.6
172
0.5
81.4
165
WEIGHT (1000 KG)
50
60
70
2.5
2.5
2.5
53.9 58.0
61.7
144
157
168
1.0
1.5
1.5
63.4 68.0
71.7
138
151
161
0.0
0.0
0.5
69.2 74.1
78.1
131
144
154
80
2.5
64.7
180
1.5
75.0
172
0.5
81.9
165
or
pr
in
te
d
40
2.0
48.7
129
1.0
57.4
124
0.0
62.9
117
ad
ed
FLAP POSITION
(VREF + INCREMENT)
PITCH ATT
FLAPS 15
%N1
(VREF15 + 10)
KIAS
PITCH ATT
FLAPS 30
%N1
(VREF30 + 10)
KIAS
PITCH ATT
FLAPS 40
%N1
(VREF40 + 10)
KIAS
40
2.0
49.1
129
1.0
58.0
124
0.0
63.4
117
U
nc
Flap placard speed exceeded in shaded area.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.29
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Flight With Unreliable Airspeed/ Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
General
GO-AROUND
Flaps 15, Gear Up, Set Go-Around Thrust
5000
SEA
LEVEL
U
nc
on
tro
lle
d
if
-2000
80
9.0
1400
175
10.5
1700
174
12.5
2200
173
14.0
2600
173
14.5
2500
173
or
pr
in
te
d
10000
WEIGHT (1000 KG)
50
60
70
14.0
11.5
10.5
2700
2200
1700
141
154
164
16.0
13.5
12.0
3200
2600
2100
141
153
163
19.0
16.0
14.0
3800
3100
2600
141
153
163
22.0
18.5
16.0
4300
3600
3000
141
153
163
22.5
18.5
16.0
4200
3500
3000
140
153
163
ad
ed
14500
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
PITCH ATT
V/S (FT/MIN)
KIAS
40
17.5
3500
127
20.0
4000
127
24.0
4600
127
28.0
5200
127
28.0
5100
127
do
w
nl
o
PRESSURE ALTITUDE (FT)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.30
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
Max Climb %N1
file Highlight
Based on engine bleed for packs on or off and anti-ice off
PRESSURE ALTITUDE (FT)/SPEED (KIAS/MACH)
10000
15000
20000
25000
30000
35000
280
280
280
280
280
.78
90.4
90.6
90.4
92.1
93.8
95.1
91.3
91.4
90.8
91.5
93.1
94.4
92.1
92.2
91.7
91.5
92.4
93.7
92.8
93.0
92.6
92.4
92.4
93.0
93.6
93.8
93.4
93.2
93.2
92.3
94.3
94.5
94.3
94.0
94.0
93.0
95.0
95.2
95.1
94.8
94.7
93.9
95.7
95.9
95.9
95.5
95.4
94.7
96.5
96.7
96.6
96.2
96.1
95.4
95.9
97.5
97.4
96.9
96.7
96.2
95.1
97.8
98.3
97.7
97.4
96.9
94.3
97.0
99.2
98.6
98.1
97.7
93.5
96.2
98.6
99.6
99.1
98.5
92.7
95.4
97.8
99.6
100.0
99.2
91.9
94.6
97.1
98.8
100.3
100.2
91.0
93.8
96.3
98.0
99.6
101.1
90.2
93.0
95.5
97.2
98.7
100.8
89.4
92.2
94.7
96.4
97.9
100.0
88.5
91.3
93.9
95.6
97.1
99.1
87.7
90.5
93.1
94.8
96.3
98.3
86.8
89.6
92.3
93.9
95.4
97.4
37000
.78
95.2
94.5
93.8
93.1
92.4
92.4
93.3
94.1
94.9
95.7
96.5
97.3
98.2
99.0
99.8
100.8
101.3
100.5
99.6
98.8
97.9
41000
.78
93.5
92.8
92.1
91.4
90.7
90.8
91.8
92.8
93.7
94.6
95.6
96.5
97.5
98.4
99.4
100.4
101.0
100.1
99.3
98.4
97.6
or
pr
in
te
d
5000
280
90.5
91.2
92.0
92.6
93.3
94.0
94.8
94.8
94.0
93.2
92.5
91.7
90.9
90.1
89.3
88.5
87.6
86.8
86.0
85.1
84.3
ad
ed
60
55
50
45
40
35
30
25
20
15
10
5
0
-5
-10
-15
-20
-25
-30
-35
-40
0
280
90.2
91.0
91.7
92.4
93.1
93.6
92.9
92.2
91.4
90.6
89.9
89.1
88.3
87.6
86.8
86.0
85.2
84.3
83.5
82.7
81.8
do
w
nl
o
TAT (°C)
%N1 Adjustments for Engine Bleeds
BLEED CONFIGURATION
ENGINE ANTI-ICE
ENGINE & WING ANTI-ICE*
PRESSURE ALTITUDE (1000 FT)
10
20
30
35
-0.8
-0.9
-0.9
-0.8
-2.1
-2.5
-2.7
-3.0
41
-0.8
-3.0
U
nc
on
tro
lle
d
if
*Dual bleed sources
0
-0.6
-1.8
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.31
Performance Inflight - QRH
General
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Go-around %N1
Based on engine bleed for packs on, engine and wing anti-ice on or off
0
96.2
96.7
97.6
98.4
99.1
99.9
99.8
99.1
98.3
97.5
96.8
96.0
95.2
94.4
93.6
92.8
92.0
91.1
90.3
89.4
88.6
87.7
86.8
1000
96.8
96.6
97.8
98.5
99.2
100.0
100.4
99.7
98.9
98.1
97.4
96.6
95.8
95.0
94.2
93.4
92.6
91.8
90.9
90.1
89.2
88.4
87.5
2000
3000
4000
5000
6000
7000
8000
96.8 97.5
97.8 97.7 97.5 98.2 98.8
98.6 98.7 98.8 98.7 98.5 98.5 99.0
99.3 99.4 99.5 99.6 99.5 99.1 98.9
100.1 100.1 100.3 100.3 100.2 99.9 99.6
100.7 100.7 100.7 100.7 100.7 100.6 100.4
100.2 100.6 100.9 100.9 100.9 100.9 100.9
99.5 99.8 100.2 100.5 100.9 101.0 101.1
98.7 99.1 99.4 99.8 100.1 100.5 100.9
98.0 98.3 98.7 99.0 99.4 99.8 100.2
97.2 97.6 97.9 98.3 98.7 99.0 99.4
96.4 96.8 97.2 97.5 97.9 98.3 98.7
95.6 96.0 96.4 96.8 97.2 97.5 97.9
94.8 95.2 95.6 96.0 96.4 96.8 97.1
94.0 94.4 94.8 95.2 95.6 96.0 96.4
93.2 93.6 94.0 94.4 94.8 95.2 95.6
92.4 92.8 93.2 93.6 94.0 94.4 94.8
91.6 92.0 92.4 92.8 93.3 93.6 94.0
90.7 91.1 91.6 92.0 92.4 92.8 93.2
89.9 90.3 90.7 91.2 91.6 92.0 92.4
89.0 89.4 89.9 90.3 90.8 91.2 91.5
88.2 88.6 89.0 89.5 90.0 90.3 90.7
9000 10000
98.8
99.6
100.4
100.9
101.0
101.3
100.5
99.8
99.0
98.3
97.5
96.7
95.9
95.1
94.3
93.5
92.7
91.9
91.0
99.1
99.5
100.3
100.8
101.0
101.2
100.9
100.2
99.4
98.6
97.9
97.1
96.3
95.5
94.7
93.9
93.0
92.2
91.4
or
pr
in
te
d
60
55
50
45
40
35
30
25
20
15
10
5
0
-5
-10
-15
-20
-25
-30
-35
-40
-45
-50
AIRPORT PRESSURE ALTITUDE (FT)
-2000
95.0
95.9
96.6
97.4
98.0
98.1
97.3
96.6
95.8
95.0
94.2
93.4
92.6
91.8
91.0
90.2
89.3
88.5
87.6
86.8
85.9
85.0
84.1
ad
ed
TAT
(°C)
do
w
nl
o
AIRPORT
OAT
°C
°F
57
134
52
125
47
116
42
108
37
99
32
90
27
81
22
72
17
63
12
54
7
45
2
36
-3
27
-8
18
-13
9
-17
1
-22
-8
-27
-17
-32
-26
-37
-35
-42
-44
-47
-53
-52
-62
%N1 Adjustments for Engine Bleeds
0
0.8
-0.1
1000
0.8
-0.1
2000
0.8
-0.1
if
-2000
0.7
-0.1
PRESSURE ALTITUDE (FT)
3000 4000 5000 6000 7000
0.8
0.9
0.9
0.9
0.9
-0.1 -0.1 -0.1 -0.1 -0.1
8000
0.9
-0.1
9000 10000
0.9
0.9
-0.1 -0.1
U
nc
on
tro
lle
d
BLEED
CONFIGURATION
PACKS OFF
A/C HIGH
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.32
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
General
Category C/N Brakes
737 Flight Crew Operations Manual
VREF
file Highlight
40
159
154
148
143
139
133
127
121
114
107
15
174
169
163
157
153
147
140
133
126
119
U
nc
on
tro
lle
d
if
do
w
nl
o
ad
ed
85
80
75
70
65
60
55
50
45
40
FLAPS
30
167
162
156
151
147
141
134
128
121
114
or
pr
in
te
d
WEIGHT (1000 KG)
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.40.33
Performance Inflight - QRH
General
do
w
nl
o
ad
ed
or
pr
in
te
d
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
U
nc
on
tro
lle
d
if
Intentionally
Blank
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.40.34
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
Performance Inflight - QRH
Chapter PI-QRH
Advisory Information
Section 41
Advisory
file
Highlight
Information
ADVISORY INFORMATION
Runway Surface Condition Correlation
Advisory Information
Advisory Information
5
4
3
Dry
Wet (Smooth, Grooved or PFC) or Frost
3 mm (0.12 inches) or less of: Water, Slush, Dry Snow or Wet Snow
Compacted Snow at or below -15°C OAT
Wet (Slippery), Dry Snow or Wet Snow (any depth) over Compacted Snow
Greater than 3 mm (0.12 inches) of : Dry Snow or Wet Snow
Compacted Snow at OAT warmer than -15°C
Greater than 3 mm (0.12 inches) of: Water or Slush
Ice
Wet Ice, Water on top of Compacted Snow, Dry Snow or Wet Snow over Ice
Good
Good to Medium
Medium
Medium to Poor
Poor
Nil
U
nc
on
tro
lle
d
if
do
w
nl
o
ad
ed
2
1
0
REPORTED
BRAKING
ACTION
Dry
RUNWAY SURFACE CONDITION DESCRIPTION
or
pr
in
te
d
RUNWAY
CONDITION
CODE
6
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.41.1
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
1250
1555
2130
2615
2850
70/-65
70/-75
115/-120
160/-165
185/-195
25/30
30/40
50/70
75/100
85/115
-40/140
-50/165
-85/280
-115/385
-130/455
40/50
40/50
50/70
75/100
85/115
-65/225
-70/235
-85/290
-115/385
-130/455
35/-30
35/-30
5/-10
35/-45
75/-80
50/65
50/70
60/80
75/100
85/115
-85/300
-85/310
-100/340
-120/410
-135/465
65/80
65/85
65/85
75/105
85/115
-105/375
-105/380
-110/390
-125/435
-140/470
Good Reported Braking Action
1640
1755
2135
2615
2850
80/-85
85/-90
115/-120
160/-165
185/-195
40
65
100
100
90
15
0
0
90
215
40
5
0
90
345
35/-35
40/-40
50/-50
70/-70
80/-80
50
65
100
100
90
70
75
5
90
215
150
165
10
90
345
65/-50
60/-50
35/-30
55/-60
90/-85
45/-45
50/-50
60/-60
70/-70
80/-80
60
70
100
100
90
130
130
70
110
220
300
315
195
170
375
90/-70
85/-70
65/-50
75/-70
105/-85
50/-60
60/-60
65/-65
75/-75
80/-80
70
80
100
100
90
190
190
130
130
225
450
460
380
245
405
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
10/-10
0/0
0/-5
35/-45
75/-80
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF30
25/-25
35/-35
50/-50
70/-70
80/-80
ad
ed
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1910
1995
2240
2645
2860
105/-110
110/-115
125/-130
160/-170
185/-195
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
2175
2235
2345
2675
2865
125/-130
130/-140
130/-140
160/-175
185/-195
U
nc
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
d
Medium Reported Braking Action
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.41.2
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
APP
SPD
ADJ
REVERSE
THRUST
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
-130/485
-130/490
-135/495
-145/525
-150/550
155/-105
150/-105
140/-95
140/-105
160/-120
65/-70
65/-70
70/-70
80/-80
85/-85
75
85
95
100
90
300
295
275
245
310
-155/600
-155/600
-160/600
-165/615
-165/635
220/-145
220/-140
215/-140
205/-140
220/-150
75/-80
75/-80
75/-80
80/-85
85/-90
80
90
90
100
90
410 1060
405 1060
415 1070
360 930
390 970
2480
2515
2585
2825
2975
155/-160
160/-160
160/-160
180/-185
195/-200
75/100
80/105
80/105
85/115
90/125
Poor Reported Braking Action
2780
2790
2825
2975
3085
185/-185
185/-185
185/-185
195/-195
200/-205
85/120
90/120
90/120
90/125
100/130
do
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o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
ad
ed
Medium To Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
PER
5 KTS ONE NO
ABOVE REV REV
VREF30
or
pr
in
te
d
REF
DIST
755
760
725
590
685
if
Reference distance is based on sea level, standard day, no wind or slope, VREF30, two-engine detent No. 2
reverse thrust, and auto speedbrakes.
For max manual braking and manual speedbrakes, increase reference landing distance by 70 m.
For autobrake and manual speedbrakes, increase reference landing distance by 60 m.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
All reference distances and adjustments shown have been increased by 15%.
U
nc
on
tro
lle
d
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.41.3
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
1200
1465
1975
2450
2690
60/-60
65/-70
105/-115
145/-155
175/-180
25/30
30/35
45/65
70/85
80/105
-40/130
-45/160
-80/270
-110/375
-125/435
35/45
40/50
45/65
70/85
80/105
-65/225
-70/230
-80/275
-110/375
-125/435
35/-30
30/-30
10/-5
30/-40
65/-75
45/60
50/65
50/70
70/90
80/105
-85/295
-85/300
-90/330
-115/400
-130/450
60/75
60/80
60/80
70/90
80/110
-105/370
-105/375
-105/380
-120/425
-130/460
Good Reported Braking Action
1580
1680
1980
2450
2690
75/-80
80/-85
105/-115
145/-155
175/-180
40
65
100
105
100
15
0
0
45
165
35
0
0
45
260
35/-35
35/-35
45/-50
65/-65
75/-75
50
65
105
105
100
65
70
5
45
165
140
150
10
45
260
60/-50
55/-45
40/-30
50/-50
80/-80
45/-45
45/-45
50/-55
65/-65
75/-75
60
70
100
105
100
120
120
70
70
175
270
280
195
125
290
85/-70
80/-65
70/-50
70/-65
90/-80
50/-50
50/-50
60/-60
70/-70
75/-75
70
80
100
105
100
175
175
130
90
185
405
410
375
200
315
do
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o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
10/-10
0/0
0/-5
30/-40
65/-75
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF40
25/-25
30/-30
45/-45
65/-65
75/-75
ad
ed
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1830
1905
2090
2485
2695
100/-100
105/-105
115/-125
145/-160
175/-180
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
2085
2125
2200
2515
2700
120/-120
125/-125
125/-130
150/-160
175/-180
U
nc
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
d
Medium Reported Braking Action
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.41.4
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Normal Configuration Landing Distance
Flaps 40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
APP
SPD
ADJ
REVERSE
THRUST
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
-130/475
-130/480
-130/485
-140/515
-150/540
150/-105
150/-100
140/-95
135/-100
150/-110
60/-65
60/-65
65/-65
70/-75
80/-80
75
85
95
100
95
275
275
255
205
265
680
680
670
520
585
-155/585
-155/585
-155/585
-160/605
-165/620
220/-140
220/-140
215/-140
200/-130
205/-145
70/-75
70/-75
70/-75
75/-80
80/-85
80
85
90
100
90
375
375
380
315
350
955
955
965
840
855
2370
2395
2445
2670
2810
145/-145
150/-150
150/-155
165/-175
180/-185
70/95
70/100
70/100
80/105
85/120
Poor Reported Braking Action
2660
2665
2690
2820
2925
175/-175
175/-175
180/-180
185/-185
190/-195
80/115
85/115
85/115
85/120
90/125
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
ad
ed
Medium To Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
AUTOBRAKE 2
AUTOBRAKE 1
PER
5 KTS ONE NO
ABOVE REV REV
VREF40
or
pr
in
te
d
REF
DIST
if
Reference distance is based on sea level, standard day, no wind or slope, VREF40, two-engine detent No. 2
reverse thrust, and auto speedbrakes.
For max manual braking and manual speedbrakes, increase reference landing distance by 65 m.
For autobrake and manual speedbrakes, increase reference landing distance by 50 m.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
All reference distances and adjustments shown have been increased by 15%.
U
nc
on
tro
lle
d
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.41.5
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
file Highlight
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Airspeed Unreliable (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1185
1540
2600
85/-60
70/-75
160/-170
25/30
35/45
80/105
-35/125
-50/160
-110/360
10/-10
0/0
50/-55
80/-80
85/-90
160/-170
40/50
40/55
80/105
-60/205
-60/215
-110/360
30/-30
30/-20
50/-55
25
0
160
50
5
185
35/-35
40/-40
75/-75
N/A
N/A
N/A
75
85
160
175
195
185
50/65
55/70
80/105
-80/275
-80/280
-115/385
55/-50
55/-40
65/-65
45/-45
50/-50
75/-75
N/A
N/A
N/A
145
155
180
350
365
265
60/80
65/85
65/90
-95/340
-95/345
-100/365
80/-65
75/-60
55/-50
55/-55
55/-55
65/-65
N/A
N/A
N/A
215
220
125
520
535
385
75/100
80/105
80/110
-120/440
-120/440
-125/455
140/-100
135/-95
120/-85
65/-70
65/-70
70/-75
N/A
N/A
N/A
335
335
280
875
880
800
90/120
90/125
90/125
-145/535
-145/535
-145/540
195/-130
195/-125
185/-120
75/-80
75/-80
75/-80
N/A
N/A
N/A
455 1230
450 1225
430 1215
Good To Medium Reported Braking Action
1825
1915
2625
105/-105
105/-110
165/-175
do
w
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o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
25/-25
35/-35
75/-75
ad
ed
1560
1680
2600
REVERSE
THRUST
ADJ
N/A
N/A
N/A
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2085
2145
2335
125/-125
125/-130
130/-140
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
150/-150
155/-155
155/-160
d
2375
2415
2540
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2665
2680
2740
175/-175
180/-180
175/-180
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.41.6
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Airspeed Unreliable (Flaps 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1145
1465
2415
65/-55
65/-70
145/-155
75/-75
80/-85
145/-155
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-35/125
-45/155
-105/345
10/-10
0/0
45/-50
20/-20
30/-30
65/-65
N/A
N/A
N/A
20
0
135
45
5
185
35/50
40/50
70/95
-60/200
-60/210
-105/345
30/-25
30/-20
45/-50
35/-35
35/-35
65/-65
N/A
N/A
N/A
70
80
135
155
175
185
-75/265
-80/275
-110/370
55/-45
55/-40
60/-60
45/-45
45/-45
65/-70
N/A
N/A
N/A
130
135
155
305
320
255
-90/330
-95/335
-100/350
80/-60
75/-60
60/-50
50/-50
50/-55
60/-60
N/A
N/A
N/A
185
190
115
450
465
340
70/95
75/95
70/95
-115/425
-120/430
-120/440
135/-95
130/-90
120/-85
60/-60
60/-65
65/-70
N/A
N/A
N/A
290
290
240
740
745
675
80/110
85/110
80/110
-140/520
-140/525
-140/525
185/-125
180/-120
180/-115
65/-70
70/-75
70/-75
N/A
N/A
N/A
390 1025
390 1025
365 1010
ad
ed
1505
1615
2415
REVERSE
THRUST
ADJ
20/30
30/40
70/95
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
1745
1830
2440
95/-95
100/-105
150/-155
45/65
50/65
75/95
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
1980
2045
2190
115/-115
120/-120
120/-125
55/75
60/80
60/80
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
140/-140
145/-145
145/-145
d
2245
2290
2380
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2510
2535
2570
160/-160
165/-165
165/-165
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.41.7
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
Airspeed Unreliable (Flaps 40)
VREF40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1105
1375
2280
55/-50
60/-65
135/-145
20/30
30/35
65/85
-35/120
-45/150
-100/335
10/-10
0/0
40/-45
70/-75
75/-80
135/-145
35/45
35/50
65/85
-55/200
-60/210
-100/335
N/A
N/A
N/A
20
0
105
40
0
125
30/-25
30/-25
40/-45
35/-35
35/-35
60/-60
N/A
N/A
N/A
65
70
105
145
160
125
45/60
45/65
70/90
-75/265
-75/270
-105/360
55/-45
55/-45
55/-55
45/-45
45/-45
65/-65
N/A
N/A
N/A
120
125
125
280
290
195
55/70
55/75
55/75
-90/325
-90/330
-95/345
75/-60
75/-60
60/-45
50/-50
50/-50
55/-55
N/A
N/A
N/A
170
175
115
410
420
335
65/90
70/90
65/90
-115/420
-115/425
-115/435
130/-90
130/-90
120/-80
60/-60
60/-60
60/-65
N/A
N/A
N/A
265
265
235
670
675
635
75/105
80/105
75/105
-135/515
-135/515
-135/520
185/-120
185/-115
180/-115
65/-70
65/-70
65/-70
N/A
N/A
N/A
355
355
355
925
925
935
Good To Medium Reported Braking Action
1680
1755
2305
90/-95
95/-100
135/-145
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
1455
1550
2280
REVERSE
THRUST
ADJ
20/-20
30/-30
60/-60
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
1905
1960
2060
110/-110
110/-115
110/-120
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
135/-135
135/-135
135/-140
d
2155
2195
2255
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
2405
2425
2450
155/-155
155/-155
155/-155
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.41.8
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
All Flaps Up Landing
VREF40 + 55
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1470
1965
3585
190/-80
90/-85
195/-225
90/-100
90/-100
195/-225
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-45/200
-60/190
-130/435
20/-15
5/0
60/-75
35/-35
50/-50
105/-105
45
75
115
40
5
215
85
15
225
50/70
55/75
115/150
-70/235
-75/245
-130/435
40/-35
30/-25
60/-75
50/-50
55/-55
105/-105
50
75
115
110
95
215
255
250
225
-90/315
-95/320
-135/460
75/-65
70/-55
80/-85
65/-65
65/-70
110/-110
60
80
115
215
210
240
525
530
340
-110/390
-115/395
-120/420
110/-90
105/-85
65/-45
75/-75
75/-80
90/-90
70
80
125
320
325
185
795
805
570
110/145
110/145
110/150
-140/505
-145/505
-145/525
190/-135
190/-130
155/-100
90/-95
90/-95
100/-105
80
90
125
520 1395
520 1390
430 1265
130/175
130/175
130/175
-170/620
-170/615
-170/625
270/-180
270/-175
245/-155
105/-110
105/-110
110/-115
90
95
120
715 1990
710 1975
675 1955
ad
ed
1950
2135
3585
REVERSE
THRUST
ADJ
50/105
45/75
115/150
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
2335
2455
3615
125/-130
125/-130
200/-225
70/95
75/95
115/155
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2720
2775
3080
155/-160
155/-160
150/-165
85/115
90/115
90/120
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
195/-200
195/-200
190/-195
d
3155
3180
3370
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3590
3580
3660
230/-235
230/-235
225/-225
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.41.9
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
ANTISKID INOPERATIVE (Flaps 15)
VREF15
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1860
100/-105
50/65
-80/280
50/-45
Autobrake Inoperative
Autobrake Inoperative
55/75
-95/340
75/-60
Autobrake Inoperative
Autobrake Inoperative
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
2070
120/-120
Good To Medium Reported Braking Action
2345
145/-145
45/-45
60
125
295
50/-50
65
185
460
795
70/95
-120/440 135/-95
Autobrake Inoperative
Autobrake Inoperative
60/-65
70
300
85/115
-140/535 190/-125
Autobrake Inoperative
Autobrake Inoperative
70/-75
75
410 1125
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
REVERSE
THRUST
ADJ
PER
5 KTS ONE NO
ABOVE REV REV
VREF
ad
ed
Good Reported Braking Action
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Medium Reported Braking Action
2615
170/-170
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
210/-210
d
3035
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
105/145
-190/760 395/-210
Autobrake Inoperative
Autobrake Inoperative
80/-95
85
710 2305
120/175
-235/985 600/-290
Autobrake Inoperative
Autobrake Inoperative
90/-110
90
1005 3480
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3455
250/-245
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
PI-QRH.41.10
D6-27370-8AS-NOK
September 30, 2022
737-800WSFP1/CFM56-7B26
Performance Inflight - QRH
JAA
Advisory Information
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
ANTISKID INOPERATIVE (Flaps 30)
VREF30
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1785
95/-100
110/-115
PER
5 KTS ONE NO
ABOVE REV REV
VREF
-75/275
50/-40
Autobrake Inoperative
Autobrake Inoperative
40/-40
55
110
260
55/70
-90/335
75/-60
Autobrake Inoperative
Autobrake Inoperative
45/-50
65
165
395
-115/430 130/-90
Autobrake Inoperative
Autobrake Inoperative
55/-60
70
260
670
-135/520 180/-120
Autobrake Inoperative
Autobrake Inoperative
65/-70
75
355
940
ad
ed
1975
REVERSE
THRUST
ADJ
45/60
Good Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
APP
SPD
ADJ
or
pr
in
te
d
REF
DIST
Good To Medium Reported Braking Action
2225
135/-135
65/90
do
w
nl
o
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
Medium Reported Braking Action
2470
155/-155
75/105
if
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
Medium To Poor Reported Braking Action
190/-190
d
2855
on
tro
lle
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
95/135
-185/740 370/-195
Autobrake Inoperative
Autobrake Inoperative
75/-90
80
610 1895
110/160
-230/960 560/-270
Autobrake Inoperative
Autobrake Inoperative
85/-105
85
860 2845
Poor Reported Braking Action
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 3
3235
225/-225
U
nc
Reference distance is based on sea level, standard day, no wind or slope, and maximum available reverse
thrust.
MAX MANUAL assumes maximum achievable manual braking.
Reference Distance includes an air distance allowance of 455 m from threshold to touchdown.
Actual (unfactored) distances are shown.
*For landing distance at or below 8000 ft pressure altitude, apply the STD adjustment. For altitudes higher
than 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply
the HIGH adjustment to this new reference distance.
Boeing Proprietary. Copyright © Boeing. ECCN: 9E991. See title page for details.
September 30, 2022
D6-27370-8AS-NOK
PI-QRH.41.11
Performance Inflight - QRH
Advisory Information
737-800WSFP1/CFM56-7B26
JAA
Category C/N Brakes
737 Flight Crew Operations Manual
ADVISORY INFORMATION
Non-Normal Configuration Landing Distance
ANTISKID INOPERATIVE (Flaps 40)
VREF40
LANDING DISTANCE AND ADJUSTMENTS (M)
WT
ADJ
ALT
ADJ
WIND
ADJ
SLOPE
ADJ
TEMP
ADJ
PER
PER
65000 KG
PER
10 KTS
BRAKING
5000 KG
LANDING
1000 FT
HEAD/
CONFIGURATION
ABV/BLW
WEIGHT
STD/HIGH* TAIL
65000 KG
WIND
PER 1%
DOWN/
UP
HILL
PER
10°C
ABV/
BLW
ISA
Dry Runway
MAX MANUAL
AUTOBRAKE MAX
AUTOBRAKE 2
1715
90/-95
40/55
-75/270
50/-40
Autobrake Inoperative
Autobra