BOEING 737NG
BOEING 737NG NORMAL PROCEDURES
Boeing 737NG Normal Procedures for passenger airplanes by Claudio
Fonseca.
Claudio Fonseca is real pilot with more than 10,000 flying hours (almost all of
them on Boeing airplanes).
At the time of writing, Claudio Fonseca is not a current Boeing 737NG,
anymore. He holds 4993 flying hours on the -700 and -800 versions.
The procedures shown here are discussed and exemplified using the
MSFS2020 simulator, on the PMDG 737NG and can be accessed through
Claudio
Fonseca
YouTube
channel
named
LEVEL
CHANGE
at
https://www.youtube.com/LEVELCHANGEbyClaudioFonseca.
This document is been updates as the real procedure changes and/or
modifications are incorporated into the Flight Crew Operations Manual.
An introductory chapter is expected to cover some operations and procedures
used during routine flights.
In addition, a chapter with standard callouts and their description is planned to
complete this document.
The current document version is 1.1 and it is dated 22-NOV-2022.
Claudio Fonseca can be reached through the YouTube channel, or directly by
mail at claudiofonseca@hotmail.com.
Thank you,
Normal Procedures
Page|1
BOEING 737NG
Preliminary Preflight Procedure
The Preliminary Preflight Procedure assumes that the Electrical Power Up
supplementary procedure is complete.
Captain
First Officer
Technical Log ...................................................................................................................................................................................................................................................................... Check
Verify that the necessary preflight checks are completed.
Verify that the reported inoperative item(s) is(are) rectified or deferred by the
maintenance staff.
Verify that the deferred item(s) is(are) fully compliant with the MEL/CDL or that the NEF
item(s) do(es) not affect the flight safety and airworthiness.
Secondary ENG display ...................................................................................................................................................................................................................................................... Check
Verify that the engine oil quantity is sufficient for the flight.
Note: Minimum Engine Oil quantity is 70% or 15 quarts.
SYS display ......................................................................................................................................................................................................................................................................... Check
Verify that the hydraulic quantity is sufficient for the flight.
Note: Confirm RF is not shown.
Flight CREW OXYGEN Pressure Indicator ......................................................................................................................................................................................................................... Check
Verify that the oxygen pressure is sufficient for the flight.
Note: Check Performance Dispatch – Enroute – Crew Oxygen Requirements when
below 1000 PSI.
PARKING BRAKE .................................................................................................. As needed
Set the parking brake to check the brake wear indicators during the exterior inspection.
If the Parking Brake is set:
Verify that the PARKING BRAKE warning light is illuminated.
EFB (as installed) .......................................................................................................... Check
IRS mode selectors ........................................................................................ OFF, then NAV
Verify that the ON DC lights illuminate then extinguish.
Verify that the ALIGN lights are illuminated.
Note: Full IRS alignment is recommended. If time does not allow a full alignment, do
the Fast Realignment supplementary procedure.
POWER switch ............................................................................................................. ON
EMERGENCY LIGHTS switch........................................................................... Guard closed
Verify that the NOT ARMED light is extinguished.
INITIALIZE FLIGHT ................................................................................................... Push
EFB (as installed) .......................................................................................................... Check
Database ................................................................................................................. Check
Verify that the database is current.
POWER switch .................................................................................................As needed
Applications .......................................................................................... Use as necessary
Calculate the Maximum Takeoff Weight and the Landing Dispatch.
Database ................................................................................................................. Check
Verify that the database is current.
Review the fuel requirements and fill the dispatch papers.
Applications .......................................................................................... Use as necessary
INITIALIZE FLIGHT ................................................................................................... Push
Obtain the ATIS or weather and operational information.
Only:
Do the remaining actions on the first flight or after any maintenance action
.
Normal Procedures
Page|2
BOEING 737NG
Captain
First Officer
Aircraft documents ......................................................................................................... Check
Fire and Overheat System ................................................................................................ Test
Note: Alert ground personnel before the following test is accomplished.
Verify that the engine No. 1, APU and the engine No. 2 fire switches are in.
Passenger Address System ......................................................................................... Check
OVERHEAT DETECTOR switches ................................................................... NORMAL
TEST switch..................................................................................... Hold to FAULT/INOP
Verify that the MASTER CAUTION lights are illuminated.
Verify that the OVHT/DET annunciator is illuminated.
Verify that the FAULT light is illuminated.
Verify that the APU DET INOP light is illuminated.
CAUTION: The fire warning light flashes and the horn sounds on the APU ground
control panel when this test is done with the APU running. This can be mistaken by
the ground crew as an APU fire.
TEST switch....................................................................................... Hold to OVHT/FIRE
Verify that the fire warning bell sounds.
Verify that the master FIRE WARN lights are illuminated.
Verify that the MASTER CAUTION lights are illuminated.
Verify that the OVHT/DET annunciator is illuminated.
Master FIRE WARN light ..................................................................................... Push
Verify that the master FIRE WARN lights are extinguished.
Verify that the fire warning bell cancels.
Verify that the engine No. 1, APU and the engine No. 2 fire switches stay
illuminated.
Verify that the ENG 1 OVERHEAT and ENG 2 OVERHEAT lights stay
illuminated.
Verify that the WHEEL WELL fire warning light stays illuminated.
TEST switch.......................................................................................................... Release
EXTINGUISHER TEST switch ................................................................................ Check
TEST Switch ............................................................................. Position to 1 and hold
Verify that the three green extinguisher test lights are illuminated.
TEST Switch ................................................................................................... Release
Verify that the three green extinguisher test lights are extinguished.
Repeat for test position 2.
CARGO FIRE System ...................................................................................................... Test
DETECTOR SELECT switches .............................................................................. NORM
TEST switch............................................................................................................... Push
Verify that the fire warning bell sounds.
Verify that the master FIRE WARN lights are illuminated.
Normal Procedures
Page|3
BOEING 737NG
Captain
First Officer
Master FIRE WARN light ..................................................................................... Push
Verify that the master FIRE WARN lights are extinguisher.
Verify that the fire warning bell cancels.
Verify that the FWD and AFT lights stay illuminated.
Verify that the green EXTINGUISHER test lights stay illuminated.
Verify that the DETECTOR FAULT light stays extinguished.
Verify that the DISCH light stay illuminated.
TEST switch.......................................................................................................... Release
Aircraft documents ......................................................................................................... Check
FLIGHT DECK ACCESS SYSTEM switch ........................................................ Guard closed
Note: Refer to the “Flight Deck Door Access System Test” Supplementary
Procedure.
Emergency equipment ................................................................................................... Check
Fire extinguisher .............................................................................. Checked and stowed
Crash axe .............................................................................................................. Stowed
Scape ropes........................................................................................................... Stowed
Smoke Hood (PBE) ......................................................................... Checked and stowed
Heat Resistant Gloves ........................................................................................... Stowed
Flashlights.............................................................................................................. Stowed
Life Vests ............................................................................................................... Stowed
Smoke goggles (if applicable) ............................................................................... Stowed
ELT switch (as installed) .................................................................................... Guard closed
Verify that the ELT light is extinguished.
PSEU light...................................................................................................................... Check
Verify that the PSEU light is extinguished.
GPS light ........................................................................................................................ Check
Verify that the GPS light is extinguished.
SERVICE INTERPHONE switch ...................................................................................... OFF
AUDIO CONTROL PANEL (observer) ........................................................................... Verify
Transmitter Selector switch in PA, and all others receivers closed and in minimum
volume.
ENGINE panel ............................................................................................................... Check
Verify that the REVERSER lights are extinguished.
Verify that the ENGINE CONTROL lights are extinguished.
Normal Procedures
Page|4
BOEING 737NG
Captain
First Officer
EEC switches................................................................................................................ON
Verify that the ALTN lights are extinguished.
Oxygen panel ................................................................................................................. Check
CAUTION: PASSANGER OXYGEN switch activation causes deployment of the
passenger oxygens masks.
PASSENGER OXYGEN switch ................................................................... Guard closed
Verify that the PASS OXY ON light is extinguished.
Landing gear indicator lights .......................................................................................... Check
Verify that the lights are illuminated.
Flight recorder switch ......................................................................................... Guard closed
MACH AIRSPEED WARNING TEST switches ............................. Push and hold one at time
Verify that the clacker sounds.
STALL WARNING TEST switches ................................................ Push and hold one at time
Verify that each control column vibrates when the respective switch pushed.
Note: The stall warning test requires that AC transfer busses are powered for up to
4 minutes.
Note: With hydraulic power off, the leading edge flaps may droop enough to cause
an asymmetry signal, resulting in a failure of the stall warning system test. Should
this occur, obtain a clearance to pressurize the hydraulic system, place the “B”
system electric pump ON and retract the flaps. When flaps are retracted repeat the
test. At the completion of the test, turn the “B” system electric pump “OFF”.
Circuit breakers (P6 panel) ............................................................................................ Check
Note: Check circuit breakers position carefully in flights after maintenance service or
overnights. CBs may be found pulled due to maintenance action.
Manual gear extension access door ............................................................................. Closed
Circuit breakers (control stand, P18 panel) ................................................................... Check
Note: Check circuit breakers position carefully in flights after maintenance service or
overnights. CBs may be found pulled due to maintenance action.
Normal Procedures
Page|5
BOEING 737NG
FMC Initial Data and Exterior Inspection
Start the FMC Initial Data after the Preliminary Preflight Procedure.
Perform the Exterior Inspection after the Preliminary Preflight Procedure.
Captain
First Officer
FMC Initial Data
Exterior Inspection
IDENT page ........................................................................................................................ Set
Verify that the MODEL is correct.
Verify that the ENG RATING is correct.
Verify that the navigation data base ACTIVE date range is current.
Before each flight the Captain or First Officer must verify that the airplane is satisfactory for
flight.
POS INIT page ................................................................................................................... Set
Enter the current airport as REF AIRPORT.
Note: The gate (parking position) do not need to be inserted.
Verify that the time is correct.
Enter the present position on the SET IRS POS.
Note: Use the most accurate latitude and longitude.
Note: If available, the GPS position is the most accurate.
Note: GPS position, if available, is shown on page 2 (POS REF).
RTE page ............................................................................................................................ Set
Enter the ORIGIN and the DESTination.
If datalink is available:
Select FLT PLAN REQUEST.
When ROUTE UPLINK READY shows:
Select LOAD.
After ROUTE DATA UPLINK has been completed, verify the route against the
Flight Plan.
At RTE 1 page 1/X:
Enter the ATC Calssing as FLT NO.
If datalink is not available:
If company route is available:
Enter the CO ROUTE name.
Verify the route against the Flight Plan.
At RTE 1 page 1/X:
Enter the ATC Calssing as FLT NO.
If company route is not available:
Use the next page(s) to enter the RTE.
At RTE 1 page 1/X:
Enter the ATC Calssing as FLT NO.
ACTIVATE and EXECute the route.
Items at each location may be checked in any sequence. Check that:
• the surfaces and structures are clear, not damaged, not missing parts and there are no
fluid leaks;
• the tires are not too worn, not damaged, and there is no tread separation;
• the gear struts are not fully compressed;
• the engine inlets and tailpipes are clear, the access panels are secured, the exterior is not
damaged, and the reversers are stowed;
• the doors and access panels that are not in use are latched;
• the probes, vents, and static ports are clear and not damaged;
• the skin area adjacent to the pitot probes and static ports is not wrinkled;
• the antennas are not damaged;
• the light lenses are clean and not damaged.
PERF INIT page ................................................................................................................. Set
Enter the COST INDEX
Enter the RESERVERS (Reserve Fuel = Alternate Fuel + Final Reserve).
Normal Procedures
Page|6
BOEING 737NG
Captain
Enter the Estimated ZFW (Zero Fuel Weight).
Enter the CRZ ALT.
Enter the CRZ WIND.
Enter or modify the T/C OAT, if needed.
Enter or modify the TRANS ALT, if needed.
EXECute the modifications.
First Officer
DEPARTURES/ARRIVAL page.......................................................................................... Set
Select the expected or planned runway and departure routing, including transitions, if
any.
EXECute the route modifications.
Select the expected or planned approach and arrival routing, including transitions, if any.
EXECute the route modifications.
RTE 2 (if installed) .............................................................................................................. Set
Copy RTE 1, then modify as required in anticipation to runway change and/or as needed
for contingency procedures.
LEGS page ......................................................................................................................... Set
Verify the LEGS pages as needed to ensure proper waypoints sequence and compliance
with procedures constraints and to remove discontinuities, as needed.
Select RTE DATA:
Select WINDS REQUEST.
When CRZ WIND UPLINK READY shows:
Select LOAD and EXECute the modification.
Note: If datalink is not available, manually enter average wind.
Note: Until wind data is loaded, and refuelling is completed, FMC message
INSUFFICIENT FUEL message can show.
PROGRESS page 1/4 ........................................................................................................ Set
Verify distance to DEST against Flight Plan ground distance for gross error check.
PROGRESS page 4/4 ........................................................................................................ Set
Verify or enter the correct RNP for the departure.
Note: This can also be verified through the ND (Navigation Display) RNP/ANP
values.
FMC Initial Data Verification:
When returning from the exterior inspection, turn off the lights used only for this purpose and
then verify that the other pilot FMC entries are correct.
Procedure Notes:
1) The Captain and the First Officer may perform each other procedures, if the First
Officer will be the Pilot Flying. The pilot performing the Exterior Inspection has to
verify the FMC after the walk around, this ensures both pilots verify the entered data.
Normal Procedures
Page|7
BOEING 737NG
Preflight Procedure
Start the Preflight Procedures after the FMC Initial Data or the Exterior Inspection.
Captain
First Officer
Flight control panel ........................................................................................................ Check
FLIGHT CONTROL switches ...................................................................... Guard closed
Verify that the flight control LOW PRESSURE lights are illuminated.
Flight SPOILER switches ............................................................................Guard Closed
YAW DAMPER switch ..................................................................................................ON
Verify that the YAW DAMPER light is extinguished.
Verify that the standby hydraulic LOW QUANTITY light is extinguished
Verify that the standby hydraulic LOW PRESSURE light is extinguished.
Verify that the STBY RUD ON light is extinguished.
ALTERNATE FLAPS master switch ............................................................ Guard closed
ALTERNATE FLAPS position switch ......................................................................... OFF
Verify that the FEEL DIFF PRESS light is extinguished.
Verify that the SPEED TRIM FAIL light is extinguished.
Verify that the MACH TRIM FAIL light is extinguished.
Verify that the AUTO SLAT FAIL light is extinguished.
NAVIGATION panel ............................................................................................................Set
VHF NAV transfer switch ................................................................................... NORMAL
IRS transfer switch ............................................................................................ NORMAL
FMC source select switch .................................................................................. NORMAL
DISPLAYS panel ................................................................................................................Set
SOURCE selector .................................................................................................... AUTO
CONTROL PANEL select switch ....................................................................... NORMAL
Fuel panel ...........................................................................................................................Set
Verify that the ENG VALVE CLOSED lights are illuminated dim.
Verify that the SPAR VALVE CLOSED lights are illuminated dim.
Verify that the FILTER BYPASS lights are extinguished.
CROSSFEED selector ............................................................................................ Closed
Verify that the VALVE OPEN light is extinguished.
Normal Procedures
Page|8
BOEING 737NG
Captain
First Officer
FUEL PUMP switches ................................................................................................ OFF
Verify that the center tank fuel pump LOW PRESSURE lights are extinguished.
Verify that the main tank fuel pump LOW PRESSURE lights are illuminated.
Note: Whenever the APU is running and AC electrical power is on the busses, turn
on one fuel boost pump to supply fuel under pressure to the APU to extend the
service life of its fuel control unit.
CAUTION: Do not operate the center tank fuel pumps with the flight deck
unattended.
Electrical panel ...................................................................................................................Set
Verify that the BAT DISCHARGE light is extinguished.
Verify that the TR UNIT light is extinguished.
Verify that the ELEC light is extinguished.
AC/DC Meter Selector:
DC indicator in BAT.
AC indicator in STBY POWER.
BATTERY switch ......................................................................................... Guard closed
CAB/UTIL power switch (as installed) ..........................................................................ON
IFE/PASS SEAT power switch (as installed) ................................................................ON
GALLEY power switch (as installed) ............................................................................ON
STANDBY POWER switch .......................................................................... Guard closed
Verify that the STANDY PWR OFF light is extinguished.
Generator drive DISCONNECT switches ...................................................Guards closed
Verify that the DRIVE lights are illuminated.
BUS TRANSFER switch .............................................................................. Guard closed
Verify that the TRANSFER BUS OFF lights are extinguished.
Verify that the SOURCE OFF lights are extinguished.
Verify that the GEN OFF BUS lights are illuminated.
If the APU is running:
Verify that the APU LOW OIL PRESSURE light is extinguished.
Verify that the APU FAULT light is extinguished.
Verify that the APU OVERSPEED light is extinguished.
L Windshield WIPER selector ........................................................................................ PARK
Verify that the windshield wipers are stowed.
Note: do not operate the wipers on a dry windshield.
Normal Procedures
Page|9
BOEING 737NG
Captain
First Officer
EQUIP COOLING switches .......................................................................................... NORM
Verify that the OFF lights are extinguished.
EMERGENCY EXIT LIGHTS switch ................................................................. Guard closed
Verify that the NOT ARMED light is extinguished.
Passenger signs .................................................................................................................Set
NO SMOKING switch (as installed) ..............................................................................ON
FASTEN BELTS switch .............................................................................................. OFF
R Windshield WIPER selector ....................................................................................... PARK
Verify that the windshield wipers are stowed.
Note: do not operate the wipers on a dry windshield.
WINDOW HEAT switches ...................................................................................................ON
Verify that the OVERHEAT lights are extinguished.
Verify that the ON lights are illuminated (except at high ambient temperatures, when
some of the lights may not be illuminated).
Note: Position switches ON at least 10 minutes before takeoff.
PROBE HEAT switches ......................................... AUTO (as installed) or OFF (as installed)
Verify that the all lights are illuminated.
WING ANTI-ICE switch ..................................................................................................... OFF
Verify that the VALVE OPEN lights are extinguished.
ENGINE ANTI-ICE switches ............................................................................................. OFF
Verify that the COWL ANTI-ICE lights are extinguished.
Verify that the COWL VALVE OPEN lights are extinguished.
Hydraulic panel ...................................................................................................................Set
ENGINE HYDRAULIC PUMPS switches .....................................................................ON
Verify that the LOW PRESSURE lights are illuminated.
ELECTRIC HYDRAULIC PUMPS switches ............................................................... OFF
Verify that the OVERHEAT lights are extinguished.
Verify that the LOW PRESURE lights are illuminated.
High altitude landing switch (as installed) ...............................................................As needed
Verify that the INOP light is extinguished.
Voice Recorder switch (as installed) ................................................................................Auto
Air conditioning panel .........................................................................................................Set
AIR TEMPERATURE source selector ..............................................................As needed
TRIM AIR switch (as installed) .....................................................................................ON
Normal Procedures
P a g e | 10
BOEING 737NG
Captain
First Officer
Verify that the DUCT OVERHEAT (as installed) are extinguished.
Verify that the ZONE TEMP lights (as installed) are extinguished.
Temperature selectors ...................................................................................... As needed
RECIRCULATION FAN switch(es) .......................................................................... AUTO
Air conditioning PACK switches .............................................................................. AUTO
ISOLATION VALVE switch ...................................................................................... OPEN
Engine BLEED air switches ..........................................................................................ON
If the APU is ON:
APU BLEED air switch ...........................................................................................ON
Verify that the DUAL BLEED light is illuminated.
If APU is OFF:
APU BLEED air switch ......................................................................................... OFF
Verify that the DUAL BLEED light is extinguished.
Verify that the PACK TRIP OFF lights (as installed) are extinguished.
Verify that the PACK lights (as installed) are extinguished.
Verify that the WING-BODY OVERHEAT lights are extinguished.
Verify that the BLEED TRIP OFF lights are extinguished.
Cabin pressurization panel .................................................................................................Set
Verify that the AUTO FAIL light is extinguished.
Verify that the OFF SCHED DESCENT light is extinguished.
Verify that th ALTN light is extinguished.
Verify that the MANUAL light is extinguished.
FLT ALT indicator ................................................................................. Set cruise altitude
LAND ALT indicator ............................................................ Set destination field elevation
Pressurization mode selector .................................................................................. AUTO
Lighting panel .....................................................................................................................Set
Retractable LANDING lights (as installed) ....................................................... RETRACT
LANDING light switches ............................................................................................. OFF
RUNWAY TURNOFF switches................................................................................... OFF
TAXI light switch ......................................................................................................... OFF
Normal Procedures
P a g e | 11
BOEING 737NG
Captain
First Officer
ENGINE START 1 switch ................................................................................................. OFF
IGNITION select switch ......................................................................................................Set
Select IGN R for the first flight and then alternate the ignition on subsequent flights.
ENGINE START 2 switch ................................................................................................. OFF
Lighting panel .....................................................................................................................Set
LOGO light switch .............................................................................................As needed
Note: Should be on during the hours of darkness.
POSITION light switch ........................................................................................ STEADY
ANTI COLLISION light switch..................................................................................... OFF
Lights ................................................................................................................................ Test
Master LIGHTS TEST and DIM switch ..................................................................... TEST
Verify that the lights are flashing or illuminated.
Verify that all system annunciator panel lights are illuminated.
The fire warning lights are not checked during this test.
WING light switch ....................................................................................................... OFF
WHEEL WELL light switch ......................................................................................... OFF
Mode control panel .............................................................................................................Set
Master LIGHTS TEST and DIM switch............................................................ As Needed
COURSE ..........................................................................................................As needed
Note: For conventional departures, enter the first VOR radial to be intercepted.
Note: For RNAV departures, enter the departure runway heading.
EFIS control panel .............................................................................................................. Set
EFIS control panel ..............................................................................................................Set
MINS reference selector ................................................................................... As needed
MINS reference selector ...................................................................................As needed
MINS selector ................................................................................................... As needed
Note: Select the minimums for the expected approach in case of immediate return
to the departure airport and then blank the selection (this allows quick reference to
the minimums).
MINS selector ...................................................................................................As needed
Note: Select the minimums for the expected approach in case of immediate return
to the departure airport and then blank the selection (this allows quick reference to
the minimums).
FPV switch ........................................................................................................ As needed
FPV switch ........................................................................................................As needed
MTRS switch .................................................................................................... As needed
MTRS switch.....................................................................................................As needed
BARO reference selector ................................................................................. As needed
BARO reference selector ..................................................................................As needed
BARO selector ...........................................................................Set local altimeter setting
BARO selector .......................................................................... Set local altimeter setting
VOR / ADF switches ......................................................................................... As needed
VOR / ADF switches .........................................................................................As needed
Navigation Display mode selector ............................................................................. MAP
Navigation Display mode selector ............................................................................. MAP
Navigation Display CTR switch ........................................................................ As needed
Navigation Display CTR switch ........................................................................As needed
Navigation Display range selector .................................................................... As needed
Navigation Display range selector ....................................................................As needed
Navigation Display TFC switch..................................................................................... On
Navigation Display TFC switch ..................................................................................... On
Normal Procedures
P a g e | 12
BOEING 737NG
Captain
First Officer
WXR switch .................................................................................................................. Off
Verify that the weather radar indications are not shown on the ND.
WXR switch .................................................................................................................. Off
Verify that the weather radar indications are not shown on the ND.
Map switches .................................................................................................... As needed
Map switches ....................................................................................................As needed
Mode control panel ............................................................................................................. Set
COURSE .......................................................................................................... As needed
Note: For conventional departures, enter the first VOR radial to be intercepted.
Note: For RNAV departures, enter the departure runway heading.
F/D switches ................................................................................................................. ON
Note: Move the switch for the pilot flying to ON first.
A/T ARM switches ..................................................................................................... ARM
HEADING selector............................................................................................ As needed
Bank Limit selector ........................................................................................................ 25
ALTITUDE selector........................................................................................... As needed
A/P DISENGAGE bar ................................................................................................... Up
Oxygen ................................................................................................................ Test and set
Note: Advise any maintenance personnel using the FLT Interphone that a test will
be done on this communication channel.
OXYGEN MASK ....................................................................... Stowed and doors closed
Flight CREW OXYGEN Pressure Indicator ............................................................. Check
Note the oxygen pressure.
Verify that the pressure is sufficient for dispatch.
RESET/TEST switch .................................................................................. Push and hold
Verify that the yellow cross shows momentarily in the flow indicator.
RESET/TEST switch ............................................................................................ Release
Verify that the yellow cross shows does not show in the flow indicator.
Mask/Boom switch.................................................................................................... Mask
FLT INT switch .......................................................................................................... Push
SPKR switch ................................................................................................................. ON
TEST/RESET switch .................................................................................. Push and hold
EMERGENCY/Test Selector ...................................................................... Push and hold
Push-to-talk switch ..................................................................................... Push and hold
Verify oxygen flow sound is heard thought the flight deck speaker.
Normal Procedures
Oxygen................................................................................................................. Test and set
Note: Advise any maintenance personnel using the FLT Interphone that a test will
be done on this communication channel.
OXYGEN MASK ....................................................................... Stowed and doors closed
Flight CREW OXYGEN Pressure Indicator ............................................................. Check
Note the oxygen pressure.
Verify that the pressure is sufficient for dispatch.
RESET/TEST switch .................................................................................. Push and hold
Verify that the yellow cross shows momentarily in the flow indicator.
RESET/TEST switch ............................................................................................ Release
Verify that the yellow cross shows does not show in the flow indicator.
Mask/Boom switch .................................................................................................... Mask
FLT INT switch........................................................................................................... Push
SPKR switch .................................................................................................................ON
TEST/RESET switch .................................................................................. Push and hold
EMERGENCY/Test Selector ...................................................................... Push and hold
Push-to-talk switch ..................................................................................... Push and hold
Verify oxygen flow sound is heard thought the flight deck speaker.
P a g e | 13
BOEING 737NG
Captain
First Officer
Push-to-Talk switch .............................................................................................. Release
Push-to-Talk switch .............................................................................................. Release
EMERGENCY/Test Selector ................................................................................ Release
EMERGENCY/Test Selector ................................................................................ Release
TEST/RESET switch ............................................................................................ Release
TEST/RESET switch ............................................................................................ Release
Mask/Boom switch.................................................................................................. BOOM
Mask/Boom switch .................................................................................................. BOOM
TEST/RESET switch .................................................................................. Push and hold
TEST/RESET switch .................................................................................. Push and hold
EMERGENCY/Test Selector ...................................................................... Push and hold
Verify that the yellow cross shows continuously in the flow indicator.
Verify that the crew oxygen pressure does not decrease more than 100 psi.
EMERGENCY/Test Selector ...................................................................... Push and hold
Verify that the yellow cross shows continuously in the flow indicator.
Verify that the crew oxygen pressure does not decrease more than 100 psi.
EMERGENCY/Test Selector ................................................................................ Release
EMERGENCY/Test Selector ................................................................................ Release
TEST/RESET switch ............................................................................................ Release
Verify that the yellow cross does not show in the flow indicator.
Note: If the oxygen cylinder valve is not in the full open position, pressure can:
Decrease rapidly, or
Decrease more than 100 PSI, or
Increase slowly back to normal.
TEST/RESET switch ............................................................................................ Release
Verify that the yellow cross does not show in the flow indicator.
Note: If the oxygen cylinder valve is not in the full open position, pressure can:
Decrease rapidly, or
Decrease more than 100 PSI, or
Increase slowly back to normal.
Normal/100% selector .............................................................................................. 100%
Normal/100% selector .............................................................................................. 100%
Clock ................................................................................................................................... Set
Clock ...................................................................................................................................Set
TIME/DATE pushbutton ..................................................................................... UTC time
TIME/DATE pushbutton ...................................................................................... UTC time
NOSE WHEEL STEERING switch .....................................................................Guard closed
Display selector panel ........................................................................................................ Set
Display selector panel .........................................................................................................Set
MAIN PANEL DISPLAY UNITS selector ................................................................ NORM
MAIN PANEL DISPLAY UNITS selector ................................................................ NORM
LOWER DISPLAY UNIT selector ........................................................................... NORM
LOWER DISPLAY UNIT selector ........................................................................... NORM
CABIN ALTITUDE light ............................................................................. Verify extinguished
CABIN ALTITUDE light ............................................................................. Verify extinguished
TAKEOFF CONFIG light ...........................................................................Verify extinguished
TAKEOFF CONFIG light ........................................................................... Verify extinguished
Disengage light TEST switch .....................................................................................Hold to 1
Verify that the A/P light is illuminated steady amber.
Verify that the A/T light is illuminated steady amber.
Verify that the FMC light is illuminated steady amber.
Disengage light TEST switch .................................................................................... Hold to 1
Verify that the A/P light is illuminated steady amber.
Verify that the A/T light is illuminated steady amber.
Verify that the FMC light is illuminated steady amber.
Disengage light TEST switch .....................................................................................Hold to 2
Verify that the A/P light is illuminated steady red.
Verify that the A/T light is illuminated steady red.
Verify that the FMC light is illuminated steady amber.
Disengage light TEST switch .................................................................................... Hold to 2
Verify that the A/P light is illuminated steady red.
Verify that the A/T light is illuminated steady red.
Verify that the FMC light is illuminated steady amber.
STAB OUT OF TRIM light ........................................................................ Verify extinguished
Hydraulic brake pressure indicator ................................................................................ Check
Verify that the pressure is in the amber or green band.
Normal Procedures
P a g e | 14
BOEING 737NG
Captain
First Officer
Flight instruments .......................................................................................................... Check
Verify that the flight instrument indications are correct.
Verify that only these flags are shown:
TCAS OFF; and
NO VSPD until takeoff V–speeds are selected.
Verify that the flight mode annunciations are correct:
Autothrottle mode ARM; and
Roll mode is blank; and
Pitch mode is blank; and
AFDS status is FD.
Flight instruments .......................................................................................................... Check
Verify that the flight instrument indications are correct.
Verify that only these flags are shown:
TCAS OFF; and
NO VSPD until takeoff V–speeds are selected.
Verify that the flight mode annunciations are correct:
Autothrottle mode ARM; and
Roll mode is blank; and
Pitch mode is blank; and
AFDS status is FD.
Standby instruments (as installed) ................................................................................ Check
GROUND PROXIMITY panel ........................................................................................ Check
Standby horizon............................................................................................................ Set
Verify that the GPWS INOP light is extinguished.
Gyro caging control ......................................................................... Pull, then release
FLAP INHIBIT switch ...................................................................................Guard Closed
Approach mode selector ...................................................................................... OFF
Verify that the flight instrument indications are correct.
Verify that no flags are shown.
GEAR INHIBIT switch ..................................................................................Guard Closed
Standby altimeter.......................................................................................................... Set
Set local altimeter setting.
Verify that the flight instrument indications are correct.
Verify that no flags are shown.
Integrated standby flight display (as installed) ................................................................... Set
Verify that the approach mode display is blank.
Set local altimeter setting.
Verify that the flight instrument indications are correct.
Verify that no flags or messages are shown.
Standby RMI (as installed) ................................................................................................ Set
Select either VOR or ADF.
SPD BRK lever ..................................................................................................DOWN detent
Verify that the SPEED BRAKE ARMED light is extinguished.
Verify that the SPEED BRAKE DO NOT ARM light is extinguished
Verify that the SPEED BRAKE EXTENDED light is extinguished.
Note: To ensure the SPEED BRAKE is properly stowed, push down firmly on top of
the speed brake handle.
Reverse thrust levers ...................................................................................................... Down
Forward thrust levers .................................................................................................... Closed
TERRAIN INHIBIT switch (as installed) ......................................................Guard Closed
Landing gear panel .............................................................................................................Set
LANDING GEAR lever .............................................................................................. Down
Verify that the green landing gear indicator lights are illuminated.
Verify that the red landing gear indicator lights are extinguished.
Engine display control panel ...............................................................................................Set
N1 SET selector ...................................................................................................... AUTO
SPEED REFERENCE selector................................................................................ AUTO
AUTOBRAKE select switch ............................................................................................. RTO
Verify that the AUTOBRAKE DISARM light is extinguished.
ANTISKID INOP light ................................................................................ Verify extinguished
FUEL FLOW switch ............................................................................................................Set
Move switch to RESET then RATE.
Engine instruments ........................................................................................................ Check
MFD .................................................................................................................. Push ENG
Verify that the primary and secondary engine indications show existing conditions
and no exceedance.
Verify the engine oil quantity is sufficient for the flight.
Note: Minimum Engine Oil quantity is 70% or 15 quarts.
FLAP lever .................................................... Set the flap lever to agree with the flap position
Normal Procedures
P a g e | 15
BOEING 737NG
Captain
First Officer
PARKING BRAKE .............................................................................................................. Set
Verify that the PARKING BRAKE warning light is illuminated.
Note: Do not assume that the parking brake will prevent airplane movement.
Accumulator pressure can be insufficient. Check the Hydraulic Brake Pressure
Indicator.
MFD ........................................................................................................................ Push SYS
Verify the hydraulic quantity is sufficient for the flight.
Note: Confirm RF is not shown.
Engine start levers .................................................................................................... CUTOFF
STAB TRIM cutout switches ........................................................................................ Normal
WARNING: Do not key the HF radio while the airplane is being fueled. Injury to
personnel can occur.
Radio tuning panel 1 ...........................................................................................................Set
Verify that the Offside Tuning Light is extinguished (as installed).
NAV radio tuning panel 1 ....................................................................................................Set
ADF tuning panel ................................................................................................................Set
WX RDR panel ...................................................................................................................Set
Select the radar mode, tilt and gain as needed.
Note: Usually the WX+T (Weather and Turbulence) is the preferred mode, Tilt is
AUTO and the Gain is Calibrated. Select the System 1 when the Captain is the pilot
flying, or the System 2 when the First Officer.
ATC / TCAS panel ..............................................................................................................Set
XPNDR system selector ...................................................................................As needed
Note: Select the system 1 when the Captain is the pilot flying, or the system 2 when
the First Officer is the pilot flying.
ALT SOURCE ...................................................................................................As needed
Note: Select the system 1 when the Captain is the pilot flying, or the system 2 when
the First Officer is the pilot flying.
Transponder mode selector ..................................................................................... STBY
WARNING: Do not key the HF radio while the airplane is being fueled. Injury to
personnel can occur.
Radio tuning panel 2 ...........................................................................................................Set
Verify that the Offside Tuning Light is extinguished (as installed).
NAV radio tuning panel 2 ....................................................................................................Set
First officer’s audio control panel ............................................................................As needed
Captain audio control panel .................................................................................... As needed
Radio tuning panel 3 ...........................................................................................................Set
Verify that the Offside Tuning Light is extinguished (as installed).
Set or verify DATA is annunciated in the active frequency window.
STABILIZER TRIM override switch ................................................................... Guard closed
FLT DECK DOOR panel ................................................................................................ AUTO
Normal Procedures
P a g e | 16
BOEING 737NG
Captain
First Officer
WARNING: Do not put objects between the seat and the aisle stand. Injury can occur
when the seat is adjusted.
WARNING: Do not put objects between the seat and the aisle stand. Injury can occur
when the seat is adjusted.
Seat ............................................................................................................................... Adjust
Adjust the seat for optimum eye reference.
Use the handhold above the forward window for assistance when pulling the seat
forward.
Do not use the glareshield as damage can occur
Whenever the seat is adjusted, verify a positive horizontal (fore and aft) seat lock by
pushing against the seat.
Seat ................................................................................................................................ Adjust
Adjust the seat for optimum eye reference.
Use the handhold above the forward window for assistance when pulling the seat
forward.
Do not use the glareshield as damage can occur
Whenever the seat is adjusted, verify a positive horizontal (fore and aft) seat lock by
pushing against the seat.
WARNING: If the rudder pedal adjust crank is not stowed after use the rudder pedals
can move out of the desired position.
WARNING: If the rudder pedal adjust crank is not stowed after use the rudder pedals
can move out of the desired position.
Rudder pedals ............................................................................................................... Adjust
Adjust the rudder pedals to allow full rudder pedal and brake pedal movement. Stow the
rudder pedal adjust crank.
Rudder pedals ............................................................................................................... Adjust
Adjust the rudder pedals to allow full rudder pedal and brake pedal movement. Stow the
rudder pedal adjust crank.
Seat belt and shoulder harness ..................................................................................... Adjust
Seat belt and shoulder harness ..................................................................................... Adjust
Call for the “PREFLIGHT CHECKLIST”.
Do the PREFLIGHT CHECKLIST.
Procedure Notes:
1) Each pilot performs its the entire flow without synchronization to the other pilot. Blank
spaces are used only as reference to identify common procedures on both sides.
2) Synchronization is only required to complete the checklist, as indicated by the table.
Normal Procedures
P a g e | 17
BOEING 737NG
Performance Calculations Procedure
Start the Performance Calculations after the Preflight Procedures.
Captain
First Officer
Takeoff Dispatch Performance ....................................................................................................................................................................................................................................... Calculate
Each pilot should calculate the Takeoff Performance independently.
Each pilot should calculate the Takeoff Performance independently.
Takeoff Dispatch Performance ......................................................................................................................................................................................................................................... Discuss
Each pilot should explain their considerations and results.
Each pilot should explain their considerations and results.
Takeoff Dispatch Performance ............................................................................................................................................................................................................................................ Adjust
Use the one that best suits the operation or mix both as to have one final result to be
Use the one that best suits the operation or mix both as to have one final result to be
used.
used.
Takeoff Dispatch Performance ............................................................................................................................................................................................................................................ Check
Read aloud the takeoff performance results.
Verify the results are the same.
All-Engine Takeoff Performance and Immediate Return to Land Performance .................................................................................................................................................................. Check
Anytime the compliance with departure gradient is in doubt (high climb gradients, high
Anytime the performance in case of an immediate return to the departure airport is in
altitude constraints, high elevation, high temperature and/or high takeoff weight),
doubt (short runway, high elevation, high temperature and/or high takeoff weight),
calculate the All-Engine Takeoff Performance and/or other approved source.
calculate the Landing En-Route Performance and/or other approved source.
Procedure Notes:
1) Be conservative on the performance calculations to avoid last minute modifications
due to weather change. Consider no wind or increase the tailwind, increase the
temperature and/or reduce the atmospheric pressure, if performance allows.
2) When required, after the All Engine Takeoff Performance and the Landing En-Route
Performance for and Immediate Return to Land are calculated, the pilots should
discuss the results and anticipate the required aircraft configuration and/or
alternative procedure.
Normal Procedures
P a g e | 18
BOEING 737NG
Refueling Procedures
After refueling is completed.
Captain
First Officer
Quantity and Distribution ..................................................................................................................................................................................................................................................... Check
Verify that the fuel in the tanks and their distribution are correct using the Fuel Quantity
Indicators.
FMC fuel quantity................................................................................................................................................................................................................................................................. Check
Verify that the fuel in the tanks matches the FMC fuel.
Use the FMC PROGress page 1/4 to check the DESTination ETA and arrival FUEL.
Normal Procedures
P a g e | 19
BOEING 737NG
ATC Clearance Procedures
Obtain the clearance as soon as possible, according to the local regulations.
Captain
First Officer
ATC Clearance ............................................................................................................. Obtain
Readback or accept the clearance.
ATC Clearance .................................................................................................................................................................................................................................................................... Check
Verify or modify the MCP and the FMC to comply with the instructions.
Verify or modify the radios to comply with the instructions.
Procedure Notes:
1) If voice clearance procedures are in use, both pilots must copy the clearance.
2) MCP verification or modification includes arming LNAV (if applicable), initial heading
and altitude/flight level.
3) FMC verification or modification includes destination, departure runway, departure
procedure, route and cruise level.
4) Radios verification or modification includes navigations radios, communication
radios and transponder.
Normal Procedures
P a g e | 20
BOEING 737NG
Taxi and Takeoff Briefings
Perform the Taxi and Takeoff Briefing after the ATC Clearance Procedures.
Captain
First Officer
Briefing .............................................................................................................................................................................................................................................................................. Perform
If late ATC clearance is expected, at the captain's discretion, briefings may be given
before clearance is obtained. In that case, update the briefings accordingly, following
the ATC clearance procedures.
Procedure Notes:
1) The takeoff briefing is a description of the expected ground maneuvers, the
departure flight path with emphasis on anticipated track and altitude restrictions and
the engine out departure procedure (if applicable). Additional briefing items may be
required when any element of the takeoff and/or departure is different from those
routinely used. These may include: adverse weather, adverse taxiways and runway
conditions, noise abatement requirements, terrain and/or obstacles, dispatch using
the Minimum Equipment List and any other situation where it is necessary to review
or define crew responsibilities.
Normal Procedures
P a g e | 21
BOEING 737NG
Performance Entry Procedure
Start the Performance Entry Procedure after the Load Sheet is on board.
Captain
First Officer
Performance Calculations ................................................................................................................................................................................................................................................... Check
Verify or modify the performance calculation, as needed.
Verify or modify the performance calculation, as needed.
PERF INIT page ...................................................................................................................................................................................................................................................................... Set
Verify or enter the AZFW.
Verify the FUEL.
Compare the FMC FUEL minus the taxi fuel with the TOF on load sheet.
Verify the GR WT.
Compare the FMC Gross Weight minus the taxi fuel with the ATOW on load sheet.
Note: All discrepancies between the load sheet and FMC weights must be resolved.
CAUTION: Any CDU messages such as MAX ALT FLXXX must be resolved.
THRUST LIM page .................................................................................................................................................................................................................................................................. Set
Select or verify the Takeoff Thrust.
Enter the Assumed Temperature, if any.
Note: Compare the FMC calculated N1 and the Performance calculated N1. Any
major discrepancy must be resolved.
Select or verify the Climb Thrust.
TAKEOFF REF page 1/2 ......................................................................................................................................................................................................................................................... Set
Enter the Takeoff CG.
Enter the Takeoff Flap Setting.
Enter the V1.
Enter the VR.
Enter the V2.
IAS / MACH selector ................................................................................................................................................................................................................................................................ Set
Enter the V2.
TAKEOFF REF page 2/2 ......................................................................................................................................................................................................................................................... Set
Verify or enter the Engine-Out Acceleration Height (EO ACCEL HT).
Verify or enter the Acceleration Height (ACCEL HT).
Verify or enter the Thrust Reduction Height (THR REDUCTION).
VNAV switch ............................................................................................................................................................................................................................................................................ Set
Arm the VNAV, as needed.
APPROACH REF page ....................................................................................................................................................................................................................................................... Check
Verify the FLAPS 40º VREF speed matches the performance calculated VREF40.
Normal Procedures
P a g e | 22
BOEING 737NG
Before Start Procedure
Start the Before Start Procedure when ready to close the aircraft doors.
Captain
First Officer
Documents and papers ....................................................................................................................................................................................................................................................... Check
Verify all the required documents and papers are completed and signed.
ELECTRICAL panel ............................................................................................................Set
APU (as needed) ....................................................................................START, then ON
When APU GEN OFF BUS light is illuminated:
APU GENERATOR bus switches ....................................................................ON
Verify that the SOURCE OFF lights are extinguished.
Verify that the TRANSFER BUS OFF lights are extinguished.
Verify that the STANDBY PWR OFF light is extinguished.
APU BLEED air switch .....................................................................................ON
Note: Run the APU for one minute before using it as pneumatic air source.
Flight deck door ......................................................................................... Closed and locked
Verify that the LOCK FAIL light is extinguished.
Flight deck windows .................................................................................. Closed and locked
Verify that the window is locked by firmly pulling the handle.
Flight deck windows ................................................................................... Closed and locked
Verify that the window is locked by firmly pulling the handle.
MCP ......................................................................................................................................................................................................................................................................................... Set
Verify or set V2 on the IAS / MACH selector.
Verify or arm the LNAV, as needed.
Verify or arm the VNAV, as needed.
Verify or set initial heading or track on the HDG / TRK selector.
Verify or set initial altitude on the ALTITUDE selector.
FMC display ............................................................................................................................................................................................................................................................................. Set
If Pilot Flying:
If Pilot Flying:
Select the TAKEOFF REF page or VNAV CLB page.
Select the TAKEOFF REF page or VNAV CLB page.
If Pilot Monitoring
If Pilot Monitoring
Select the LEGS page.
Select the LEGS page.
Exterior doors ...................................................................................................................................................................................................................................................................... Check
Verify that the exterior doors are closed.
Establish communications with the ground personnel:
Verify the external checks are complete.
If pushback is needed:
Confirm the nose gear steering is locked out.
Verify ground equipment is ready for pushback.
Obtain clearance to pressurize the hydraulic system.
Normal Procedures
P a g e | 23
BOEING 737NG
Captain
First Officer
Fuel Panel ...........................................................................................................................Set
AFT and FORWARD FUEL PUMP switches ................................................................ON
Verify that the LOW PRESSURE lights are extinguished.
If the center tank fuel quantity exceeds 460 kilograms:
Trim ..................................................................................................................................... Set
Verify each trim for freedom of movement.
Stabilizer trim:
Set the trim for takeoff.
Verify that the trim is in the green band.
Aileron trim:
Set the trim to 0 units.
Rudder trim:
Set the trim to 0 units.
LEFT and RIGHT CENTER FUEL PUMP switches ...............................................ON
Verify that LOW PRESSURE lights illuminate momentarily and then extinguish.
If the center tank fuel quantity is less than 1.000 kilograms
LEFT and RIGHT CENTER FUEL PUMP switches ....................................... OFF
FASTEN BELTS switch ......................................................................................................ON
HYDRAULIC PANEL ..........................................................................................................Set
Electric HYDRAULIC PUMP switches ..........................................................................ON
Verify that the electric pump LOW PRESSURE lights are extinguished.
Verify that the brake accumulator pressure is 2.800 psi minimum.
ANTI COLLISION light switch .............................................................................................ON
Transponder Mode Selector .......................................................................................... STBY
Call for the “BEFORE START CHECKLIST”.
Do the BEFORE START CHECKLIST.
Normal Procedures
P a g e | 24
BOEING 737NG
Pushback or Towing Procedure
Start the Pushback or Towing Procedure after the Before Start Procedure.
Captain
First Officer
Request ATC clearance for Pushback (and Engine Start), as needed.
CAUTION: Do not hold or turn the nose wheel tiller during pushback or towing. This
can damage the nose gear or the tow bar.
CAUTION: Do not use airplane brakes to stop the airplane during pushback or
towing. This can damage the nose gear or the tow bar.
Parking brake.....................................................................................................Set or release
Set or release as directed by ground personnel.
When pushback or towing is complete:
Confirm the tow bar is disconnected.
Confirm the nose gear steering is not locked out.
Normal Procedures
P a g e | 25
BOEING 737NG
Engine Start Procedure
The Engine Start procedure may be done during pushback or towing.
Captain
First Officer
Engine start requirements ................................................................................................................................................................................................................................................... Check
Start Attempts:
Multiple consecutive start attempts are permitted;
Each start attempt has a limit of 2 minutes of starter usage;
A minimum of 10 seconds is needed between start attempts;
Do the ABORTED ENGINE START checklist if one or more of the following abort start
conditions occur:
The N1 or N2 does not increase or increases very slowly after the EGT increases;
There is no oil pressure indications by the time that the engine is stable at IDLE;
The EGT does not increase by 15 seconds after the engine start lever is moved to
IDLE;
The EGT quickly nears or exceeds the start limit.
Engine start recommendations ............................................................................................................................................................................................................................................ Check
Engine Start Lever:
Do not move an engine start lever to IDLE early or a hot start can occur;
Keep a hand on the engine start lever while monitoring RPM, EGT and FUEL FLOW,
until stable;
If fuel is shut off accidentally (by closing the engine start lever) do not reopen the
engine start lever in an attempt to restart the engine.
Engine Start Switch
Failure of the ENGINE START switch to stay in GRD until the starter cutout can
cause a hot start. Do not re-engage the ENGINE START switch until engine RPM
is below 20% N2.
Ignition:
For the first flight of the day, at airport elevations at or above 2.000 feet MSL, if the
temperature is below 5ºC / 41ºF, consider placing the Ignition select switch in
BOTH before starting the engines. This may increase the likelihood of a
successful engine start on the first attempt.
Request ATC clearance for Engine Start, as needed.
Engine instruments ........................................................................................................ Check
MFD .................................................................................................................. Push ENG
Verify that the secondary engine indications are shown.
Announce “START SEQUENCE (2) THEN (1)”.
Obtain clearance to start the engines with ground personnel.
Call “START (2) ENGINE”.
Air conditioning PACK switches ....................................................................................... OFF
Normal Procedures
P a g e | 26
BOEING 737NG
Captain
First Officer
ENGINE START (2) switch .............................................................................................. GRD
Clock ................................................................................................................................... Set
Chronometer .............................................................................................................. Start
Monitor starter duty cycle time.
N2 (starting engine) ............................................................................................................................................................................................................................................................. Check
Verify that the N2 RPM increases.
Verify that the N2 RPM increases.
When:
At:
There is N1 rotation (starting engine) AND
25% N2* (starting engine)
.
*If N2 at 25% is not possible (starting engine):
At maximum motoring and N2 at least 20% (starting engine)
Note: Maximum motoring occurs when N2 acceleration is less than 1% in
approximately 5 seconds.
Engine start lever (2) ....................................................................................................... IDLE
Clock ................................................................................................................................... Set
Chronometer .............................................................................................................. Start
Monitor time to EGT rise.
Engine indications (starting engine) .................................................................................................................................................................................................................................... Check
Monitor N1, N2, EGT, fuel flow and oil pressure.
Monitor N1, N2, EGT, fuel flow and oil pressure.
Announce any abnormal indications.
Announce any abnormal indications.
At:
56% N2 (starting engine)
.
Verify that the ENGINE START (2) switch moves to OFF automatically.
If the ENGINE START (2) switch does not move to OFF automatically:
ENGINE START (2) switch......................................................................................... OFF
Verify that the START VALVE OPEN (2) alert extinguishes and announce: “STARTER
CUTOUT”.
When:
The starting engine is stable at idle
.
Call “START (1) ENGINE”.
ENGINE START (1) switch .............................................................................................. GRD
Clock ................................................................................................................................... Set
Chronometer .............................................................................................................. Start
Monitor starter duty cycle time.
Normal Procedures
P a g e | 27
BOEING 737NG
Captain
First Officer
N2 (starting engine) ............................................................................................................................................................................................................................................................. Check
Verify that the N2 RPM increases.
Verify that the N2 RPM increases.
When:
At:
There is N1 rotation (starting engine) AND
25% N2* (starting engine)
.
*If N2 at 25% is not possible (starting engine):
At maximum motoring and N2 at least 20% (starting engine)
Note: Maximum motoring occurs when N2 acceleration is less than 1% in
approximately 5 seconds.
Engine start lever (1) ....................................................................................................... IDLE
Clock ................................................................................................................................... Set
Chronometer .............................................................................................................. Start
Monitor time to EGT rise.
At:
56% N2 (starting engine)
.
Verify that the ENGINE START (1) switch moves to OFF automatically.
If the ENGINE START (1) switch does not move to OFF automatically:
ENGINE START (1) switch......................................................................................... OFF
Verify that the START VALVE OPEN (1) alert extinguishes and announce: “STARTER
CUTOUT”.
When:
Both engines are stable at idle
.
Dismiss the ground personnel.
Normal Procedures
P a g e | 28
BOEING 737NG
Before Taxi Procedure
Start the Before Taxi Procedure after the Pushback and Engine Start Procedure.
Captain
First Officer
Call “FLAPS (1/2/5/10/15/25)”, as needed for takeoff.
Flap lever ....................................................................................................... Set takeoff flaps
Verify that the LE FLAPS EXT green light is illuminated.
GENERATOR 1 and 2 switches .........................................................................................ON
PROBE HEAT switches ........................................... AUTO (as installed) or ON (as installed)
WING ANTI-ICE switch ...........................................................................................As needed
ENGINE ANTI-ICE switches ...................................................................................As needed
Announces “FLIGHT CONTROLS” and check the flight controls.
Make slow and deliberate inputs, one direction at a time.
Move the control wheel and the control column to full travel in both directions and verify:
Freedom of movement; and
That the controls return to center.
PACK switches .............................................................................................................. AUTO
ISOLATION VALVE switch ............................................................................................ AUTO
APU BLEED air switch ...................................................................................................... OFF
APU switch........................................................................................................................ OFF
ENGINE START switches ............................................................................................. CONT
Engine instruments ........................................................................................................ Check
MFD .................................................................................................................. Push ENG
Verify the Secondary Engine indications are blank.
CAUTION: Verify that the ground equipment is clear and ground personnel has
disconnected prior to carrying out rudder check.
Announces “RUDDER”.
Hold the nose wheel tiller during the rudder check to prevent nose wheel movement.
Move the rudder pedals to full travel in both directions and verify:
Freedom of movement; and
That the rudder pedals return to center.
Follow the rudder check physically with the feet to ensure proper pedal adjustment position.
Recall ............................................................................................................................. Check
Announce: “RECALL”
System Annunciator Panel ........................................................................................ Push
Verify that all system annunciator panel lights illuminate and then extinguish.
Call for the “BEFORE TAXI CHECKLIST.”
Do the BEFORE TAXI CHECKLIST.
Normal Procedures
P a g e | 29
BOEING 737NG
Taxi Procedure
Start the Taxi Procedure after the Before Taxi Procedure.
Pilot Flying
Pilot Monitoring
Request taxi clearance, as needed.
Confirm the taxi clearance and update the briefing, as needed.
TAXI light switch .................................................................................................................ON
Parking brake.............................................................................................................. Release
Verify that the PARKING BRAKE warning light is extinguished.
Every Time:
The aircraft has to be brought to a halt
.
PARKING BRAKE .............................................................................................................. Set
Verify that the PARKING BRAKE warning light is illuminated.
Announce “PARKING BRAKE SET”.
Verify that the PARKING BRAKE warning light is illuminated and announce “CHECKED”.
TAXI light switch ............................................................................................................... OFF
Follow the procedure from the beginning to start the taxi again.
Every Time Before:
Crossing an active runway during taxi
.
LANDING light switches .....................................................................................................ON
RUNWAY TURNOFF light switches ...................................................................................ON
POSITION light switch ...................................................................... STROBE AND STEADY
Transponder mode selector .......................................................................................... TA/RA
Verify TFC is shown on the ND.
Every Time After:
Crossing an active runway during taxi
.
LANDING light switches ................................................................................................... OFF
RUNWAY TURNOFF light switches ................................................................................. OFF
POSITION light switch .............................................................................................. STEADY
Transponder mode selector ........................................................................................ XPNDR
Verify that TCAS OFF is shown on the ND and announce “TCAS OFF”.
Normal Procedures
P a g e | 30
BOEING 737NG
Before Takeoff Procedure
Start the Before Takeoff Procedure when clear of close proximity obstacles.
Pilot Flying
Pilot Monitoring
Engine warm up requirements............................................................................................................................................................................................................................................. Check
Engine oil temperature must be above the bottom of the temperature scale.
Run the engines for at least 5 minutes before takeoff when grounded for more than 5
hours.
Engine warm up recommendations ..................................................................................................................................................................................................................................... Check
Run the engines for at least 2 minutes; and
Use a thrust setting normally used for taxi operations.
Update changes to the takeoff briefing, as needed.
Takeoff Review ................................................................................................................................................................................................................................................................. Perform
Call for: “Takeoff Review”.
Verify and announce the FMA modes and selections according to the following
sequence: Autothrottle (including the speed), Roll Mode (including the heading),
Pitch Mode (including the altitude) and AFDS Status.
For example:
“Autothrottle: ARM, with V2 132”;
“Roll Mode: LNAV armed, with Initial Heading 097”;
“Pitch Mode: VNAV armed, with Initial Altitude 19.000”;
“Flight Director ON”.
Note: When there are no armed modes, only announce the MCP selections.
If the selections are desired:
Announce: “Checked”.
If the selections are not desired:
Request desired changes in MCP and start the Takeoff Review from the beginning.
After:
Receiving CABIN READY for departure
.
WXR radar display .............................................................................................................. ON
Verify WX+T (or WXR) is shown on the ND.
TERR display ......................................................................................................................ON
Verify TERR is shown on the ND.
Call for the “BEFORE TAKEOFF CHECKLIST”.
Do the BEFORE TAKEOFF CHECKLIST.
Procedure Notes:
1) Takeoff review is designed to address AFDS changes after Preflight Scan due to
lack of system monitoring during flight preparation, to ensure proper FD guidance
after takeoff.
Normal Procedures
P a g e | 31
BOEING 737NG
Takeoff Procedure
Start the Takeoff Procedure before entering the runway for departure.
Pilot Flying
Pilot Monitoring
Runway Environment .......................................................................................................................................................................................................................................................... Check
Before entering the departure runway, verify that the runway and runway entry point
CAUTION: Do NOT cross any red light, even when cleared to do so, unless an
are correct. Use all available means to verify the correct position (taxiway and
explicit instruction to ignore it has been received and confirmed with ATC.
runway markings, sign and lights, charts, moving maps, navigation displays).
When:
Entering the departure runway
.
RUNWAY TURNOFF light switches ...................................................................................ON
POSITION light switch ...................................................................... STROBE AND STEADY
Notify the cabin crew: “CABIN CREW, PREPARE FOR TAKEOFF”.
Transponder mode selector .......................................................................................... TA/RA
Verify TFC is shown on the ND.
When:
Cleared for Takeoff
.
LANDING lights switches ....................................................................................................ON
Announce “TAKEOFF”.
Advance the thrust levers to approximately 40% N1.
Allow the engines to stabilize.
TO/GA switch................................................................................................................... Push
Verify that the thrust increases and call “SET TAKEOFF THRUST”.
Engine Instruments ...................................................................................................... Monitor
Monitor the engine instruments during the takeoff. Announce any abnormal indications.
Adjust takeoff thrust before 60 knots, as needed.
During strong headwinds, if the thrust levers do not advance to the planned takeoff thrust,
manually advance the thrust levers by 60 knots.
When:
Correct takeoff thrust is set
.
Announce “THRUST SET”.
If the First Officer is the Pilot Flying, the Captain takes over the control of the thrust levers.
Airspeed ............................................................................................................................................................................................................................................................................. Monitor
Normal Procedures
P a g e | 32
BOEING 737NG
Pilot Flying
Pilot Monitoring
Maintain light forward pressure on the control column until 80 knots.
At:
80 knots indicated airspeed
.
Announce “EIGHTY KNOTS”.
Verify 80 knots and announce “CHECKED”.
Verify that the autothrotlle THR HLD mode engages.
If the autothrottle THR HLD mode fails to engage:
Announce: “THR HLD FAILED”.
If the autothrottle THR HLD mode fails to engage:
A/T disconnect switch ................................................................................................ Push
If disconnecting the A/T was necessary:
Verify that the A/T mode blanks and announce: “Autothrottle BLANK”.
At:
V1 speed
.
Verify the automatic V1 callout or announce “V1.”
Verify V1 speed.
The Captain removes the hand from the thrust levers.
At:
VR speed
.
Call “ROTATE”.
Rotate towards 15° pitch attitude.
After liftoff, follow F/D commands.
Establish a positive rate of climb.
Monitor airspeed and vertical speed.
Verify a positive rate of climb on the altimeter and announce: “POSITIVE RATE.”
Verify a positive rate of climb on the altimeter and call: “GEAR UP.”
Landing gear lever .............................................................................................................. UP
If LNAV is armed for departure, the mode is engaged automatically at 50’ RA.
Engage the autopilot anytime when at or above the minimum altitude for autopilot.
When Above:
400 feet radio altitude
.
Verify, select or call for a roll and a pitch modes, as needed.
Select or verify the roll and pitch modes, as needed.
Normal Procedures
P a g e | 33
BOEING 737NG
At:
Thrust reduction height
.
Thrust Limit .......................................................................................................................................................................................................................................................................... Check
Verify that climb thrust is set.
Verify that climb thrust is set.
At:
Acceleration height
.
Verify acceleration to or set the desired speed.
Flap retraction ................................................................................................................................................................................................................................................................... Perform
Request for flaps retraction according to the flap retraction schedule.
Retract flaps according to the flap retraction schedule.
Note: Flap Retraction Speed Schedule is described after the Takeoff Procedure.
After:
Flap retraction complete
.
Call for the “AFTER TAKEOFF CHECKLIST”.
PACKS ........................................................................................................................... AUTO
ENGINE BLEEDS ...............................................................................................................ON
Engine Start Switches .............................................................................................As needed
Landing gear .............................................................................................................. Up & Off
Auto Brake ........................................................................................................................ OFF
Do the AFTER TAKEOFF CHECKLIST.
Normal Procedures
P a g e | 34
BOEING 737NG
Flap Retraction Speed Schedule
Takeoff Flaps
25
15 or 10
5
1
Normal Procedures
At Speed
Command Speed
Select Flaps
V2 + 15KT
“15” or above
15
“15”
“5” or above
5
“5”
“1” or above
1
“1”
“UP” or above
UP
V2 + 15KT
“5” or above
5
“5”
“1” or above
1
“1”
“UP” or above
UP
V2 + 15KT
“1” or above
1
“1”
“UP” or above
UP
“1”
“UP” or above
UP
P a g e | 35
BOEING 737NG
Climb and Cruise Procedure
Start the the Climb and Cruise Procedure after the Takeoff Procedure.
Pilot Flying
Pilot Monitoring
During climb and cruise, verify the RNP as needed.
When:
Passing through the Minimum Safe Altitude
.
Announce: “MSA”.
Verify minimum safe altitude on the altimeter and announce: “CHECKED”.
WXR switch...................................................................................................................... Push
Verify WX+T (or WXR) is shown on the ND.
Note: TERR can be selected anytime the terrain is a factor and/or can improve
situational awareness.
At:
10,000' MSL (20,000’ MSL for aerodrome elevation above 5,000’) and climbing above
.
Announce: “TEN THOUSAND” (“TWENTY THOUSAND”).
Verify ten (twenty) thousand feet on the altimeter and announce: “CHECKED”.
PASS SIGNS panel ............................................................................................................Set
NO ELECTRONICS selector (if installed) ............................................................... AUTO
FASTEN BELTS selector ........................................................................................ AUTO
Note: During the flight, above 10,000’ MSL (20,000’ MSL for aerodrome elevation
above 5,000’), the seat belts sign should be ON anytime turbulent air is present or
anticipated. The captain retains the final decision about the switch operation for this
purpose.
LANDING light switches ................................................................................................... OFF
RUNWAY TURNOFF light switches ................................................................................. OFF
TAXI light switch ............................................................................................................... OFF
LOGO light switch ............................................................................................................. OFF
When:
Approaching and climbing above transition altitude
.
Announce: “TRANSITION ALTITUDE”.
Note: If climbing to a Flight Level close spaced to the Transition Altitude and the rate
of climb is high, announce it soon enough to complete the altimeter reference change
prior to starting the level off maneuver.
Verify the transition altitude is approaching and call: “SET STANDARD”.
Normal Procedures
P a g e | 36
BOEING 737NG
Pilot Flying
Pilot Monitoring
BARO STD switch ........................................................................................................... Push
Verify STD shows as reference for the altimeter.
BARO STD switch ........................................................................................................... Push
Verify STD shows as reference for the altimeter.
Integrated standby flight display .........................................................................................Set
BARO selector ........................................................................................................... Push
Verify STD shows as reference for the standby altimeter.
Announce: “STANDARD SET”.
If:
There is fuel in the center tank
.
CENTER FUEL PUMP switches.........................................................................................ON
If:
The center fuel pump LOW PRESSURE light illuminates or the center fuel tank is empty
.
CENTER FUEL PUMP switches....................................................................................... OFF
After:
Reaching cruise level
.
Perform the Cruise Briefing, as needed.
Note: If the wind was manually entered during the FMC Initial Data and the cruise
level flight time is greater than one hour:
Verify or modify the wind at next waypoint and then at waypoints where the wind
direction and/or speed changes by more than 30 degrees or 10 knots.
Procedure Notes:
1) The procedure is design with this sequence because in the US (the state of
manufacture of the airplane) the local altimeter setting is used until 18,000’ MSL.
This ensures that the Takeoff Procedure can be completed, before the start of the
Climb and Cruise Procedures. At places with lower Transition Altitudes (especially
when below 10,000’ MSL), the sequence of actions should be handled accordingly.
Normal Procedures
P a g e | 37
BOEING 737NG
Descent Procedure
Start the Descent Procedure before the airplane descends below the cruise altitude for
arrival at destination.
Pilot Flying
Pilot Monitoring
Verify the RNP, as needed during the descent.
Obtain the ATIS or weather and operational information.
Modify the active route for the arrival and approach as needed.
Verify that pressurization is set to landing altitude.
Recall ............................................................................................................................. Check
Announce: “RECALL”
System Annunciator Panel ........................................................................................ Push
Verify that all system annunciator panel lights illuminate and then extinguish.
Discuss any inoperative item, as needed.
Discuss any operational notes, as needed.
EFIS control panel .............................................................................................................. Set
EFIS control panel ..............................................................................................................Set
MINS reference selector ......................................................................... RADIO or BARO
MINS reference selector ......................................................................... RADIO or BARO
MINS selector ................................................................................................... As needed
MINS selector ...................................................................................................As needed
BARO reference selector .................................................................................. IN or HPA
BARO reference selector ................................................................................... IN or HPA
BARO selector ......................................................................Preset local altimeter setting
BARO selector ..................................................................... Preset local altimeter setting
COURSE ................................................................................................................ As needed
Note: For instrument approaches, enter the final approach course.
Note: For visual approaches, enter the arrival runway heading.
COURSE.................................................................................................................As needed
Note: For instrument approaches, enter the final approach course.
Note: For visual approaches, enter the arrival runway heading.
Check the landing performance.
AUTOBRAKE selector ............................................................................................ As needed
FMC APPROACH REF page..............................................................................................Set
Enter the expected landing weight.
Verify and select the landing flaps and VREF speeds.
NAV radio tuning panel 1 and 2 ..........................................................................................Set
ADF tuning panel ................................................................................................................Set
Perform the Descent Briefing.
Call for the “DESCENT CHECKLIST.”
Do the DESCENT CHECKLIST.
Normal Procedures
P a g e | 38
BOEING 737NG
Approach Procedure
The Approach Procedure is normally started at Transition Level.
Pilot Flying
Pilot Monitoring
Verify the RNP, as needed during the arrival and approach.
When:
Cleared and descending to an altitude
.
Announce: “TRANSITION LEVEL”.
Note: If complying with a level restriction above the transition level, only change the
altimeter subscale to the local altimeter setting when this restriction is met.
Verify the transition level and call: “SET QNH ____ (ALTIMETER ____)”.
Note: Call for the actual local altimeter setting numbers. Even if the local pressure
met the ISA conditions, call for 1013.
BARO STD switch ........................................................................................................... Push
Verify the local altimeter setting shows as reference for the altimeter.
Integrated standby flight display .........................................................................................Set
BARO STD switch ........................................................................................................... Push
Verify the local altimeter setting shows as reference for the altimeter.
BARO selector ........................................................................................................... Push
Verify the local altimeter setting shows as reference for the standby altimeter.
Announce: “____ SET”.
Note: Announce the actual local altimeter setting numbers. Even if the local pressure
met the ISA conditions, announce 1013.
When:
Reaching 10,000' MSL (20,000’ MSL for aerodrome elevation above 5,000’)
.
Announce: “TEN THOUSAND” (“TWENTY THOUSAND”).
Verify ten (twenty) thousand feet on the altimeter and announce: “CHECKED”.
PASS SIGNS panel ............................................................................................................Set
NO ELECTRONICS selector (if installed) ....................................................................ON
FASTEN BELTS selector .............................................................................................ON
LANDING light switches .....................................................................................................ON
RUNWAY TURNOFF light switches ...................................................................................ON
TAXI light switch .................................................................................................................ON
LOGO light switch ...................................................................................................As needed
Notify the cabin crew: “CABIN CREW, PREPARE FOR LANDING”.
Normal Procedures
P a g e | 39
BOEING 737NG
Pilot Flying
Pilot Monitoring
Call for the “APPROACH CHECKLIST”.
Do the APPROACH CHECKLIST.
When:
Passing through the Minimum Safe Altitude
.
Announce: “MSA”.
Verify minimum safe altitude on the altimeter and announce: “CHECKED”.
TERR switch .................................................................................................................... Push
Verify TERR is shown on the ND.
Procedure Notes:
1) The procedure is design with this sequence because in the US (the state of
manufacture of the airplane) the standard altimeter setting is used above 18,000’
MSL. This ensures that the Approach Procedure can be completed, before the start
of the ILS or VNAV Procedures. At places with lower Transition Levels (especially
when below 10,000’ MSL), the sequence of actions should be handled accordingly.
Normal Procedures
P a g e | 40
BOEING 737NG
Flap Extension Speed Schedule
Current Flap Position
At Speed
Select Flaps
Command Speed
UP
“UP”
1
“1”
1
“1”
5
“5”
5
“5”
15
“15”
15
“15”
30 or 40
(VREF30 or VREF40) + Wind additives
Normal Procedures
P a g e | 41
BOEING 737NG
ILS Procedure
The ILS Procedure is normally started at the IAF or the beginning of radar vectors.
Pilot Flying
Pilot Monitoring
If on radar vectors:
Use HDG SEL and the pitch mode as needed.
If enroute to a fix
Use LNAV or other roll mode and VNAV or other pitch mode.
Plan to intercept the localizer with Flaps 5 and at Flaps 5 speed.
Speed reduction................................................................................................................................................................................................................................................................... Check
Verify reduction to or set the desired speed.
Flap extension .................................................................................................................................................................................................................................................................. Perform
Request for flaps extension according to the flap extension schedule.
Extend flaps according to the flap retraction schedule.
Note: Flap Extension Speed Schedule is described after the Approach Procedure.
When:
On localizer intercept heading
.
ILS signal ............................................................................................................................................................................................................................................................................. Check
Verify that the ILS is tuned and identified; and
Verify that the ILS is tuned and identified; and
Verify that the LOC and G/S pointers are shown in the proper position.
Verify that the LOC and G/S pointers are shown in the proper position.
APP mode ......................................................................................................................... Arm
WARNING: When using LNAV to intercept the final approach course, LNAV might
parallel the localizer without capturing it.
Use LNAV or HDG SEL to intercept the final approach course as needed.
When:
On localizer
.
Localizer tracking ................................................................................................................................................................................................................................................................. Check
Verify that the localizer is captured; and
Verify that the localizer is captured; and
Set the final approach course heading on the heading selector.
Verify the final approach course heading is set on the heading selector.
At:
Glideslope alive
.
Call “GEAR DOWN, FLAPS 15”; and
Speedbrake lever........................................................................................................ ARMED
Landing gear lever .............................................................................................................. DN
Flap lever ............................................................................................................................. 15
ENGINE START switches ............................................................................................. CONT
Normal Procedures
P a g e | 42
BOEING 737NG
Pilot Flying
Pilot Monitoring
At:
Glideslope capture
.
Call “FLAPS (30/40)”, as needed for landing.
Flap lever ........................................................................................................... Landing flaps
Missed approach altitude .................................................................................................... Set
Call for the “LANDING CHECKLIST”.
Do the LANDING CHECKLIST.
At:
Final approach fix
.
FAF Crossing Altitude .......................................................................................................................................................................................................................................................... Check
Verify the crossing altitude on the altimeters. Be aware of the temperature deviation to the
standard atmosphere and its relation to the indicated altitude when following the Glide
Slope.
Announce: “APPROACH FIX, ____”.
Note: Announce the final approach fix altitude as depicted on the approach
procedure chart.
Announce: “CHECKED”.
WARNING: Interference with the glideslope signal can result in erroneous AFDS
pitch guidance indicated by FMA mode degradation, the AUTOPILOT caution
message, and removal of the F/D pitch bar. If this occurs, do a go-around unless
suitable visual references can be established and maintained.
Approach ........................................................................................................................................................................................................................................................................... Monitor
Both pilots must monitor the approach. Call out any significant deviations. Perform an
immediate go-around if not within the criteria to continue the approach.
If the Autopilot is Engaged, At:
500 feet radio altitude
.
Autoland Status ................................................................................................................................................................................................................................................................... Check
Verify the autoland status.
Announce: “(CMD/SINGLE CHANNEL/LAND 2/LAND 3/NO AUTOLAND)”.
Announce: “CHEKED”.
If an ILS CAT3B is being conducted, At:
200 feet radio altitude
.
Announce: “ALERT HEIGHT”.
Announce: “CHEKED”.
Normal Procedures
P a g e | 43
BOEING 737NG
VNAV Procedure
The VNAV Procedure is normally started at the IAF or the beginning of radar vectors.
Pilot Flying
Pilot Monitoring
If on radar vectors:
Use HDG SEL and the Pitch mode as needed.
If enroute to a fix
Use LNAV or other roll mode and VNAV or other pitch mode.
Plan to intercept the final approach course with Flaps 5 and at Flaps 5 speed.
Speed reduction................................................................................................................................................................................................................................................................... Check
Verify reduction to, set or request for the desired speed.
Verify reduction to or set the desired speed.
Flap extension .................................................................................................................................................................................................................................................................. Perform
Request for flaps extension according to the flap extension schedule.
Extend flaps according to the flap retraction schedule.
Note: Flap Extension Speed Schedule is described after the Approach Procedure.
When:
On final approach course intercept heading
.
For LOC, LOC-BC, or LDA approaches:
LOC signal ..................................................................................................................................................................................................................................................................... Check
Verify that the localizer is tuned and identified; and
Verify that the localizer is tuned and identified; and
Verify that the LOC pointer is shown in the proper position.
Verify that the LOC pointer is shown in the proper position.
LNAV or LOC mode .......................................................................................................... Arm
Note: The recommended roll mode for the final approach is LNAV.
Note: LOC is also recommended for a Localizer or LDA Approaches.
WARNING: When using LNAV to intercept the localizer final approach course, LNAV
might parallel the localizer without capturing it.
Use LNAV or HDG SEL to intercept the final approach course as needed.
When:
On final approach course
.
For approaches using LNAV Mode:
Final Approach Tracking ...................................................................................................................................................................................................................................................... Check
Verify that LNAV is engaged; and
Verify that LNAV is engaged; and
Set the final approach course heading on the heading selector.
Verify that the final approach course heading on the heading selector.
For approaches using LOC Mode:
Localizer tracking ................................................................................................................................................................................................................................................................. Check
Verify that the localizer is captured; and
Verify that the localizer is captured; and
Set the final approach course heading on the heading selector.
Verify the final approach course heading is set on the heading selector.
Normal Procedures
P a g e | 44
BOEING 737NG
Pilot Flying
Pilot Monitoring
When:
Approximately 2 NM before the final approach fix
.
Announce “APPROACHING GLIDE PATH”.
Verify, select or call for the VNAV mode, as needed.
Select or verify the VNAV mode, as needed.
Verify, select or call for the minimum altitude.
Verify or select the minimum altitude.
Call “GEAR DOWN, FLAPS 15”; and
Speedbrake lever........................................................................................................ ARMED
Landing gear lever .............................................................................................................. DN
Flap lever ............................................................................................................................. 15
ENGINE START switches ............................................................................................. CONT
At:
Final approach fix
.
FAF Crossing Altitude .......................................................................................................................................................................................................................................................... Check
Announce: “APPROACH FIX, ____”.
Note: Announce the final approach fix altitude as depicted on the approach
procedure chart.
Announce: “CHECKED”.
Verify the crossing altitude on the altimeters. Be aware of the temperature deviation
to the standard atmosphere and its relation to the indicated altitude when
following the Glide Slope.
At:
Verify the crossing altitude on the altimeters. Be aware of the temperature deviation
to the standard atmosphere and its relation to the indicated altitude when
following the Glide Slope.
The beginning the final approach descent
.
Call “FLAPS (30/40)”, as needed for landing.
Flap lever ........................................................................................................... Landing flaps
Call for the “LANDING CHECKLIST”.
Do the LANDING CHECKLIST.
When:
At least 300 feet below missed approach altitude
.
Missed approach altitude .................................................................................................... Set
Approach ........................................................................................................................................................................................................................................................................... Monitor
Both pilots must monitor the approach. Call out any significant deviations. Perform an
immediate go-around if not within the criteria to continue the approach.
Normal Procedures
P a g e | 45
BOEING 737NG
Go-Around and Missed Approach Procedure
The Go-Around and Missed Approach Procedure must be performed when an approach
needs to be abandoned when below the missed approach altitude.
Pilot Flying
Pilot Monitoring
Announce “GO-AROUND”.
CAUTION: during a single autopilot approach, the autopilot disengages when GoAround Mode is selected. Manual flight is needed until the airplane is under control
and above the minimum autopilot engagement height.
TO/GA switch................................................................................................................... Push
Note: If the A/T is engaged, the thrust advances toward the reduced go-around N1
to produce 1.000 to 2.000 feet per minute rate of climb. If needed, a second push on
the TO/GA switch is required for the A/T to command full go-around N1 limit.
Note: If the A/T is NOT engaged, it is required to advance the thrust levers manually
to the required go-around thrust.
Go-Around Thrust ................................................................................................................................................................................................................................................................ Check
Verify that the thrust increases.
Verify that the thrust increases.
Call “FLAPS 15”, as needed.
Flap lever ............................................................................................................ 15, if needed
Go-Around Attitude .............................................................................................................................................................................................................................................................. Check
Verify the rotation to go–around attitude.
Verify the rotation to go–around attitude.
Verify that the thrust is sufficient for the go-around or adjust as needed.
Verify a positive rate of climb on the altimeter and announce: “POSITIVE RATE”.
Verify a positive rate of climb on the altimeter and call: “GEAR UP”.
Landing gear lever .............................................................................................................. UP
At:
400 feet radio altitude or above
.
CAUTION: Limit bank angle to 15 degrees if airspeed is below minimum maneuver
speed for the existing flap.
Verify, select or call for a roll mode, as needed.
Verify or select the roll mode, as needed.
Missed Approach Track ....................................................................................................................................................................................................................................................... Check
Verify that the missed approach route is tracked.
Verify that the missed approach route is tracked.
Verify that the missed approach altitude is set.
Engage the autopilot anytime when at or above the minimum altitude for autopilot.
Normal Procedures
P a g e | 46
BOEING 737NG
Pilot Flying
Pilot Monitoring
At:
Acceleration height
.
Flap retraction ................................................................................................................................................................................................................................................................... Perform
Request for flaps retraction according to the flap retraction schedule.
Retract flaps according to the flap retraction schedule.
Note: Flap Retraction Speed Schedule is described after the Takeoff Procedure.
Note: If the desired missed approach speed is below flap up minimum maneuver
speed, maintain the flap required to fly the procedure speed; and, when performing
the After Takeoff Checklist, verify that the actual flap position is desired.
After:
Flap retraction is complete (or set to the planned flap setting)
.
FLCH or VNAV ................................................................................................................ Push
Verify, set or request the desired airspeed.
Verify or set the desired airspeed.
Thrust Limit .......................................................................................................................................................................................................................................................................... Check
Verify that climb thrust is set.
Verify that climb thrust is set.
Missed Approach Altitude .................................................................................................................................................................................................................................................... Check
Verify that the missed approach altitude is captured.
Verify that the missed approach altitude is captured.
Call for the “AFTER TAKEOFF CHECKLIST”.
PACKS ........................................................................................................................... AUTO
ENGINE BLEEDS ...............................................................................................................ON
Engine Start Switches .............................................................................................As needed
Landing gear .............................................................................................................. Up & Off
Auto Brake ........................................................................................................................ OFF
Do the AFTER TAKEOFF CHECKLIST.
Normal Procedures
P a g e | 47
BOEING 737NG
Landing and Landing Roll Procedure
Manually land the airplane or monitor the autopilot when an autoland is desired.
Pilot Flying
Pilot Monitoring
At:
Procedure minimum altitude or height
.
Announce: “LANDING” or “GO AROUND”.
Note: For Go Around follow the Go-Around and Missed Approach Procedure.
If:
Manual flight is required or desired
.
Disengage the autopilot anytime when at or above the minimum altitude for autopilot.
Begin with a stabilized approach on speed, in trim, and on glide path.
Maintain the glide path to landing.
When a manual landing is planned from an approach with the autopilot connected, the
transition to manual flight should be planned early enough to allow the pilot time to
establish airplane control before beginning the flare.
Establish a final approach that assures safe threshold clearance and gear touchdown at
least 1,000 feet down the runway.
When the threshold passes out of sight under the airplane nose shift the visual sighting point
to the far end of the runway.
Initiate the flare when the main gear is approximately 20 feet above the runway, by
increasing pitch attitude approximately 2 to 3 degrees.
Smoothly retard the thrust levers to idle after the flare is initiated and make small pitch
attitude adjustments to maintain the desired descent rate to the runway. Ideally, main
gear touchdown should occur simultaneously with the thrust levers reaching idle.
Typically, the pitch attitude increases slightly during the actual landing, but avoid overrotating. Do not increase the pitch attitude, trim, or hold the nose wheel off the runway
after landing.
Immediately after:
Touchdown
.
Verify the thrust levers are closed.
Move the speedbrake up manually, as needed.
Verify the speedbrake lever position and announce: “SPEEDBRAKES UP” or
“SPEEDBRAKES NOT UP”.
Autobrake ............................................................................................................................................................................................................................................................................ Check
Verify correct autobrake operation, as needed.
Verify correct autobrake operation, as needed.
Normal Procedures
P a g e | 48
BOEING 737NG
Pilot Flying
Pilot Monitoring
WARNING: After the reverse thrust levers are raised, a full stop landing must be
made. If an engine remains in reverse, safe flight is not possible.
Without delay, raise the reverse thrust levers to the interlocks and hold light pressure until
the interlocks release.
Verify the REV indications are green and announce: “REVERSERS NORMAL”.
Apply reverse thrust as needed.
If the is no REV indication(s) or the indication(s) stays amber, announce “NO REVERSERS”
ou “NO REVERSER LEFT/RIGHT”, as needed.
By 60 knots, start movement of the reverse thrust levers to reach the reverse idle detent
before taxi speed.
Announce: “SIXTY KNOTS”.
After the engines are at reverse idle, move the reverse thrust levers to fully down.
Before taxi speed, announce: “MANUAL BRAKES”.
Disarm the autobrake and use manual braking, as needed.
Verify the AUTOBRAKE DISARM light illuminates and announce: “AUTOBRAKE DISARM”.
Before turning off the runway, disconnect the autopilot, as needed.
Reverse Thrust Lever Positions
Normal Procedures
P a g e | 49
BOEING 737NG
After Landing Procedure
Start the After Landing Procedure when clear of the active runway and after the taxi route
has been confirmed.
Pilot Flying
Pilot Monitoring
SPEEDBRAKE lever ....................................................................................................DOWN
PROBE HEAT switches ......................................... AUTO (as installed) or OFF (as installed)
ENGINE ANTI-ICE switches ...................................................................................As needed
LANDING light switches ................................................................................................... OFF
RUNWAY TURNOFF switches ......................................................................................... OFF
APU selector .................................................................................................START, then ON
POSITION light switch .............................................................................................. STEADY
WXR radar display ............................................................................................................ OFF
Verify that the weather radar indications are not shown on the ND.
TERR display .................................................................................................................... OFF
Verify that the terrain indications are not shown on the ND.
AUTOBRAKE selector ...................................................................................................... OFF
FLAP lever .......................................................................................................................... UP
Transponder mode selector ........................................................................................ XPNDR
Verify that TCAS OFF is shown on the ND and announce “TCAS OFF”.
When:
Approaching the parking position
.
TAXI light switch ............................................................................................................... OFF
Normal Procedures
P a g e | 50
BOEING 737NG
Shutdown Procedure
Start the Shutdown Procedure after taxi is complete.
Captain
First Officer
Engine cool down recommendations................................................................................................................................................................................................................................... Check
Use a thrust setting normally used for taxi operations; and
Run the engines for at least 3 minutes after reverse idle.
Note: If a thrust setting above those normally used for taxi is required at any stage
after the standard 3 minutes recommendation: run the engine for at least 1 minute
after thrust reduction.
PARKING BRAKE .............................................................................................................. Set
Verify that the PARKING BRAKE warning light is illuminated.
Electrical power ..................................................................................................................Set
If APU power is needed:
Verify that the APU GENERATOR OFF BUS light is illuminated.
APU GENERATOR bus switches ...........................................................................ON
Verify that the SOURCE OFF lights are extinguished.
If external power is needed:
Verify that the GRD POWER AVAILABLE light is illuminated.
GRD POWER switch ..............................................................................................ON
Verify that the SOURCE OFF lights are extinguished.
Engine Start Levers .................................................................................................. CUTOFF
If towing is needed:
Establish communications with the ground personnel.
WARNING: If the nose gear steering is not locked out, any change to hydraulic power
with the tow bar connected may cause unwanted tow bar movement.
Confirm the nose gear steering is locked out.
CAUTION: Do not hold or turn the nose wheel tiller during pushback or towing. This
can damage the nose gear or the tow bar.
CAUTION: Do not use airplane brakes to stop the airplane during pushback or
towing. This can damage the nose gear or the tow bar.
Parking brake ........................................................................................Set or release
Set or release as directed by ground handling personnel.
FUEL PUMP switches ...................................................................................................... OFF
Verify that the center tank fuel pump LOW PRESSURE lights are extinguished.
Normal Procedures
P a g e | 51
BOEING 737NG
Captain
First Officer
Verify that the main tank fuel pump LOW PRESSURE lights are illuminated.
Note: Whenever the APU is running and AC electrical power is on the busses, turn
on one fuel boost pump to supply fuel under pressure to the APU to extend the
service life of its fuel control unit.
CAUTION: Do not operate the center tank fuel pumps with the flight deck
unattended.
FASTEN BELTS switch .................................................................................................... OFF
WING ANTI-ICE switch ..................................................................................................... OFF
Verify that the VALVE OPEN lights are extinguished.
ENGINE ANTI-ICE switches ............................................................................................. OFF
Verify that the COWL ANTI-ICE lights are extinguished.
Verify that the COWL VALVE OPEN lights are extinguished.
ELECTRIC HYDRAULIC PUMPS switches ..................................................................... OFF
Verify that the OVERHEAT lights are extinguished.
Verify that the LOW PRESURE lights are illuminated.
Air conditioning PACK switches .................................................................................... AUTO
ISOLATION VALVE switch ............................................................................................ OPEN
Engine BLEED air switches ................................................................................................ON
If the APU is ON:
APU BLEED air switch .................................................................................................ON
Verify that the DUAL BLEED light is illuminated.
ANTI COLLISION light switch ........................................................................................... OFF
F/D switch ......................................................................................................................... OFF
F/D switch ......................................................................................................................... OFF
EFB (as installed) .......................................................................................... CLOSE FLIGHT
EFB (as installed) .......................................................................................... CLOSE FLIGHT
Transponder Mode Selector .......................................................................................... STBY
If wheel chocks are going to be used:
Establish communications with the ground personnel.
Confirm that chocks are in place.
Parking brake ................................................................................................. Release
Verify that the PARKING BRAKE warning light is extinguished.
Call for the “SHUTDOWN CHECKLIST”.
Do the SHUTDOWN CHECKLIST.
Normal Procedures
P a g e | 52
BOEING 737NG
Secure Procedure
Start the Secure Procedure after all the passengers have been disembarked.
Captain
First Officer
IRS mode selectors .......................................................................................................... OFF
CAB/UTIL power switch (as installed) .............................................................................. OFF
IFE/PASS SEAT power switch (as installed) .................................................................... OFF
GALLEY power switch (as installed) ................................................................................ OFF
EMERGENCY EXIT LIGHTS switch ................................................................................ OFF
Verify that the NOT ARMED light is illuminated.
WINDOW HEAT switches ................................................................................................. OFF
Verify that the ON lights are extinguished.
TRIM AIR switch (as installed).......................................................................................... OFF
Air conditioning PACK switches ....................................................................................... OFF
POSITION light switch ............................................................................................As needed
EFB (as installed) ..................................................................................................Power OFF
EFB (as installed) ................................................................................................. Power OFF
Call for the “SECURE CHECKLIST”.
Do the SECURE CHECKLIST.
FLIGHT DECK ACCESS SYSTEM switch ....................................................................... OFF
Normal Procedures
P a g e | 53