BOEING 737-800SFP (All SFP)
NORMAL CHECKLIST
PREFLIGHT
OXYGEN
NAV. TRANSFER & DISPLAY SWITCHES
WINDOW HEAT
PRESSURIZATION MODE SELECTOR
FLIGHT INSTRUMENTS
ENGINE START LEVERS
TESTED, 100%
NORMAL & AUTO
ON
AUTO
HEADING ___ ALTIMETER ___
CUTOFF
(BOTH)
(F/O)
(F/O)
(F/O)
(BOTH)
(C)
BEFORE START B737-____ - ____ K
FLIGHT DECK DOOR
CLOSED AND LOCKED
FUEL
_____ KG , PUMPS ON
DOORS / WINDOWS
LOCKED
MCP
V2 ___, HEADING ___, ALTITUDE___
AUTOBRAKE
RTO
TAKEOFF SPEEDS
V1 ___, VR ___, V2 ___
CDU PREFLIGHT
COMPLETED
PARKING BRAKE
SET
RUDDER AND AILERON TRIM
FREE AND 0
TAXI AND TAKEOFF BRIEFING
COMPLETED
------------------------------------------------------------------------FASTEN BELTS SWITCH
ON
ANTICOLLISION LIGHT
ON
PARKING BRAKE
AS REQUIRED
(F/O)
(BOTH)
(BOTH)
(BOTH)
(F/O)
(C)
(C)
(C)
(C)
(BOTH)
(F/O)
(F/O)
(C)
SINGLE ENGINE BEFORE TAXI
GENERATOR (Operating Engine only)
PACKS
ISOLATION VALVE
FLIGHT CONTROLS
GROUND EQUIPMENT
Single Engine with:
PACKS
Isolation
Valve
Engine
Bleeds
APU
Bleed
APU and ENG No.2
AUTO
APU and ENG No.1
AUTO
CLOSED
ON
ON
OPEN
OFF
APU OFF (Any Eng)
AUTO
ON
CLOSED
ON
OFF
ON
AUTO
________
CHECKED
CLEAR
(F/O)
(F/O)
(F/O)
(C)
(BOTH)
ON
___
___
CONT
CHECKED
IDLE IDLE
CHECKED
CLEAR
(F/O)
(F/O)
(F/O)
(F/O)
(BOTH)
(C)
(C)
(BOTH)
DUAL ENGINE BEFORE TAXI
GENERATORS
ANTI-ICE
APU
ENGINE START SWITCHES
RECALL
ENGINE START LEVERS
FLIGHT CONTROLS
GROUND EQUIPMENT
SHUTDOWN
OFF (F/O)
OFF (BOTH)
CUTOFF (C)
AS REQUIRED (C)
STBY (F/O)
ANTICOLLISION LIGHT
WEATHER RADAR
ENGINE START LEVERS
PARKING BRAKE
TRANSPONDER
SECURE
IRS
EMERGENCY EXIT LIGHTS
WINDOW HEAT
PACKS
OFF
OFF
OFF
OFF
(F/O)
(F/O)
(F/O)
(F/O)
RUNWAY CHANGE
FLAPS
N1
IAS BUGS
STABLIZER TRIM
TAKEOFF BRIEFING
CDU SID UPDATE
___GREEN LIGHT (C)
___K, FULL/REDUCED (C)
V1___,VR___, V2___ (C)
____UNITS (C)
COMPLETED (BOTH)
COMPLETED (F/O)
Rev. 26 – Outubro 2020 / DC-MN-FLT-OH-001-570
BOEING 737-800SFP (All SFP)
OPT Airport Category
REQUIREMENTS FOR ILS CAT II / ILS CAT I AUTOLAND
QUALIFIED CREW FOR OPERATION
METEOROLOGICAL CONDITIONS NOT BELOW THE MINIMA SPECIFIED BY IAL
CERTIFIED AIRCRAFT
MINIMUM EQUIPMENT LIST
 DUAL CHANNEL AUTOPILOT
 RADIO ALTIMETER AND DISPLAY FOR EACH PILOT
 AUTOTHROTTLE
 WINDSHIELD WIPERS FOR EACH PILOT
 ILS RECEIVER AND DISPLAY FOR EACH PILOT
 FLIGHT MODE ANNUNCIATOR FOR EACH PILOT
 TWO ADIRU'S IN NAV MODE
 BOTH MAIN HYDRAULIC SYSTEMS OPERATING
 TWO INDEPENDENT SOURCES OF AC POWER (APU MAY BE USED)
 BOTH ENGINES OPERATING
OPERATIONAL PROCEDURES
Request the Cabin Crew to advise the passenger to TURN OFF any PED
Advise ATC about ILS critical areas
Pilots must be ready to promptly respond to inappropriate AFDS performance
CALLOUTS
1000 ft AFE
Inform "1000 ft"
Observe and inform: "STABILIZED" or "NOT STABILIZED
GO-AROUND"
Acknowledge
For the 'NOT STABILIZED GO AROUND'
Callout, confirm "GO-AROUND" and perform missed
approach procedure.
500 ft AFE
Verify on FMA the A/P status and inform: "FLARE ARMED
or FLARE NOT ARMED"
Confirm "FLARE ARMED" or;
For the "FLARE NOT ARMED" Callout, advise "GO
AROUND"
100 FT above minimum (RA)
Inform: "approaching minimuns"
Acknowledge and inform: "Head Up"
DH (CAT II) / DA (CAT I)
Inform "LANDING" or "GO-AROUND"
Night flight: request "All lights ON"
Inform: "MINIMUNS"
Turn the retractable landing lights - ON
Acknowledge
For "NO FLARE" perform missed approach
procedure.
50 ft (RA)
Monitor FMA
Inform: "FLARE" or "NO FLARE"
27 FT (RA)
Acknowledge
Monitor FMA
Inform: "RETARD"
After touchdown: DISENGAGE AUTOPILOT
PLACARD PHILOSOPHY
BP31-1312
CAT II / RNP-AR
LIMITATION
BP31-1313
RNP-AR
NOT ALLOWED
The placard
above means that
the aircraft does
not have
limitation to ILS
CAT II or RNPAR.
The placard above
means that the aircraft is
restricted to RNP-AR
operation.
ILS CAT II operations
are allowed.
CAT II / RNP-AR
LIMITATION
CAT II
NOT ALLOWED
The placard
above means that
the aircraft is
restricted to ILS
CAT II operation.
CAT II / RNP-AR
LIMITATION
CAT II / RNP-AR
NOT ALLOWED
The placard above means
that the aircraft is
restricted to ILS CAT II
and RNP-AR
RNP-AR
operations are
allowed.
Rev. 26 – Outubro 2020 / DC-MN-FLT-OH-001-570
Climb Thrust