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Cleared onto active
runway.
Captain:
· Call for “BEFORE TAKEOFF
CHECKLIST”
· Arm Autothrottles
(First Officer)
· Complete Before Takeoff Procedure and Read
Checklist
CONDITION: PRIOR TO TO/GA ACTIVIATION
The N1 limit on the EFIS aircraft is
annunciated on the Thrust Mode
Annunicator (TMA) above the N1
RPM indicators.
(---) Annunicated on the TMA
indicates the FMC is not
computing thrust limits.
Cleared for takeoff. · Advance throttles to approximately 40%
N1 and stabilize
· Advance throttles to vertical and engage
TO/GA at approximately 70% N1.
· Ensure engine acceleration to takeoff
power range prior to 60 knots
· Call “CHECK POWER”
· Observe TO/GA Annunciation
· Crosscheck Takeoff N1 is set at desired power
setting
· Call “POWER SET _______ % N1”
CONDITION: TO/GA, LESS THAN 60 KNOTS
FMA annunciations depicted
assume the full utilization of the
flight guidance with all of the
autoflight features operating
normally.
60 knots to V1. · Verify airspeed at “100 KNOTS”
First Officer Takeoff:
· Place both hands on control yoke after
initial power set.
· Observe “THR HLD”
· Monitor Instruments and Warning Lights
· At 100 KIAS call “100 KNOTS”
First Officer Takeoff:
· Captain guards and retains exclusive control of
throttles after initial power set.
CONDITION: TO/GA, GREATER THAN 84 KNOTS
Command Bars pitch from 10
degrees nose down to 15 degrees
nose up at 60 knots. Do not follow
pitch commands until after rotating
through 15 degrees of nose up
pitch during rotation.
> THR HLD annunciates at 64
kts.
>@BCD THR HLD
annunciates at 84 kts.
V1, VR, Rotation and
Liftoff.
· Rotate at VR (2.5 degrees/Sec)
· Call “POSITIVE RATE”
· Call “GEAR UP”
· Adjust pitch as indicated by F/D
Captain Takeoff:
· Remove hand from throttles at V1
· Call “V1”
· Call “ROTATE”
· Call “POSITIVE RATE”
· Retract Gear on Command
CONDITION: INITIAL CLIMB
Do not exceed normal rotation rate
(2.5 degrees/sec) as tail contact
with the runway is possible if the
normal rotation rate is exceeded.
Sec. 3 Page 126 737
Rev. 11/15/02 #41 Continental Flight Manual
TAKEOFF CHART – ICAO B
PHASE OF
FLIGHT
PILOT FLYING:
DUTIES / CALLOUTS
PILOT MONITORING:
DUTIES / CALLOUTS
> FMA DISPLAY >@BCD
FMA DISPLAY
NOTES - SINGLE
CHANNEL
400 Feet AGL · Call for desired AFDS Roll Mode (HDG
SEL or LNAV)
· Upon command select the desired AFDS Roll
Mode
· Verify FMA
CONDITION: ABOVE 400°, GREATER THAN
18 SECONDS AFTER LIFTOFF
CONDITION: ABOVE 400°, GREATER THAN
18 SECONDS AFTER LIFTOFF
‘HDG SEL’ will automatically arm
with any pitch mode change after a
TO/GA takeoff (ALT ACQ, ALT
HLD, MCP SPD, V/S). If ALT
ACQ, then ALT HLD will engage
automatically. The A/T will
automatically revert to MCP SPD
and the N1 LIMIT to CLB, then
CRZ limit.
1,000 Feet AFE · Reduce pitch toward 10 degrees
Calls are for a Flaps 5 departure
· Call “FLAPS 1 VNAV” or if level change
departure call “FLAPS 1 CLIMB POWER
LVL CHG, SET TOP BUG”
· Continue flap retraction on schedule; Call
“FLAPS UP, AFTER TAKEOFF
CHECKLIST”
· Climb at VM Flaps 0 speed to 3000 feet
AFE
· Select Flaps on command
· Press VNAV on MCP or if level change mode
takeoff is desired Press N1; LVL CHG ;Slew
Airspeed Cursor to Vm Flaps 0 speed.
· Check FMA (TMA on EFIS) for CLB
· Check FMA for Pitch Mode, MCP SPD or
VNAV
· Complete After Takeoff Procedure and
Checklist
CONDITION: CLEAN AIRCRAFT CLIMBING TO
3,000 AGL
CONDITION: CLEAN AIRCRAFT CLIMBING TO
3,000 AGL
If the autopilot is engaged after
1000 feet AGL, the A/P STATUS
annunciation of A/P OFF on the
non-EFIS aircraft will go blank.
On the EFIS aircraft, the A/P
STATUS will change from FD to
CMD.
3,000 Feet AGL · Call for “VNAV” if not called for already
(Manual)
· Select “VNAV” (Autoflight)
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737 FLIGHT MANUAL 737飞行手册2(17)
