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Pilot Option: To remain in LVL CHG and
slew Airspeed Cursor (Command Bug on
EFIS) to 250 KIAS
· Select “VNAV” on command
· Check FMA annunciation
CONDITION: LNAV / VNAV CLIMB AUTOPILOT OFF CONDITION: LNAV / VNAV CLIMB AUTOPILOT OFF When FMC waypoint navigation is
desired the LNAV roll mode may
be engaged to provide AFDS
steering for the flight planned
course entered on the CDU. CDU
updates below 10,000 feet should
be avoided if they decrease
outside vigilance.
737 Sec. 3 Page 127
Flight Manual Continental Rev. 11/15/02 #41
NORMAL TAKEOFF
(ICAO Procedure B)
Note: VNAV departures (L2 or L3 Climb) require the FMC to be programmed accordingly.
Do not accelerate above VM flaps 0 until above 3000’ AFE.
Sec. 3 Page 128 737
Rev. 11/15/02 #41 Continental Flight Manual
TAKEOFF PROFILE
(ICAO Procedure A)
Note: To be used at airports that require close in noise abatement procedures. (Ref. Jeppesen 10-7 page for specific airport.)
737 Sec. 3 Page 129
Flight Manual Continental Rev. 11/15/02 #41
>>@ AFTER TAKEOFF FLOW
Sec. 3 Page 130 737
Rev. 11/15/02 #41 Continental Flight Manual
BCD AFTER TAKEOFF FLOW
737 Sec. 3 Page 131
Flight Manual Continental Rev. 11/15/02 #41
AFTER TAKEOFF
The Pilot Flying should call for the AFTER TAKEOFF checklist in conjunction
with the Flaps Up call. The AFTER TAKEOFF flow will not be initiated until
the PF calls for the checklist. The Pilot Monitoring will ensure the procedures
have been accomplished and then read the checklist. Do not allow the reading
of the checklist to interfere with outside vigilance while departing the terminal
area.
Caution: To avoid the possibility of the shoulder harness buckles snapping
back and inadvertently pulling circuit breakers, hold both straps
before releasing and then allow the straps to retract slowly to the
stowed position.
PM CHALLENGE AFTER TAKEOFF PM RESPOND
Air Conditioning & Pressurization ...........................................................SET
Gear...................................................................................OFF, LIGHTS OUT
Flaps.................................................................................... UP, LIGHTS OUT
PM Challenge PM Respond
Air Conditioning & Pressurization ...........................................................SET
Verify that the cabin is climbing to the pre-selected altitude, the rate of
climb is within the desirable range, and cabin differential pressure is
increasing.
If takeoff was made using APU for pressurization (bleeds off takeoff),
restore pressurization using the following procedure.
Caution: Do not configure the Bleed Air Switches to ON prior to 800
feet AGL
No. 2 Engine Bleed Air Switch ....................................................... ON
When cabin rate of climb indicator stabilizes:
APU Bleed Switch..........................................................................OFF
No. 1 Engine Bleed Air Switch ....................................................... ON
Isolation Valve Switch................................................................AUTO
Start Switches (Flow) ..........................................................(AS REQUIRED)
Normally turned OFF. Ignition switches will be in the CONT position prior
to engine anti-ice activation and will remain in CONT position during engine
anti-ice operation.
Sec. 3 Page 132 737
Rev. 11/15/02 #41 Continental Flight Manual
Gear...................................................................................OFF, LIGHTS OUT
Leave landing gear lever in the UP position approximately 10 seconds after
all red landing gear lights have extinguished to ensure positive uplock of
the landing gear.
Flaps .................................................................................... UP, LIGHTS OUT
Check that flap gauge indicates up and that leading edge lights are
extinguished.
Autobrake (Flow)........................................................................................OFF
APU (Flow) ...........................................................................(AS REQUIRED)
If the APU was used for takeoff and no longer required, it should be
shutdown after being pneumatically unloaded for a minimum of one minute.
737 Sec. 3 Page 133
Flight Manual Continental Rev. 11/15/02 #41
CLIMB
THRUST MANAGEMENT
Once climb thrust is set, the >>@ PMC / BCD EEC will
automatically compensate for the various changes in environmental conditions
during the climb.
>>@ With the PMCs off or inoperative, thrust should be adjusted as
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