737 Flight Crew Operations Manual
Normal Procedures -
Amplified Procedures
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
NP.21.30 D6-27370-866-EGP
At 56% N2, verify that the ENGINE START switch moves to
OFF. If not, move the ENGINE START switch to OFF. F/O
Verify that the START VALVE OPEN alert extinguishes when
the ENGINE START switch moves to OFF. F/O
Call “STARTER CUTOUT.” F/O
Monitor N1, N2, EGT, fuel flow and oil pressure for normal
indications while the engine accelerates to a stable idle. C, F/O
After the engine is stable at idle, start the other engine.
Before Taxi Procedure
GENERATOR 1 and 2 switches .................................... ON F/O
PROBE HEAT switches ..................................................ON F/O
WING ANTI–ICE switch .....................................As needed F/O
ENGINE ANTI–ICE switches .............................As needed F/O
PACK switches .......................................................... AUTO F/O
ISOLATION VALVE switch ..................................... AUTO F/O
APU BLEED air switch ................................................ OFF F/O
APU switch ................................................................... OFF F/O
ENGINE START switches .........................................CONT F/O
Engine start levers ............................................IDLE detent C
Verify that the ground equipment is clear. C, F/O
Call “FLAPS ___” as needed for takeoff. C
Flap lever.................................................... Set takeoff flaps F/O
Verify that the LE FLAPS EXT green light is illuminated.
Flight controls ............................................................ Check C
Push the MFD SYS switch to display the flight control
surface position indications on the lower display unit, if
desired.
Make slow and deliberate inputs, one direction at a time.
September 15, 2016
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