737 Operations Manual
Non-Normal Checklists -
Engines, APU
Copyright © The Boeing Company. See title page for details.
D6-27370-400E-TBCE NNC.7.19
Continued from previous page
When engine parameters have stabilized:
APU BLEED AIR SWITCH . . . . . . . . . . . . . . . . . . . . . . . .OFF
ENGINE START SWITCH. . . . . . . . . . . . . . . . . . . . . . . . . FLT
THRUST LEVER . . . . . . . . . . . . . . . . . . . . . . . . . . .ADVANCE
ENGINE GENERATOR SWITCH . . . . . . . . . . . . . . . . . . . .ON
PACK SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
Accomplish the INFLIGHT ENGINE START checklist to start
the other engine.
If neither IRS attitude display recovers after a generator bus
is restored:
IRS MODE SELECTOR SWITCHES . . . . . . . . . . . . . . . . ATT
Maintain straight and level, constant airspeed flight
until attitude displays recover (approximately 30
seconds).
MAGNETIC HEADING . . . . . . . . . . . . . . . . . . . . . . . . ENTER
APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
LOW IDLE
Condition: The LOW IDLE light illuminated indicates the related
engine is below minimum required RPM.
AUTOTHROTTLE (if engaged) . . . . . . . . . . . . . . .DISENGAGE
[Allows thrust lever to remain where manually positioned.]
THRUST LEVERS . . . . . . . . . . . . ADVANCE THRUST LEVERS
UNTIL LIGHT EXTINGUISHES
June 07, 2002
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