737 Flight Crew Operations Manual
7.25
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
D6-27370-4Q8-SJA
7.25
8 Choose one:
9 Plan to land at the nearest suitable airport.
►►Go to the One Engine Inoperative Landing
checklist on page 7.30
■ ■ ■ ■
10 Engine GEN switch (affected side) . . . . . . . . . ON
11 PACK switch (affected side) . . . . . . . . . . . . AUTO
12 ENGINE START switch . . . . . . . . . . . . .As needed
13 APU . . . . . . . . . . . . . . . . . . . . . . . . .As needed
PM398, PM411 - PP519, PQ976 - PT832
14 Transponder mode selector . . . . . . . . . . . .TA/RA
■ ■ ■ ■
▼Engine In-Flight Start continued▼
EGT increases within 30 seconds and a normal
start occurs:
►►Go to step 10
EGT does not increase within 30 seconds or
another abort start condition as listed in the
Normal Procedures occurs:
Engine start lever
(affected engine) . . . Confirm . . . CUTOFF
ENGINE START switch
(affected engine) . . . . . . . . . . . . . . . OFF
►►Go to step 9
Note: Do not use FMC performance predictions.
June 15, 2020
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