737 Flight Crew Operations Manual
12.6
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D6-27370-4Q8-SJA
12.6
15 When the affected engine is at idle thrust:
Engine start lever
(affected engine) . . . . Confirm . . . . . CUTOFF
This closes the engine fuel shutoff valve
and stops an engine fuel leak.
16 PACK switch (affected side) . . . . . . . . . . . . . OFF
This causes the operating pack to regulate to
high flow in flight with the flaps up.
PM398, PM411, PQ976 - PT832
17 Choose one:
PM398, PM411, PQ976 - PT832
18 Transponder mode selector . . . . . . . . . . . . . . TA
This step prevents climb commands which can
exceed single engine performance capability.
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Continued on next page
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▼Fuel Leak Engine continued▼
APU is available for start:
APU . . . . . . . . . . . . . . . . . . . . . . START
When APU is running:
APU GEN switch
(affected side) . . . . . . . . . . . . .ON
►►Go to step 18
APU is not available:
►►Go to step 18
June 15, 2020