737 Operations Manual
Non-Normal Checklists -
Engines, APU
Copyright © The Boeing Company. See title page for details.
D6-27370-400E-TBCE NNC.7.5
ENGINE FAILURE/SHUTDOWN
Condition: Loss of thrust on an engine as indicated by the engine
indicators, or abnormal engine indications.
Accomplish an engine shutdown only when flight
conditions permit.
AUTOTHROTTLE (if engaged) . . . . . . . . . . . . . . .DISENGAGE
[Allows thrust lever to remain where manually positioned.]
THRUST LEVER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSE
[Assists in recognition of affected engine.]
Conditions permitting, operate for three minutes at idle
thrust.
ENGINE START LEVER . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
APU (if available) . . . . . . . . . . . . . . . . . . . . . START & ON BUS
PACK SWITCH (affected side). . . . . . . . . . . . . . . . . . . . . . .OFF
[Causes operating pack to regulate to high flow in flight with flaps up.]
FUEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .BALANCE
TRANSPONDER MODE SELECTOR
(TCAS equipped airplanes) . . . . . . . . . . . . . . . . . . . . . . . . . . TA
[Prevents climb commands which can exceed single engine performance
capability.]
If wing anti–ice is required:
ISOLATION VALVE SWITCH . . . . . . . . . . . . . . . . . . . . AUTO
Plan to land at the nearest suitable airport.
Accomplish the ONE ENGINE INOPERATIVE LANDING
checklist.
June 07, 2002
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