737 Operations Manual
Non-Normal Checklists -
Fire Protection
Copyright © The Boeing Company. See title page for details.
NNC.8.6 D6-27370-400E-TBCE
ENGINE FIRE, SEVERE DAMAGE
OR SEPARATION
Condition: Fire is detected in the associated engine; severe
damage which may be associated with airframe
vibration and/or abnormal engine indications has
occurred; or the engine has separated.
AUTOTHROTTLE (if engaged) . . . . . . . . . . . . . . .DISENGAGE
[Allows thrust lever to remain where manually positioned.]
THRUST LEVER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSE
[Assists in recognition of the afftected engine.]
ENGINE START LEVER . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
ENGINE FIRE WARNING SWITCH . . . . . . . . . . . . . . . . . .PULL
To manually unlock the engine fire warning switch, press
the override and pull.
If the engine fire warning switch or ENG OVERHEAT light
remains illuminated:
ENGINE FIRE WARNING SWITCH . . . . . . . .ROTATE L or R
Rotate to the stop and hold for one second.
If after 30 seconds the engine fire warning switch or ENG
OVERHEAT light remains illuminated:
ENGINE FIRE
WARNING SWITCH. . . . . . . . . . . . . . . . . . . . ROTATE TO
REMAINING BOTTLE
Rotate to the opposite stop and hold for one
second.
Continued on next page
December 06, 2002
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