AIRPLANE
OPERATIONS
MANUAL
ABNORMAL
PROCEDURES
REVISION 40
1-03-39
Page
1
Code
03
AOM-145/1114
FIRE PROTECTION
ENGINE TAILPIPE FIRE
CONDITION: Tailpipe fire was detected visually by crew or ground
personnel. No EICAS message displayed.
Affected engine:
Thrust Lever ............................................................ IDLE
Start/Stop Selector .................................................. STOP
Ignition ..................................................................... OFF
Fuel Pump ............................................................... OFF
XFeed Selector Knob .............................................. OFF
Start/Stop Selector .................................................. START,
THEN RUN
ITT................................................................................. MONITOR
ATC............................................................................... NOTIFY
Wait 90 seconds.
Associated Start/Stop Selector.....................................STOP
Associated Fire Extinguishing Handle.......................... PULL (DO NOT
ROTATE)
NOTE: If fire is not extinguished while the engine is motored, ground
personnel support must be requested.
FIRE DETECTION FAILURE
EICAS CAUTION: E1 (2) FIREDET FAIL or APU FIREDET FAIL
LIGHT: Master Caution
Engine or APU .............................................................. MONITOR
If engine fire or overheat is suspected or if E1 (2) FIREDET FAIL
message appears simultaneously with engine failure:
ENGINE FIRE, SEVERE DAMAGE
OR SEPARATION Procedure ............................ ACCOMPLISH
If APU fire or overheat is suspected or if APU FIREDET FAIL message
appears simultaneously with APU failure:
APU FIRE Procedure .............................................. ACCOMPLISH
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