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FIRE CARD ENG L ...................................... 261 041 41 Left engine fire/overheat detection card fault or failure, or AIMS loss of ARINC 629/429 communication with card.
FIRE CARD ENG R ...................................... 261 041 42 Right engine fire/overheat detection card fault or failure, or AIMS loss of ARINC 629 or 429 communication with card.
FIRE LOOP 1 APU ...................................... 261 161 01 Auxilary Power Unit (APU) fire detection system loop 1 failure.
FIRE LOOP 1 ENG L .................................... 261 031 41 Left engine fire detection system loop 1 failure.
EFFECTIVITY
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EICAS STATUS MESSAGES
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ALL PW .
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MESSAGE/DESCRIPTION___________________ FAULT CODE
FIRE LOOP 1 ENG R .................................... 261 031 42 Right engine fire detection system loop 1 failure.
FIRE LOOP 2 APU ...................................... 261 161 02 Auxilary Power Unit (APU) fire detection system loop 2 failure.
FIRE LOOP 2 ENG L .................................... 261 032 41 Left engine fire detection system loop 2 failure.
FIRE LOOP 2 ENG R .................................... 261 032 42 Right engine fire detection system loop 2 failure.
FLAP/SLAT CONTROL 1 .................................. 275 022 01 High lift control lane #1 has a fault.
FLAP/SLAT CONTROL 2 .................................. 275 022 02 High lift control lane #2 has a fault.
FLAP/SLAT SKEW SNSRS ................................. 275 031 00 Failure of one or more Slat and/or Flap skew detection sensors. Loss of Slat and/or Flap Skew detection sensor redundancy.
FLAPS SECONDARY FAIL ................................. 275 012 00 Secondary (electric) flaps drive failure during the 100 flight cycle automatic secondary mode test. Flaps operate in primary (hydraulic) mode.
FLIGHT CONTROL SYS ................................... 270 071 00 Any condition of the flight control system or it's system interfaces which would prevent dispatch. Flight controls system below minimum dispatch requirements.
EFFECTIVITY
.
EICAS STATUS MESSAGES
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ALL PW .
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MESSAGE/DESCRIPTION___________________ FAULT CODE
FLOW VALVE CARGO AFT ................................. 262 221 45 Cargo compartment fire extinguishant flow valve to the aft cargo compartment has failed. One or both of the flow valve squibs are inoperative.
FLOW VALVE CARGO FWD ................................. 262 221 44 Cargo compartment fire extinguishant flow valve to the forward cargo compartment has failed. One or both of the flow valve squibs are inoperative.
FLT DECK FLOW DET .................................... 212 081 00 Flight deck low flow detector failed BITE test.
FLT INST BUS CAPT .................................... 245 012 31 Captain's flight instrument bus unpowered.
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Fault Reporting Manual 故障报告手册(93)
