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TIRE PRESS SYS ....................................... 324 081 00 Tire pressure indication system has failed causing partial or total loss of tire pressure indication, or loss of ARINC 629 bus inputs from the tire pressure monitor unit.
TRANSPONDER L ........................................ 345 042 41 Left ATC transponder failure.
TRANSPONDER R ........................................ 345 042 42 Right ATC transponder failure.
TRIM AIR L ........................................... 216 032 41 Loss of left cabin temp control system. Left trim air Pressure Relief Shut Off Valve (PRSOV) closed due to zone duct overtemp condition or failure of trim air pressure sensor.
TRIM AIR PRSOV L ..................................... 216 041 41 Left trim air Pressure Relief Shut Off Valve (PRSOV) failed.
TRIM AIR PRSOV R ..................................... 216 041 42 Right trim air Pressure Relief Shutoff Valve (PRSOV) failed.
EFFECTIVITY
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EICAS STATUS MESSAGES
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ALL PW .
Page 61 D633W113-BEJ Jan 05/04
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MESSAGE/DESCRIPTION___________________ FAULT CODE
TRIM AIR R ........................................... 216 032 42 Loss of right cabin temp control system. Right trim air Pressure Relief Shutoff Valve (PRSOV) is closed due to zone duct overtemp condition or failure of trim air pressure sensor.
TURB CASE COOL HPT L ................................. 752 011 61 Left engine high pressure turbine (HPT) case cooling actuator is stuck or reverted to its fail-safe position.
TURB CASE COOL HPT R ................................. 752 011 62 Right engine high pressure turbine (HPT) case cooling actuator is stuck or reverted to its fail-safe position.
TURB CASE COOL LPT L ................................. 752 012 61 Left engine low pressure (LPT) turbine case cooling actuator is stuck or reverted to its fail-safe position.
TURB CASE COOL LPT R ................................. 752 012 62 Right engine low pressure (LPT) turbine case cooling actuator is stuck or reverted to its fail-safe position.
TURB COOLING AIR L ................................... 752 021 61 Left engine turbine cooling air actuator is stuck or reverted to its fail-safe position.
TURB COOLING AIR R ................................... 752 021 62 Right engine turbine cooling air actuator is stuck or reverted to its fail-safe position.
EFFECTIVITY
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EICAS STATUS MESSAGES
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ALL PW .
Page 62 D633W113-BEJ Jan 05/04
MESSAGE/DESCRIPTION___________________ FAULT CODE
VOR L ................................................ 345 001 41 Failure of left Very High Frequency Omnidirectional Receiver (VOR) System.
VOR R ................................................ 345 001 42 Failure of right Very High Omnidirectional Receiver (VOR) System.
VSCF VALVE CLOSED L .................................. 753 021 61 Left engine VSCF air cooling valve failed closed.
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Fault Reporting Manual 故障报告手册(106)
