EICAS STATUS MESSAGES
PW Page 1 D633W113-BEJ May 05/03
A
MESSAGE/DESCRIPTION___________________ FAULT CODE
AFDC R ............................................... 221 041 42
Right autopilot flight director computer (AFDC)
is inoperative.
AIMS ................................................. 314 001 00
1) Either one (1) or more of the SAFEbus(tm)
lanes has failed or one (1) or more of the
power input channels to the AIMS has failed for
1 second or 2) Incompatible OPS, OPCs, or
program pins exist between Left and Right
Cabinets at uninhibited cold power-up or
software load time or 3) Data Conversion
Gateway has failed (more than 1 of 4 CPMs
failed or insufficient I/O resources for 1
second) or 4) Primary Display System has OPC
faults.
AIR/GROUND L ......................................... 320 001 41 Left Air/Ground system is failed.
AIR/GROUND R ......................................... 320 001 42 Right Air/Ground system is failed.
AIR/OIL VLV CLOSED L ................................. 792 002 61
Left engine air/oil valve failed in the closed
position.
AIR/OIL VLV CLOSED R ................................. 792 002 62
Right engine air/oil valve failed in the closed
position.
ALTITUDE ALERT SYS ................................... 341 011 00
Failure of altitude alert function or loss of
Warning Electronic System (WES) input to AIMS.
ALTN GEAR EXTEND ..................................... 323 031 00
Alternate extend control relay(s) have been
energized for greater than 60 seconds.
EICAS STATUS MESSAGES
PW Page 2 D633W113-BEJ May 05/03
A
MESSAGE/DESCRIPTION___________________ FAULT CODE
ALTN PITCH TRIM LEV .................................. 274 052 00 Alternate pitch trim lever switch failed.
ANTISKID ............................................. 324 012 00
Antiskid fault causing loss of skid protection
to two or more wheels per gear in the NORMAL
brake hydraulic system, including control unit
failure, normal antiskid valve failures, and
parking brake valve not fully open with parking
brake released; antiskid fault causing loss of
braking to two or more wheels per gear
including control unit failure or wheel speed
transducer failures; or loss of both ARINC 629
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：Fault Reporting Manual 故障报告手册(78)
