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时间:2011-09-26 11:49来源:蓝天飞行翻译 作者:航空
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 STALL WARNING SYS R .................................. 315 051 42 Failure of right stall warning system or loss of right stall warning input to AIMS-right.
 STANDBY INVERTER ..................................... 243 071 00 Standby inverter failure.
 STATIC ADM C ......................................... 342 051 43 Center static ADM is faulted or unpowered.
 STATIC ADM L ......................................... 342 051 41 Left static ADM's faulted or unpowered.
 STATIC ADM R ......................................... 342 051 42 Right static ADM is faulted or unpowered.
EFFECTIVITY
 .
EICAS STATUS MESSAGES
.
 ALL PW .
Page 59 D633W113-BEJ Jan 05/04
T
MESSAGE/DESCRIPTION___________________ FAULT CODE
 TAIL STRIKE CHAN 1 ................................... 327 011 01

 Tail strike detector channel number 1 fault or
 failure. Detector channel #1 has failed such
 that it a) indicates a tail strike has
 occurred, or b) it is incapable of in- dicating
 a tail strike occurrance. Note: Both channels
 (#1 and #2) must indicate that a tail strike
 has occurred to set the TAIL STRIKE Caution
 alert message.
 TAIL STRIKE CHAN 2 ................................... 327 011 02

 Tail strike detector channel number 2 fault or
 failure. Detector channel #2 has failed such
 that it a) indicates a tail strike has
 occurred, or b) it is incapable of in- dicating
 a tail strike occurrance. Note: Both channels
 (#1 and #2) must indicate that a tail strike
 has occurred to set the TAIL STRIKE Caution
 alert message.
 TAT .................................................. 342 061 00

 TAT channels #1 and #2 are faulted or
 unpowered.
 TCAS ................................................. 344 012 00

 Traffic Alert and Collision Avoidance System
 (TCAS) fault or system failure.
 TERR SYS ............................................. 344 034 00

 EGPWS terrain awareness (ENHANCED) function is
 failed.
 THRUST ASYM COMP ..................................... 270 062 00

 Loss of thrust asymmetry compensation (TAC)
 function.
EFFECTIVITY
 .
EICAS STATUS MESSAGES
.
 ALL PW .
Page 60 D633W113-BEJ Jan 05/04
T
MESSAGE/DESCRIPTION___________________ FAULT CODE
 TIRE PRESS ........................................... 324 072 00 Abnormal tire pressure condition exits defined as: 1) Any main or nose gear tire pressure is less than low pressure threshold or 2) any main gear tire pressure deviates from the average main gear tire pressure by more than a maximum amount, or 3) the pressure of two tires on the same axle deviate by more than a maximum amount.
 
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本文链接地址:Fault Reporting Manual 故障报告手册(105)