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 ENG IGNITOR L1 ....................................... 742 001 61 Left engine failed to ignite using ignitor 1.
 ENG IGNITOR L2 ....................................... 742 002 61 Left engine failed to ignite using ignitor 2.
 ENG IGNITOR R1 ....................................... 742 001 62 Right engine failed to ignite using ignitor 1.
 ENG IGNITOR R2 ....................................... 742 002 62 Right engine failed to ignite using ignitor 2.
 ENG L START EGT ...................................... 732 191 61 An exceedance of the ground start EGT limit has been recorded during an in-flight start of the left engine.
 ENG OIL FILT SNSR L .................................. 793 053 61 The pressure switch for detecting impending oil filter bypass on the left engine has failed.
 ENG OIL FILT SNSR R .................................. 793 053 62 The pressure switch for detecting impending oil filter bypass on the right engine has failed.
 ENG OIL FILTER L ..................................... 793 051 61 Left engine primary oil filter approaches bypass (large pressure differential across normal filter) with engine running.
 ENG OIL FILTER R ..................................... 793 051 62 Right engine primary oil filter approaches bypass (large pressure differential across normal filter) with engine running.
EFFECTIVITY
 .
EICAS STATUS MESSAGES
.
 ALL PW .
Page 27 D633W113-BEJ Jan 05/04
E
MESSAGE/DESCRIPTION___________________ FAULT CODE
 ENG R START EGT ...................................... 732 191 62 An exceedance of the ground start EGT limit has been recorded during an in-flight start of the right engine.
 ENG REVERSER L ....................................... 783 002 61 Left engine thrust reverser control system fault.
 ENG REVERSER R ....................................... 783 002 62 Right engine thrust reverser control system fault.
 ENG REVERSER SNSR L .................................. 783 021 61 One (and only one) of the left thrust reverser sensing elements is failed.
 ENG REVERSER SNSR R .................................. 783 021 62 One (and only one) of the right thrust reverser sensing elements is failed.
 ENG START VALVE L .................................... 801 032 61 Left starter air valve position disagrees with commanded position or starter air valve position indication is lost.
 ENG START VALVE R .................................... 801 032 62 Right starter air valve position disagrees with commanded position or starter air valve position indication is lost.
 ENG VIB MONITOR L .................................... 773 001 61 Left engine airborne vibration monitoring (AVM) system is inoperative, or loss of tachometer data.
EFFECTIVITY
 .
EICAS STATUS MESSAGES
.
 ALL PW .
Page 28 D633W113-BEJ Jan 05/04
　
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本文鏈接地址：Fault Reporting Manual 故障報告手冊(91)