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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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 not support its complete set of
 functionalities.
 ELMS P310 PANEL ...................................... 240 021 03

 The Electrical Load Management System (ELMS)
 P310 panel is faulted such that it cannot
 support airplane dispatch. 1) AIMS has lost
 ARINC 629 communication with the P310 panel. OR
 2) One P310 panel channel is lost and the other
 faulted and is operating in a degraded mode. OR
 3) Both P310 panel channels are faulted and are
 operating in a degraded mode.
 ENG CONTROL L ........................................ 732 132 61

 Left engine Electronic Engine Control (EEC) is
 in a "No Dispatch" configuration. EEC may be
 operating with a limited set of engine control
 parameters and may not be capable of
 controlling all aspects of engine operation.
EFFECTIVITY
 .
EICAS STATUS MESSAGES
.
 ALL PW .
Page 25 D633W113-BEJ Jan 05/04
E
MESSAGE/DESCRIPTION___________________ FAULT CODE
 ENG CONTROL R ........................................ 732 132 62 Right engine Electronic Engine Control (EEC) is in a "No Dispatch" configuration. EEC may be operating with a limited set of engine control parameters and may not be capable of controlling all aspects of engine operation.
 ENG EEC C1 L ......................................... 732 161 61 Left engine control is in a time limited dispatch condition. Engine control system is operating with reduced redundancy.
 ENG EEC C1 R ......................................... 732 161 62 Right engine control is in a time limited dispatch condition. Engine control system is operating with reduced redundancy.
 ENG EEC MODE L ....................................... 732 142 61 Left engine Electronic Engine Control (EEC) is in the alternate control mode due to a control system fault.
 ENG EEC MODE R ....................................... 732 142 62 Right engine Electronic Engine Control (EEC) is in the alternate control mode due to a control system fault.
 ENG FUEL FILTER L .................................... 731 101 61 Differential pressure across left fuel filter approaches bypass condition.
 ENG FUEL FILTER R .................................... 731 101 62 Differential pressure across right fuel filter approaches bypass condition.
 ENG FUEL VALVE L ..................................... 732 152 61 Left High Pressure (HP) fuel shutoff valve position disagrees with commanded position.
EFFECTIVITY
 .
EICAS STATUS MESSAGES
.
 ALL PW .
Page 26 D633W113-BEJ Jan 05/04
E
MESSAGE/DESCRIPTION___________________ FAULT CODE
 ENG FUEL VALVE R ..................................... 732 152 62 Right High Pressure (HP) fuel shutoff valve position disagrees with commanded position.
 
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本文链接地址:Fault Reporting Manual 故障报告手册(90)