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EFFECTIVITY
.
EICAS STATUS MESSAGES
.
ALL PW .
Page 21 D633W113-BEJ Jan 05/04
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MESSAGE/DESCRIPTION___________________ FAULT CODE
ECON COOL VALVE R .................................... 215 041 42 Right pack economy cooling valve not in commanded position.
ECS CARD L ........................................... 210 001 41 Failure of left Environment Control System (ECS) card.
ECS CARD R ........................................... 210 001 42 Failure of right Environment Control System (ECS) card.
EFIS CONTROL PNL L ................................... 316 072 41 Left EFISCP is inoperative. If CDU backup of the left EFISCP is not desired, deselect backup control on the CDU.
EFIS CONTROL PNL R ................................... 316 072 42 Right EFISCP is inoperative. If CDU backup of the right EFISCP is not desired, deselect backup control on the CDU.
ELEC BACKUP GEN L .................................... 242 062 41 Left backup generator off due to a protective trip.
ELEC BACKUP GEN R .................................... 242 062 42 Right backup generator off due to a protective trip.
ELEC BACKUP SYS ...................................... 242 052 00 A failure in the backup electrical system has occurred that cannot be attributed to a backup generator.
ELEC BATTERY BUS ..................................... 243 001 00 Battery Bus unpowered. Captain's flight instrument bus may be unpowered.
EFFECTIVITY
.
EICAS STATUS MESSAGES
.
ALL PW .
Page 22 D633W113-BEJ Jan 05/04
E
MESSAGE/DESCRIPTION___________________ FAULT CODE
ELEC DC BUS L ........................................ 246 002 41 Left DC bus unpowered.
ELEC DC BUS R ........................................ 246 002 42 Right DC bus unpowered.
ELEC GEN SYS L ....................................... 242 021 41
IDG has disconnected OR a protective trip of
the generator control breaker has occurred OR a
protective trip of the BTB has occurred.
ELEC GEN SYS R ....................................... 242 021 42
IDG has disconnected OR a protective trip of
the generator control breaker has occurred OR a
protective trip of the BTB has occurred.
ELEC GND HDLG BUS .................................... 242 042 00 Ground handling bus fault.
ELEC HOT BATTERY BUS ................................. 243 002 00 Hot Battery Bus unpowered.
ELEC STANDBY BUS ..................................... 243 062 00 115 VAC standby bus unpowered.
ELEC STANDBY SYS ..................................... 243 052 00
Electrical DC/Standby Power System failed the
system self-check.
ELEC TRU C1 .......................................... 243 042 01 Transformer rectifier unit C1 failed.
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本文链接地址：Fault Reporting Manual 故障报告手册(88)
