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EFFECTIVITY
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EICAS STATUS MESSAGES
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 ALL PW .
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MESSAGE/DESCRIPTION___________________ FAULT CODE
 OPIC RA1 ............................................. 239 013 01 Overhead Panel Intefce Card (OPIC) on standby power is faulted.
 OPIC RA2 ............................................. 239 013 02 Overhead Panel Interface Card (OPIC) is faulted.
 OUTFLOW VALVE AFT .................................... 213 022 45 Auto control on aft outflow valve failed.
 OUTFLOW VALVE FWD .................................... 213 022 44 Auto control on forward outflow valve failed.
 OVERHEAT CIRCUIT L1 .................................. 261 071 41 Left engine overheat detection circuit 1 failure.
 OVERHEAT CIRCUIT L2 .................................. 261 072 41 Left engine overheat detection circuit 2 failure.
 OVERHEAT CIRCUIT R1 .................................. 261 071 42 Right engine overheat detection circuit 1 failure.
 OVERHEAT CIRCUIT R2 .................................. 261 072 42 Right engine overheat detection circuit 2 failure.
 OVERSPEED SYS ........................................ 315 042 00 Failure of 3 out of 4 Warning Electronic System (WES) channels, or loss of input from 3 out of 4 (WES) channels's to AIMS left and right.
 OVERSPEED VFE ........................................ 315 044 00 Airplane has exceeded VFE overspeed by 15 knots requiring a phase 2 inspection.
EFFECTIVITY
 .
EICAS STATUS MESSAGES
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 ALL PW .
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MESSAGE/DESCRIPTION___________________ FAULT CODE
 OVERSPEED VMO/MMO .................................... 315 043 00 The airplane has exceeded VMO or MMO overspeed by 20 knots requiring a phase 2 inspection.
 OVRD VALVE MOTOR L ................................... 212 091 41 Equipment Cooling Override valve actuator #1 has failed BITE test or the override valve has failed to reach commanded position within TBD seconds.
 OVRD VALVE MOTOR R ................................... 212 091 42 Override valve actuator #2 has failed BITE test or the override valve has failed to reach commanded position within TBD seconds.
EFFECTIVITY
 .
EICAS STATUS MESSAGES
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 ALL PW .
Page 52 D633W113-BEJ Jan 05/04
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MESSAGE/DESCRIPTION___________________ FAULT CODE
 PACK ACM L ........................................... 215 036 41 Left pack air cycle machine (ACM) failed.
 PACK ACM R ........................................... 215 036 42 Right pack air cycle machine (ACM) failed.
 PACK FCV L ........................................... 215 021 41 One (but not both) of the two left pack flow control valves (FCV) are not in the commanded position.
 PACK FCV R ........................................... 215 021 42 One (but not both) of the two right pack flow control valves (FCV) are not in the commanded position.
　
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本文鏈接地址：Fault Reporting Manual 故障報告手冊(101)