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L GEAR UPLOCK SENSOR ................................. 326 021 41 Failure of one (but not both) uplock sensor on the left main landing gear disagreement of uplock sensors on same gear for more than 5 sec.
LAV-GALLEY FAN L ..................................... 212 011 41 Failure of Left Lavatory/Galley Ventilation Fan.
LAV-GALLEY FAN R ..................................... 212 011 42 Failure of Right Lavatory/Galley Ventilation Fan.
LOC ANTENNA C ........................................ 343 041 43 Center localizer (LOC) antenna failed to switch to the nose or to the tail antennas when commanded by the center AFDC.
LOC ANTENNA L ........................................ 343 041 41 Left localizer (LOC) antenna failed to switch to the nose or to the tail antenna when commanded by the left AFDC.
LOC ANTENNA R ........................................ 343 041 42 Right localizer (LOC) antenna failed to switch to the nose or to the tail antenna when commanded by the right AFDC.
LSCF ASG CARD L ...................................... 310 001 41 Left Systems Card File (LSCF) ARINC Signal Gateway (ASG) Right (R) card failure.
EFFECTIVITY
.
EICAS STATUS MESSAGES
.
ALL PW .
Page 46 D633W113-BEJ Jan 05/04
MESSAGE/DESCRIPTION___________________ FAULT CODE
LSCF ASG CARD R ...................................... 310 001 42 Left Systems Card File (LSCF) ARINC Signal Gateway (ASG) right (R) card failure.
LSCF PWR SUPPLY 1 .................................... 310 011 01 Left Systems Card File (LSCF) card power supply card #1 failure.
LSCF PWR SUPPLY 2 .................................... 310 011 02 Left Systems Card File (LSCF) card power supply card #2 failure.
EFFECTIVITY
.
EICAS STATUS MESSAGES
.
ALL PW .
Page 47 D633W113-BEJ Jan 05/04
M
MESSAGE/DESCRIPTION___________________ FAULT CODE
MAIN BATTERY ......................................... 243 023 00 Main Battery failure.
MAIN BATTERY OVHT .................................... 243 022 00 Main battery over temperature.
MAIN GEAR STEERING ................................... 325 002 00 Either main gear aft axle is manually disabled, is not responding to commands, or loss of ARINC 629 bus input from main gear steering control unit.
MAN PRESS SENSOR L ................................... 361 031 41 Left engine bleed pressure sensor failed.
MAN PRESS SENSOR R ................................... 361 031 42 Right engine bleed pressure sensor failed.
MODE CTRL PANEL LANE ................................. 221 051 00 One of the two lanes in the Autopilot Flight Director System (AFDS) mode control panel (MCP) or its interface to the AFDC has failed.
EFFECTIVITY
.
EICAS STATUS MESSAGES
.
ALL PW .
Page 48 D633W113-BEJ Jan 05/04
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Fault Reporting Manual 故障报告手册(99)
