Right engine fuel spar valve is not in
commanded position.
FUEL TEMP INDICATION ................................. 284 102 00 Fuel temperature sensing fault or failure.
FUEL VALVE APU ....................................... 282 102 00 APU fuel valve is not in commanded position.
EFFECTIVITY
.
EICAS STATUS MESSAGES
.
ALL PW .
Page 36 D633W113-BEJ Jan 05/04
G
MESSAGE/DESCRIPTION___________________ FAULT CODE
G/S ANTENNA C ........................................ 343 031 43 Center Glide Slope (G/S) antenna failed to switch to the track or to the capture antenna as commanded by center AFDC.
G/S ANTENNA L ........................................ 343 031 41 Left Glide Slope (G/S) antenna failed to switch to the track or to the capture antenna as commanded by left AFDC.
G/S ANTENNA R ........................................ 343 031 42 Right Glide Slope (G/S) antenna failed to switch to the track or to the capture antenna as commanded by the right AFDC.
GEAR CONTROL ......................................... 323 011 00 Disagreement between individual landing gear control signals from the control lever module to the gear selector valves.
GEAR INDICATION SYS .................................. 326 011 00 Failure of both up sensors on same gear, or both door sensors on same gear, or any main landing gear (MLG) side brace down sensor, or any MLG drag brace down sensor, or any truck tilt sensor, or any nose landing gear (NLG) down sensor, or any NLG lock sensor, or any NLG not compressed sensor, or any disagreement on the same gear of MLG side brace down, MLG drag brace down, truck tilt, NLG down, NLG lock, or NLG not compressed sensors for more than 5 seconds, or landing gear partition PSEU channel faults.
GND PROX SYS ......................................... 344 032 00 Ground proximity system fault.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:Fault Reporting Manual 故障报告手册(95)