-
first officer's ................................ 351 631 32

 -second observer's .............................. 351 631 34

OBSERVED FAULTS
PW Page 71 D633W113-BEJ May 05/02
P
FAULT DESCRIPTION_________________ FAULT CODE
 P310 panel relays for electrical power DC/standby system: energize and de-energize repeatedly .......... 243 811 00
 PACK FLOW MASS indications (on Air Conditioning maintenance page) for left and right packs differ by more than 10 kg/min when both packs are operating ............................................ 215 811 00
 PACK L switch: OFF light does not come on when switch set to off .................................... 215 611 41
 PACK R switch: OFF light does not come on when switch set to off .................................... 215 611 42
 PANEL FAIL shows in the frequency window of radio tuning panel:
 -center ......................................... 231 617 43

 -left ........................................... 231 617 41

 -right .......................................... 231 617 42

 Parking brake lever:. Does not release ................................. 324 652 00 . Does not set ..................................... 324 651 00
 PARKING BRAKE SET EICAS memo message: does not show when expected ........................................ 324 656 00
 Passenger address handset (flight deck) problem ...... 233 611 00
 Passenger entry door: exterior handle difficult to operate.
 -
left No. 1 ..................................... 521 811 01

 -
left No. 2 ..................................... 521 811 02

 -
left No. 3 ..................................... 521 811 03

 -
left No. 4 ..................................... 521 811 04

 -
right No. 1 .................................... 521 811 11

 -
right No. 2 .................................... 521 811 12

 -
right No. 3 .................................... 521 811 13

 -
right No. 4 .................................... 521 811 14

OBSERVED FAULTS
PW Page 72 D633W113-BEJ May 05/02
P
FAULT DESCRIPTION_________________ FAULT CODE
 Performance of engine decreases over time:
 -left engine .................................... 710 811 61

 -right engine ................................... 710 811 62

 PFD: . A/P indication does not show and A/P lights on mode control panel stay off when A/P engage switch is pushed.
 -captain's ...................................... 221 613 31

 -
first officer's ................................ 221 613 32 . Airspeed display blank or incorrect.
　
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本文鏈接地址：Fault Reporting Manual 故障報告手冊(60)