Drain mast: has ice on it.
 -aft ............................................ 307 811 45

 -forward ........................................ 307 811 44

OBSERVED FAULTS
PW Page 23 D633W113-BEJ Jan 05/04
D
FAULT DESCRIPTION_________________  FAULT CODE__________
 DRIVE light on DRIVE DISC switch: stays off after
 engine is stopped.

 -left engine .................................... 241 672 41

 -right engine ................................... 241 672 42

 DRIVE light on DRIVE DISC switch and OFF light on
 GEN CTRL switch: stay on after engine is started.

 -left engine .................................... 241 671 41

 -right engine ................................... 241 671 42

 Dust (extreme) condition ............................. 055 613 00

OBSERVED FAULTS
PW Page 24 D633W113-BEJ Sep 05/03
E
FAULT DESCRIPTION_________________ FAULT CODE
 EAI CARD L maintenance memo shows on the MAT ......... 301 480 41

 EAI CARD R maintenance memo shows on the MAT ......... 301 480 42

 EDP pressure and case drain filter module:. Differential pressure indicator on case drain filter is extended.
 -C1 system ...................................... 291 816 01

 -C2 system ...................................... 291 816 02

. Differential pressure indicator on pressure
 filter is extended.

 -C1 system ...................................... 291 817 01

 -C2 system ...................................... 291 817 02

 EEC-related ground test on MAT: EEC-related test prevented because of incorrect Mach value ............ 732 501 00
 EFIS control panel:. Does not show desired information on ND.
 -captain's ...................................... 316 693 31

 -first officer's ................................ 316 693 32 . Does not show desired information on PFD.
 -captain's ...................................... 316 692 31

 -first officer's ................................ 316 692 32

 EFIS control panel problem:
 -captain's ...................................... 316 691 31

 -first officer's ................................ 316 691 32

 EGT (engine) fluctuates:
 -left engine .................................... 772 611 61

 -right engine ................................... 772 611 62

OBSERVED FAULTS
PW Page 25 D633W113-BEJ May 05/02
E
FAULT DESCRIPTION_________________ FAULT CODE
 EGT indication (engine):. Amber.
 -left engine .................................... 772 303 61

 -
right engine ................................... 772 303 62. Blank.

 -left engine .................................... 772 301 61
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Fault Reporting Manual 故障報告手冊(30)