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时间:2011-09-26 11:49来源:蓝天飞行翻译 作者:航空
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 -right system ................................... 291 812 42

. Differential pressure indicator on pressure filter is extended.
 -C1 system ...................................... 291 813 01

 -C2 system ...................................... 291 813 02

 -left system .................................... 291 813 41

 -right system ................................... 291 813 42

 ACMS Engine Stable report: report is not present ..... 313 632 00

OBSERVED FAULTS
PW Page 1 D633W113-BEJ May 05/02
A
FAULT DESCRIPTION_________________ FAULT CODE
 ADF: . ADF (left) indication blank on ND.
 -
captain's ...................................... 345 641 31


 -
captain's and first officer's .................. 345 641 48

 

 -
first officer's ................................ 345 641 32 . ADF (right) indication blank on ND.

 -
captain's ...................................... 345 642 31


 -
captain's and first officer's .................. 345 642 48

 


 -
first officer's ................................ 345 642 32 . Audio problem.


 -left ........................................... 345 643 41

 -right .......................................... 345 643 42

 ADF L flag shows on ND:
 -captain's ...................................... 345 321 41

 -first officer's ................................ 345 322 41

 ADF R flag shows on ND:
 -captain's ...................................... 345 321 42

 -first officer's ................................ 345 322 42

 ADIRS maintenance memo shows on the MAT .............. 342 480 00

 ADIRU: does not align after 6-15 minutes ............. 342 631 00

 ADP pressure and case drain filter module:. Differential pressure indicator on case drain filter is extended.
 -C1 system ...................................... 291 814 01

 -C2 system ...................................... 291 814 02

. Differential pressure indicator on pressure
 filter is extended.

 -C1 system ...................................... 291 815 01

 -C2 system ...................................... 291 815 02

 ADU turbine gearbox assembly: differential pressure indicator on oil filter is extended.
 -C1 system ...................................... 291 818 01

 -C2 system ...................................... 291 818 02


OBSERVED FAULTS
PW Page 2 D633W113-BEJ May 05/02
A
FAULT DESCRIPTION_________________ FAULT CODE AFDS (AFDC C) maintenance memo shows on the MAT ...... 221 480 43 AFDS (AFDC L) maintenance memo shows on the MAT ...... 221 480 41 AFDS (AFDC R) maintenance memo shows on the MAT ...... 221 480 42 Aileron control wheel: does not move freely.
 
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本文链接地址:Fault Reporting Manual 故障报告手册(16)