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(30)
