-right engine ................................... 801 622 62
STBY A/S IND maintenance memo shows on the MAT ....... 341 480 00
STBY ALT IND maintenance memo shows on the MAT ....... 341 486 00
STBY ATT IND maintenance memo shows on the MAT ....... 342 481 00
Steering tiller: stiff or inoperative ................ 325 611 00
Storm light(s): do not come on ....................... 331 614 00
Strobe light: does not come on.
-left wing ...................................... 331 634 41
-right wing ..................................... 331 634 42
-tailcone ....................................... 331 635 00 Strut (engine):
-left engine strut .............................. 281 817 41
-
right engine strut ............................. 281 817 42 Strut or nacelle dragged or damaged:
-left engine .................................... 055 641 41
-
right engine ................................... 055 641 42 Sun visor problem:
-captain's ...................................... 251 644 31
-first officer's ................................ 251 644 32
OBSERVED FAULTS
PW Page 88 D633W113-BEJ May 05/02
S
FAULT DESCRIPTION_________________ FAULT CODE Surge or stall of engine during forward thrust:
-left engine .................................... 710 612 61
-
right engine ................................... 710 612 62 Surge or stall of engine during reverse thrust:
-left engine .................................... 710 613 61
-
right engine ................................... 710 613 62 Synoptic (air) problem ............................... 210 611 00 Synoptic (fuel) problem .............................. 280 611 00 System configuration display on the MAT:
. Shows LRU DOES NOT GIVE A REPLY .................. 451 814 00
. Shows LRU INACTIVE/FAULTED ....................... 451 811 00
OBSERVED FAULTS
PW Page 89 D633W113-BEJ May 05/02
T
FAULT DESCRIPTION_________________ FAULT CODE
Tail dragged ......................................... 055 643 00
Take-off thrust too low: . N1, N2, and fuel flow normal for observed EPR.
-left engine .................................... 732 621 61
-right engine ................................... 732 621 62. N1, N2, and fuel flow not known.
-left engine .................................... 732 623 61
-right engine ................................... 732 623 62
. N1, N2, and fuel flow not normal for observed
EPR.
-left engine .................................... 732 622 61
-right engine ................................... 732 622 62 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(71)