-
right engine ................................... 055 651 42 Engine Stable (ACMS) report: report is not present ... 313 632 00 Engine strut:

 -left engine strut .............................. 281 817 41

 -
right engine strut ............................. 281 817 42 Engine strut or nacelle dragged or damaged:

 -left engine .................................... 055 641 41

 -
right engine ................................... 055 641 42 EPR indication (engine): blank.

 -left engine .................................... 771 301 61

 -
right engine ................................... 771 301 62 Escape reel problem .................................. 251 655 00 External electrical power: is not available and APU

 does not start ....................................... 491 831 00
 Extinguisher, fire (flight deck) problem ............. 251 654 00

OBSERVED FAULTS
PW Page 36 D633W113-BEJ Sep 05/03
F
FAULT DESCRIPTION_________________ FAULT CODE
 Fault did not occur in any system during the flight leg .................................................. 999 999 99
 Fire bell sounds and master WARNING lights come on but no related EICAS message shows ................... 261 611 00
 Fire extinguisher (flight deck) problem .............. 251 654 00

 Fire extinguishing (engine): incorrect signal
 specification bit state shows on the MAT during
 Thrust Reverser Isolation Valve and OPAS Check ....... 262 611 00 . Flameout of engine:. With no fuel flow or low fuel flow.
 -left engine .................................... 732 631 61

 -right engine ................................... 732 631 62. With normal fuel flow.
 -left engine .................................... 732 632 61

 -right engine ................................... 732 632 62

 Flaps, trailing edge: operation is slow .............. 275 631 00

 Flaps/slats extended with airplane speed over placard limit ........................................ 055 635 00
 Flight control shutoff valve power VALVE CLOSED
 light: does not come on with switch set to SHUTOFF.

 -
C hydraulic system for TAIL .................... 270 812 43

 -
C hydraulic system for WING .................... 270 811 43

 -
L hydraulic system for TAIL .................... 270 812 41

 -
L hydraulic system for WING .................... 270 811 41

 -
R hydraulic system for TAIL .................... 270 812 42

 -
R hydraulic system for WING .................... 270 811 42

 FLIGHT CONTROLS (C) maintenance memo shows on the MAT .................................................. 270 480 43
　
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