-left engine .................................... 793 323 61
-
right engine ................................... 793 323 62. Performance decreases over time.
-left engine .................................... 710 811 61
-
right engine ................................... 710 811 62. Power fluctuates.
-left engine .................................... 710 614 61
-
right engine ................................... 710 614 62. Servo fuel heater filter differential pressure
OBSERVED FAULTS
PW Page 33 D633W113-BEJ May 05/02
E
FAULT DESCRIPTION_________________ FAULT CODE
pop-out indicator is extended.
-left engine .................................... 732 812 61
-right engine ................................... 732 812 62
. Servo fuel heater thermal pop-out indicator is extended.
-left engine .................................... 732 811 61
-
right engine ................................... 732 811 62. Slow response to thrust lever movement.
-left engine .................................... 710 631 61
-
right engine ................................... 710 631 62. Start fails during manual start.
-left engine .................................... 801 811 61
-
right engine ................................... 801 811 62. Start fails with fuel flow OK.
-left engine .................................... 801 612 61
-
right engine ................................... 801 612 62. Start fails with fuel flow zero or low.
-left engine .................................... 801 611 61
-
right engine ................................... 801 611 62. Start fails with ignition system 1 or 2.
-left engine .................................... 801 613 61
-
right engine ................................... 801 613 62. Start has slow acceleration to idle.
-left engine .................................... 801 617 61
-right engine ................................... 801 617 62
. Start hot or impending hot), more than 10 seconds to light.
-left engine .................................... 801 614 61
-right engine ................................... 801 614 62
. START/IGNITION L switch moves to the NORM position with N2 < 41%.
-left engine .................................... 801 621 61
-right engine ................................... 801 621 62
. START/IGNITION L switch stays in the START position with N2 > 46%.
-left engine .................................... 801 622 61
-right engine ................................... 801 622 62. Surge or stall during forward thrust.
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(36)
