Stall Management Computer BITE Present Faults
Figure 104
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH STALL MANAGEMENT ú
27-32-00
COMPUTER P/N 65-52822 ú CONFIG 2 ú 01 Page 107 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
Stall Management Computer BITE Self Test
Figure 105
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH STALL MANAGEMENT ú
27-32-00
COMPUTER P/N 65-52822 ú CONFIG 2 ú 01 Page 108 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
Stall Management Computer BITE Fault History
Figure 106
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH STALL MANAGEMENT ú
27-32-00
COMPUTER P/N 65-52822 ú CONFIG 2 ú 01 Page 109 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
Figure 107
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH STALL MANAGEMENT ú
27-32-00
COMPUTER P/N 65-52822 ú CONFIG 2 ú 01 Page 110 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
FROM FIG. 102 FROM FIG. 102
Stall Management Computer BITE System Config, and Clear and Retest
Figure 108
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH STALL MANAGEMENT ú
27-32-00
COMPUTER P/N 65-52822 ú CONFIG 2 ú 01 Page 111 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
~............................................................................... | SMC FAULT | FROM | CORRECTIVE ACTION | .................................................................................| | |
| | 26V AC | SMC 1 | Check and repair circuit between left autotransformer| | MISSING | | T352 terminal LV at the E1-1 electronics shelf and| | | | connector D2771A pin 30 at SMC 1 M1506 (WDM 27-32-12).| | | | If the problem continues, check and repair circuit| | | | between SMC 1 SNSR EXC AC circuit breaker C1205 on the| | | | P18-2 panel and left autotransformer T352 terminal HV at| | | | the E1-1 electronics shelf.| | | | If the problem continues, replace left autotransformer| | | | T352 (WDM 27-32-12).| .................................................................................| | |
| | 26V AC | SMC 2 | Check and repair circuit between left autotransformer| | MISSING | | T352 terminal LV at the E1-1 electronics shelf and| | | | connector D2773A pin 30 at SMC 2 M1507 (WDM 27-32-22).| | | | If the problem continues, check and repair circuit| | | | between SMC 2 SNSR EXC AC circuit breaker C1206 on the| | | | P6-1 panel and right autotransformer T353 terminal HV at| | | | the E1-1 electronics shelf.| | | | If the problem continues, replace right autotransformer| | | | T353 (WDM 27-32-22).| .................................................................................| | |
| | A/S DC | SMC 1 | Check and repair circuit between AUTOSLAT 1 DC circuit| | MISSING | | breaker C1068 on the P6-2 panel and connector D2771A pin| | | | 1 at SMC 1 M1506 (WDM 27-83-11).| .................................................................................| | |
| | A/S DC | SMC 2 | Check and repair circuit between AUTOSLAT 2 DC circuit| | MISSING | | breaker C1070 on the P6-2 panel and connector D2773A pin| | | | 1 at SMC 2 M1507 (WDM 27-83-21).| .................................................................................| | |
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊 飛行操縱 FLIGHT CONTROLS 3(34)
