• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-01 19:20来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 STALL MANAGEMENT COMPUTER FAULT INDEX

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH STALL MANAGEMENT ú

 27-32-00
 COMPUTER P/N 65-52822  ú CONFIG 2 ú 03 Page 118 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 ~............................................................................... | SMC FAULT | FROM | CORRECTIVE ACTION | .................................................................................| | |
| | N2 #2 | SMC 2 | Check and repair circuit between connector D10096 pins 13| | INACTIVE | | and 14 at the EIS primary display N182 and connector| | | | D2773B pins 38 and 28 at SMC 2 M1507 (WDM 27-32-22).| | | | If the problem continues, replace the EIS primary display| | | | N182 (MM 31-42-01/401).| .................................................................................| | |
| | N2 #1 | SMC 1 | Check and repair circuit between connector D10098 pins 13| | INVALID | | and 14 at the EIS primary display N182 and connector| | | | D2771B pins 38 and 28 at SMC 1 M1506 (WDM 27-32-12).| | | | If the problem continues, replace the EIS primary display| | | | N182 (MM 31-42-01/401).| .................................................................................| | |
| | N2 #2 | SMC 2 | Check and repair circuit between connector D10096 pins 13| | INVALID | | and 14 at the EIS primary display N182 and connector| | | | D2773B pins 38 and 28 at SMC 2 M1507 (WDM 27-32-22).| | | | If the problem continues, replace the EIS primary display| | | | N182 (MM 31-42-01/401).| .................................................................................| | |
| | PROGRAM | SMC 1 | Check that connector D2771A pin 9 and connector D2771B| | PIN ERR | | pins 2, 8, 18, 19, 24, and 27 at SMC 1 M1506 are grounded| | | | or open per WDM 27-32-12.| .................................................................................| | |
| | PROGRAM | SMC 2 | Check that connector D2773A pin 9 and connector D2773B| | PIN ERR | | pins 2, 8, 18, 19, 24, and 27 at SMC 2 M1507 are grounded| | | | or open per WDM 27-32-22.| .................................................................................| | |
| | PROG PIN | SMC 1 | Check that connector D2771A pin 9 and connector D2771B| | FAULT | | pins 2, 8, 18, 19, 24, and 27 at SMC 1 M1506 are grounded| | | | or open per WDM 27-32-12.| .................................................................................| | |
| | PROG PIN | SMC 2 | Check that connector D2773A pin 9 and connector D2773B| | FAULT | | pins 2, 8, 18, 19, 24, and 27 at SMC 2 M1507 are grounded| | | | or open per WDM 27-32-22.| .................................................................................| | |
| | SELFTEST | SMC 1 | Check and repair circuit between connector D2349 pin 5| | SW BAD | | at the stall warning test module (P5-18 panel) and| | | | connector D2771B pin 50 at SMC 1 M1506 (WDM 27-32-12).| | | | If the problem continues, replace the stall warning test| | | | module (MM 27-32-21/401).| .................................................................................| | |
| | SELFTEST | SMC 2 | Check and repair circuit between connector D2351 pin 5| | SW BAD | | at the stall warning test module (P5-18 panel) and| | | | connector D2773B pin 50 at SMC 2 M1507 (WDM 27-32-22).| | | | If the problem continues, replace the stall warning test| | | | module (MM 27-32-21/401).| 2...........….......…...........................................................1
 STALL MANAGEMENT COMPUTER FAULT INDEX

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH STALL MANAGEMENT ú

 27-32-00
 COMPUTER P/N 65-52822  ú CONFIG 2 ú 03 Page 119 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 | .................................................................................| | |
| | SMC LRU | SMC 1 | Replace SMC 1 M1506 (MM 27-32-42/401).| | FAIL| | | .................................................................................| | |
| | SMC LRU | SMC 2 | Replace SMC 2 M1507 (MM 27-32-42/401).| | FAIL| | | .................................................................................| | |
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 3(39)