27-32-00
 COMPUTER P/N 65-52822  ú CONFIG 2 ú 02 Page 115 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 ~............................................................................... | SMC FAULT | FROM | CORRECTIVE ACTION | .................................................................................| | |
| | ASYMETRY | SMC 1 | Make sure that LE slats are fully retracted (the LE slats| | INVALID | | may have drooped if hydraulic power has been off). Open| | | | SMC STALL WARNING ASYM MODE circuit breaker C1208. If| | | | ASYMETRY INVALID is still displayed on the SMC, check and| | | | repair circuit between connector D728A pin 55 at the LE| | | | flaps and slats indication module M229 and connector| | | | D2771B pin 46 at the SMC 1 M1506 (WDM 27-32-12).| .................................................................................| | |
| | ASYMETRY | SMC 2 | Make sure that LE slats are fully retracted (the LE slats| | INVALID | | may have drooped if hydraulic power has been off). Open| | | | SMC STALL WARNING ASYM MODE circuit breaker C1208. If| | | | ASYMETRY INVALID is still displayed on the SMC, check and| | | | repair circuit between connector D728A pin 55 at the LE| | | | flaps and slats indication module M229 and connector| | | | D2773B pin 46 at the SMC 2 M1507 (WDM 27-32-22).| .................................................................................| | |
| | AUTOSLAT | SMC 1 | Check and repair circuit between AUTOSLAT 1 DC circuit| | POWER | | breaker C1068 on the P6-2 panel and connector D2771A pin| | | | 1 at SMC 1 M1506 (WDM 27-83-11).| .................................................................................| | |
| | AUTOSLAT | SMC 2 | Check and repair circuit between AUTOSLAT 2 DC circuit| | POWER | | breaker C1070 on the P6-2 panel and connector D2773A pin| | | | 1 at SMC 2 M1507 (WDM 27-83-21).| .................................................................................| | |
| | DADC #1 | SMC 1 | Check and repair circuit between connector D309A pins 56| | INACTIVE | | and 57 at DADC 1 M196 and connector D2771B pins 4 and 14| | | | at SMC 1 M1506 (WDM 27-32-12).| | | | If the problem continues, replace DADC 1 M196| | | | (MM 34-12-01/401).| .................................................................................| | |
| | DADC #2 | SMC 2 | Check and repair circuit between connector D311A pins 56| | INACTIVE | | and 57 at DADC 2 M368 and connector D2773B pins 4 and 14| | | | at SMC 2 M1507 (WDM 27-32-22).| | | | If the problem continues, replace DADC 2 M368| | | | (MM 34-12-01/401).| .................................................................................| | |
| | FLAP #1 | SMC 2 | Check and repair circuit between connector D275 pins 4,| | INACTIVE | | 5, 7, 8, and 9 at the left flap position transmitter T427| | | | and connector D2773B pins 30, ground, 5, 25, and 15 at| | | | SMC 2 M1507 (WDM 27-32-22).| | | | If the problem continues, replace left flap position| | | | transmitter T427 (MM 27-58-12/401).| | | | | | | | | | | | | 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 02 Page 116 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 | .................................................................................| | |
| | FLAP #2 | SMC 1 | Check and repair circuit between connector D229 pins 4,| | INACTIVE | | 5, 7, 8, and 9 at the right flap position transmitter| | | | T428 and connector D2771B pins 30, ground, 5, 25, and 15| | | | SMC 1 M1506 (WDM 27-32-12).| | | | If the problem continues, replace right flap position| | | | transmitter T428 (MM 27-58-12/401).| .................................................................................| | |
| | FLAP SYN | SMC 1 | Check and repair circuit between connector D229 pins 4,| | INVALID | | 5, 7, 8, and 9 at the right flap position transmitter| | | | T428 and connector D2771B pins 30, ground, 5, 25, and 15| | | | SMC 1 M1506 (WDM 27-32-12).| .................................................................................| | |
| | FLAP SYN | SMC 2 | Check and repair circuit between connector D275 pins 4,| | INVALID | | 5, 7, 8, and 9 at the left flap position transmitter T427| | | | and connector D2773B pins 30, ground, 5, 25, and 15 at| | | | SMC 2 M1507 (WDM 27-32-22).| .................................................................................| | |
　
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