(1)  
Location Zone
 205 Electronic Compartment

 (2)  
Access Panel
 1201 Electronic Equipment Access Door

 C.  
Procedure

 S 864-010
 (1)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  
P6 Panel
 1) AUTOSLAT NO. 1 AC
 2) AUTOSLAT NO. 1 DC
 3) AUTOSLAT NO. 2 AC
 4) AUTOSLAT NO. 2 DC

 S 864-009
 CAUTION: YOU MUST DO THE STEPS IN THE SPECIFIED PROCEDURE WHEN YOU MOVE
_______ THE AUTOSLAT COMPUTER. STATIC DISCHARGE CAN CAUSE DAMAGE TO THE AUTOSLAT COMPUTER.
 (2)  
Obey the procedure for electrostatic discharge sensitive devices (Ref 20-40-12/201).

 S 024-003

 (3)  
Remove the autoslat computer from the shelf.

 TASK 27-83-11-404-004
 3.  Leading Edge Autoslat Computer Installation (Fig. 401)
___________________________________________
 A.  References
 (1)  
20-40-12/201, Electrostatic Discharge Sensitive Devices

 (2)  
27-83-11/501, Leading Edge Autoslat Computer

 B.  
Access

 (1)  
Location Zone
 205 Electronic Compartment

 (2)  
Access Panel
 1201 Electronic Equipment Access Door

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH AUTOSLAT ú

 27-83-11
 COMPUTER P/N 65-52818  ú ú 02 Page 401 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

A

Autoslat Computer Installation
Figure 401

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH AUTOSLAT ú

 27-83-11
 COMPUTER P/N 65-52818  ú ú 02 Page 402 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 C. Procedure
 S 864-005
 CAUTION: YOU MUST DO THE STEPS IN THE SPECIFIED PROCEDURE WHEN YOU MOVE
_______ THE AUTOSLAT COMPUTER. STATIC DISCHARGE CAN CAUSE DAMAGE TO THE AUTOSLAT COMPUTER.
 (1)  
Obey the procedure for electrostatic discharge sensitive devices (Ref 20-40-12/201).

 S 424-006

 (2)  
Install the autoslat computer on the shelf.

 S 864-007

 (3)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P6 Panel
 1) AUTOSLAT NO. 1 AC
 2) AUTOSLAT NO. 1 DC
 3) AUTOSLAT NO. 2 AC
 4) AUTOSLAT NO. 2 DC

 S 734-008
 (4)  Do this task: "Leading Edge Autoslat Computer Test"
 (Ref 27-83-11/501).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH AUTOSLAT ú

 27-83-11
 COMPUTER P/N 65-52818  ú ú 02 Page 403 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 LEADING EDGE AUTOSLAT COMPUTER - ADJUSTMENT/TEST
________________________________________________
 1.  General_______
 A.  This task is a test of the autoslat computer. Do this test after you replace the autoslat computer.
 TASK 27-83-11-715-027
 2.  Leading Edge Autoslat Computer Test___________________________________
 A.  General
 (1)  
This test is a check of the electrical connections between the autoslat computer and the external circuits of the autoslat system. The external systems must operate satisfactorily before you do this test.

 (2)  
The components of the autoslat system used in this test are the No. 1 and No. 2 autoslat computers (ASC 1 and ASC 2), the angle of airflow (AOA) sensors, the antiskid control unit, and the E-11 landing gear logic shelf.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 6(131)