S 862-019

 (2)  
Connect the electrical connectors to the spoiler control shutoff valves.

 S 862-020

 (3)  
Set the FLT CONTROL SPOILER A and B switches on the forward overhead panel to the ON position.

 S 862-021

 (4)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P6-2 Panel
 1) SHUTOFF VALVES - SPOILER

 S 862-022
 (5)  Pressurize the hydraulic reservoirs if it is necessary
 (AMM 29-09-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-61-00
 ALL  ú ú 01 Page 206 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 FLIGHT SPOILER CONTROL SYSTEM - ADJUSTMENT/TEST
_______________________________________________
 1.  General_______
 A.  There are three tasks in this procedure. There is a task for the operational test, the adjustment and the system test of the spoiler control system.
 B.  The spoiler control system gives lateral control and speed brake signals to the flight spoiler actuators through the spoiler mixer. The speed brake signals also control the ground spoilers.
 C.  You must not use the decals installed on the aileron control wheels during the adjustment or the test of the spoiler control system. The decals are for flight crew use only.
 D.  Before you do the adjustment or the test of the spoiler control system, the adjustment of these systems must be correct:
 (1)  
The aileron control system (Ref 27-11-00/501).

 (2)  
The trailing edge flaps (Ref 27-51-00/501).

 (3)  
The speed brake system (Ref 27-62-00/501).

 TASK 27-61-00-715-001
 2.  Spoiler Control System Operational Test_______________________________________
 A.  General
 (1)  
You can use the operational test to quickly give the status of the spoiler control system. You can do this test without special tools or equipment.

 B.  
References

 (1)  
27-61-00/201, Spoiler Control System

 C.  
Access

 (1)  
Location Zone
 101, 102 Control Cabin

 D.  
Procedure

 (1)
Supply the systems A and B hydraulic power (Ref 27-61-00/201).

 S 715-005

 (2)
Turn the captain's aileron control wheel fully clockwise.

 (a)  
Make sure the No. 6 and 7 flight spoilers move to the up position.

 S 865-004
 S 715-006
 (3)
Turn the captain's aileron control wheel fully counterclockwise.

 (a)  
Make sure the No. 2 and 3 flight spoilers move to the up position.

 S 715-007
 (4)  
Turn the captain's aileron control wheel to the neutral position.

 (a)  
Make sure the flight spoilers move to the retracted position.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-61-00
 ALL  ú ú 01 Page 501 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 715-008
 (5)  
Move the speed brake lever from the DOWN position to the UP position.

 (a)  
Make sure the spoilers move to the up position.

 S 715-009
 (6)  
Move the speed brake lever from the UP position to the DOWN position.

 (a)  
Make sure the flight spoilers move to the retracted position.

 S 865-010
 (7)  Remove the systems A and B hydraulic power (Ref 27-61-00/201).
 TASK 27-61-00-825-002
 3.  Spoiler Control System Adjustment_________________________________
 A. Special Tools and Equipment
 (1)  4MIT65B80307-1 Control Surface Protractor (2 Necessary)
 NOTE: You will use one protractor with the stand to measure the
　
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 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 5(27)