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

 (b)  
Quickly move the speed brake lever from the DOWN position to the UP position. 1) Make sure all flight spoilers move to the extended position

 in less than 1 second.

 (c)  
Quickly move the speed brake lever from the UP position to the DOWN position: 1) Make sure all flight spoilers move to the retracted

 position in less than 1 second.
 S 735-051
 (9) Do a test of the autopilot aileron actuator (Ref 22-11-25/501).
 NOTE: The autopilot actuator test for the ailerons also does the
____ test of the autopilot authority for the spoilers.
 G. Put the Airplane Back to Its Usual Condition
 S 865-052
 (1) Remove the systems A and B hydraulic power (Ref 27-61-00/201).
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A 737-300/400/500MAINTENANCE MANUAL
 (2)  S 085-053Remove the protractor and the protractor mount from the captain's aileron control wheel.
 (3)  S 085-054Remove the protractor and the protractor stands from the flight spoilers No. 2 and 7.
 (4)  S 865-055Remove the electrical power (Ref 24-22-00/201).

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A
737-300/400/500MAINTENANCE MANUAL
 FLIGHT SPOILER - REMOVAL/INSTALLATION
_____________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There is a task for the removal and a task for the installation of the flight spoilers.
 B.  The graphite/composite flight spoilers and the aluminum/fiberglass flight spoilers are interchangeable.
 TASK 27-61-11-004-001
 2.  Flight Spoiler Removal (Fig. 401)______________________
 A.  Special Tools and Equipment
 (1)  
F80017-33 Spoiler Ground Lock (Recommended). (Use with Chamfered Flight Spoiler Clevis)

 (2)  
F80017-23 Spoiler Ground Lock (Alternative). (Use with Chamfered Flight Spoiler Clevis)

 (3)  
C27047-16 Spoiler Ground Lock (Use with Rounded Flight Spoiler Clevis)

 B.  
References

 (1)  
22-11-27/401, Spoiler Position Sensor

 (2)  
24-22-00/201, Manual Control

 (3)  
27-61-00/201, Flight Spoiler Control System

 C.  
Access

 (1)  
Location Zone 307, 407 Wing Trailing Edge Outboard Flap and Spoilers

 D.  
Procedure

 S 864-002
 (1)  
Supply the electrical power (Ref 24-22-00/201)

 S 864-003

 (2)
Supply systems A and B hydraulic power (Ref 27-61-00/201).

 S 864-005

 (3)  
Move the flap control lever to the 40-unit position to extend the trailing edge flaps.

 (4)  
Move the speed brake lever to the UP position to lift the spoilers.

 (5)
Remove the systems A and B hydraulic power (Ref 27-61-00/201).

 S 494-008

 (6)  
Install the spoiler ground locks on the actuator for the applicable spoiler.

 S 024-009

 (7)  
Remove the flight spoiler:

 (a)  
Remove the bolt that attaches the rod end of the spoiler actuator to the spoiler.

 (b)  
Disconnect the bonding jumpers from the spoiler.

 S 864-006
 S 864-007
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