(j)  
Make sure the tension in the cables is in the limits.

 (k)  
Install the lock clips on the turnbuckles.

 (l)  
Remove the rig pins A/S-1, A/S-1A and A/S-3.

 S 724-019
 (11)
 Do the test of the spoiler control quadrant (Ref 27-61-41/501).

 G.  
Put the Airplane Back to Its Usual Condition

 (1)  
Close the forward access door.

 S 414-021

 (2)  
Install the right floor panel between the seat tracks at the second window aft of the wing escape hatch:

 (a)  
Install the floor panel (Ref 53-21-00/401).

 (b)  
Install the carpet on the floor panel (Ref 25-27-15/401).

 (c)  
Install the seats (Ref/25-22-00/201).

 S 414-020
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 27-61-41
 ALL  ú ú 01 Page 408 ú Jul 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 SPOILER CONTROL QUADRANT - ADJUSTMENT/TEST
__________________________________________
 1.  General_______
 A.  There is one task in this procedure, a functional test of the spoiler control quadrant.
 TASK 27-61-41-725-001
 2.  Spoiler Control Quadrant Functional Test________________________________________
 A.  Special Tools and Equipment
 (1)  
4MIT65B80307-1 Control Surface Protractor (3 necessary)

 (2)  
F71292-17 Control Surface Protractor Stand (optional) (2 necessary)

 (3)  
F72790 Aileron Control Wheel Protractor Mount

 (4)  
Rig Pin A/S-4 - 0.311 +0.000/-0.002 inch diameter, 6.70 |0.25-inches long (F70207-11)

 NOTE: The rig pin is a part of the kit F70207-69, -78, or -83.
____
 B.  References
 (1)  
24-22-00/201, Manual Control

 (2)  
27-61-00/201, Spoiler Control System

 C.  
Access

 (1)  
Location Zone 101, 102 Control Cabin 307, 407 Wing Trailing Edge Outboard Flap and Spoilers

 D.  
Prepare for the Functional Test

 S 485-002
 (1)  
Install the protractor mount and the protractor on the captain's aileron control wheel.

 S 485-003

 (2)  
Install the protractor stand and the protractor on the spoilers No. 2 and 6.

 NOTE: You can use hand held protractors on the spoilers.
____
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 27-61-41
 ALL  ú ú 02 Page 501 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 865-004
 (3)  
Supply the electrical power (Ref 24-22-00/201).

 S 865-005

 (4)
Supply the systems A and B hydraulic power (Ref 27-61-00/201).

 S 865-006

 (5)  
Put the speed brake lever in the DOWN position.

 S 865-007

 (6)  
Put the aileron in the neutral position.

 NOTE: The ailerons are in the neutral position when you can easily
____ install the rig pin A/S-4 in the aileron bus drums.
 (a)  
Remove the rig pin A/S-4.

 E.
Do the Functional Test of the Spoiler Control Quadrant

 S 725-008
 (1)  
Turn the captain's aileron control wheel 87 degrees
 counterclockwise.

 (a)  
Make sure that the spoiler No. 2 moves 38 |2 degrees up from the retracted position.

 S 725-009
 (2)
Turn the captain's aileron control wheel 87 degrees clockwise.

 (a)  
Make sure that the spoiler No. 6 moves 38 |2 degrees up from the retracted position.

 S 725-010
 (3)
Turn the captain's aileron control wheel to the neutral position.

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

 F.
Put the Airplane Back to Its Usual Condition
　
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