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 (a)  Do this task to adjust the aileron power control unit if you cannot easily install the rigging pin A/S-4: "Aileron Power Control Unit Adjustment" (Ref 27-11-71/501).
 S 094-024
 (18)
 Remove the rig pins A/S-1, A/S-1A, A/S-4 and A/S-15.

 S 494-025

 (19)
 Install the protractor and protractor mount on the first officer's aileron control wheel.

 S 484-026

 (20)
 Install the adapter on the captain's control wheel (Fig. 404).

 S 224-027

 (21)
 Use a torque wrench on the adapter to measure the force necessary to turn the captain's aileron control wheel.

 NOTE: If the adapter is not available, put a tangent force to the
____
 captain's control wheel at a 6.5-inch radius.

 (a)  Turn the control wheel clockwise until the aileron starts to move. 1) Make sure the necessary force is not more than 220
 pound-inches torque or 33.8 pounds.
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A
737-300/400/500MAINTENANCE MANUAL
 (b)  
Continue to turn the control wheel to 20 degrees.

 1)  Make sure the necessary force is not more than 220 pound-inches torque or 33.8 pounds.

 (c)  
Continue to turn the control wheel to 40 degrees.

 1)  Make sure the necessary force is not more than 256 pound-inches torque or 39.4 pounds.

 (d)  
Continue to turn the control wheel to 75 degrees.

 1)  Make sure the necessary force is not more than 310 pound-inches torque or 47.7 pounds.

 (e)  
Do steps (a) thru (d) again in the counterclockwise direction.

 S 284-028
 (22)
 Compare the movement of the aileron control wheel to the movement of the aileron surface:

 (a)  
Turn the captain's aileron control wheel more than 87 degrees counterclockwise from the neutral position.

 (b)  
Make sure the left aileron moves up and the right aileron moves down in the specified limits (Fig. 405).

 (c)  
Turn the captain's aileron control wheel more than 87 degrees clockwise from the neutral position.

 (d)  
Make sure the left aileron moves down and the right aileron moves up in the specified limits (Fig. 405).

 F.  
Put the Airplane Back to Its Usual Condition

 S 094-029
 (1)  
Remove the control surface protractor and protractor mount from the aileron control wheel.

 (2)  
Remove the adapter from the captain's aileron control wheel.

 (3)  
Do this task: "Carpets Installation" (Ref 25-27-15/401).

 (4)
Do this task: "Passenger Seats Installation" (Ref 25-22-00/201).

 S 084-030
 S 424-031
 S 424-032
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 AILERON BODY QUADRANT - INSPECTION/CHECK
________________________________________
 1.  General_______
 A.  This procedure contains the task to do the inspection of the aileron body quadrant.
 B.  The procedure does not include instructions for access, removal, or replacement of the component after inspection of the worn parts. Refer to the Aileron Body Quadrant - Removal/Installation for instructions to do these tasks.
 TASK 27-11-91-206-001
 2.  Aileron Body Quadrant Inspection/Check______________________________________
 A.  References
 (1)  
27-11-91/401, Aileron Body Quadrant

 B.  
Access

 (1)  
Location Zone
 216,217 Main Wheel Well

 C.  
Procedure

 S 026-002
 (1)  
Do this task: "Aileron Body Quadrant Removal" (Ref 27-11-91/401).
　
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