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 (Fig. 401).
 (h)  Attach the aileron control rod to the wing quadrant clevis with
 the steps that follow:
 1) Connect the aileron control rod to the wing quadrant with
 bolt, washer, and nut.
 2) Tighten the nut to 60-85 pound-inches.
 3) Install the cotter pin.
 (i)  Connect the cables ABSA and ABSB to the turnbuckles, but keep
 the cable tension at zero.
 (j)  Make sure that the rig pin A/S-4 is installed (Fig. 402).
 (k)  Tighten the turnbuckles for each cable (ABSA and ABSB) to put
 the ailerons at the correct position (Fig. 403).
 NOTE: The index point B on the inboard end of each aileron____
 must align with the index point A on the adjacent wing
 structure (use a tolerance of |0.03 inch).
 (l)  Continue to tighten cables in equal increments until you get
 the correct tension (Fig. 404).
 (m)  Install the turnbuckle clip locks.

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A 737-300/400/500MAINTENANCE MANUAL
 (3)  S 414-010Install the access panels.
 (4)  S 494-011Install the protractor mount and the protractor on the captain's aileron control wheel.
 (5)  S 284-013Compare the movement of the aileron control wheel with 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 that the left aileron moves up and the right aileron moves down in the specified limits (Fig. 403). (c) Turn the captain's aileron control wheel more than 87 degrees clockwise from the neutral position. (d) Make sure that the left aileron moves down and the right aileron moves up in the specified limits (Fig. 403).
 (6)  S 094-012Remove the protractor and protractor mount from the captain's aileron control wheel.

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 AILERON WING QUADRANT - INSPECTION/CHECK
________________________________________
 1.  General_______
 A.  This procedure contains the task to do a check of the wing quadrant of the aileron.
 TASK 27-11-24-206-004
 2.  Aileron Wing Quadrant Inspection/Check______________________________________
 A.  References
 (1)  
27-11-24/401, Aileron Wing Quadrant

 B.  
Access

 (1)  
Location Zone 306 Wing Trailing Edge, Aileron and Control Tab, LH 406 Wing Trailing Edge, Aileron and Control Tab, RH

 C.  
Procedure

 S 026-001
 (1)  
Do this task: "Aileron Wing Quadrant Removal" (Ref 27-11-24/401).

 S 226-002

 (2)  
Do a check of the wing quadrant (Fig. 601):

 (a)  
Remove the parts to be examined.

 (b)  
Measure the dimensions of these parts.

 (c)  
Compare the part dimensions to the limit dimensions.

 (d)  
If the part dimension is out of tolerance, replace the part.

 (e)  
Install all the parts removed to do the check.

 S 426-003
 (3)  Do this task: "Aileron Wing Quadrant Installation" (Ref 27-11-24/401).
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
QUADRANT AILERON WING  A  B  ACCESS PANEL WING UPPER 
SEE  A  B  C 
FWD  INBD  A  C 
　
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