S 824-033

 (15)
 Adjust the cables ACBA and ACBB at turnbuckles to the specified tension (Fig. 402).

 S 094-034

 (16)
 Remove the rigging pin A/S-1A.

 NOTE: The rigging pin must be easy to remove.
____
 S 094-035
 (17)
 Remove the straightedge from the control wheels.

 S 864-036

 (18)
 Operate the control wheels through a minimum of two cycles.

 S 864-037

 (19)
 Put the control wheels at the center.

 S 834-038

 (20)
 Do a check of the rigging:

 (a)  With a clamp, attach the straightedge across the top ends of
 the captain's and the first officer's aileron control wheels.
 (b)  Make sure that all four ends of the control wheels touch the
 straightedge.
 NOTE:____ One end of the first officer's control wheel cannot be
 farther than 0.20 inch from the straightedge.

 S 434-039
 (21)
 Install the turnbuckle clip locks.

 S 434-040

 (22)
 Install the cable shields and clamps.

 S 824-041

 (23)
 Adjust the left aileron control cables AA and AB:

 (a)  
With a clamp, attach the straightedge across the top ends of the two aileron control wheels to keep them in the neutral position.

 NOTE: One end of the first officer's control wheel cannot be
____ farther than 0.20 inch from the straightedge.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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737-300/400/500MAINTENANCE MANUAL
 (b)  
Make sure the rigging pin A/S-15 is installed.

 (c)  
Make sure the trim roller in in the cam detent.

 (d)  
Tighten the left cables AA and AB to the specified tension (Fig. 402).

 (e)  
Remove the rigging pin A/S-15.

 (f)  
Move the captain's aileron control wheel through a minimum of two full cycles.

 (g)  
Install the rigging pins A/S-1, A/S-1A and A/S-15 to do a check on the rigging.

 (h)  
Make sure the cable tension is in the specified values (Fig. 402).

 (i)  
Remove all the rigging pins.

 (j)  
Install the turnbuckle clip locks.

 S 714-044
 (24)
 Do this task to do a test on the control wheel drum:  "Aileron Control Wheel Drum Adjustment Test" (AMM 27-11-51/501).

 S 824-042

 (25)
 Do this task:  "Roll Force Transducer Adjustment"
 (AMM 22-11-11/501).

 S 714-043

 (26)
 Do this task: "Roll Force Transducer Test" (AMM 22-11-11/501).

 S 714-046

 (27)
 AIRPLANES WITH THE AILERON FORCE LIMITER; Do this task: "Aileron Force Limiter Test" (AMM 22-11-13/501).

 S 414-079

 (28)
 Close the access door of the lower nose compartment.

 TASK 27-11-51-004-005
 4.  Aileron Control Wheel Drum Removal (With Ribs and Brackets Disconnected)__________________________________
 A. References
 (1)  
AMM 22-11-11/401, Roll Control Wheel Steering Force Transducer

 (2)  
22-11-13/401, Aileron Force Limiter

 B.
Access

 (1)  
Location Zone
 101 Control Cabin, LH
 102 Control Cabin, RH
 202 Lower Nose Compartment

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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737-300/400/500MAINTENANCE MANUAL
 C. Procedure
 S 024-047
 (1)  
Remove the control wheel drum (Fig. 401):

 (a)  
Disconnect the electrical connector of the roll force transducer (Fig. 401).
　
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