(15)
 Connect the PCA input-rods to the PCA input-levers (AMM 27-11-20/201).

 S 824-028

 (16)
 Adjust the PCAs to aileron installation (AMM 27-11-00/501).

 S 434-029

 (17)
 Connect the aileron position-transmitter control-rod (19) to the aileron (1).

 (a)  
Install the screw (20), bushing (21), washers (22 and 23), and nut (24).

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757 MAINTENANCE MANUAL
 S 824-030
 (18)
 Adjust the position transmitter if a new aileron is installed or if the position sensor or its attach fittings are moved (AMM 27-18-00/501).

 S 824-039

 (19)
 Do the MCDP Test #66 - XDCR Outputs if the same aileron is installed and the position sensor or its attach fittings are not changed (FIM 22-00-04/101, Fig. 109).

 (a)  
If the aileron position is in the MCDP #66 test limits, the aileron installation is ok.

 (b)  
If the aileron position is not in the MCDP #66 test limits, adjust the position transmitter (AMM 27-18-00/501).

 G.
Put the Airplane Back to its Usual Condition

 S 864-031
 (1)  
Remove the power from the left, right, and center hydraulic systems (AMM 29-11-00/201).

 S 864-032

 (2)
Remove electrical power if it is not necessary (AMM 24-22-00/201).

 (3)
Replace the access panels that were removed (AMM 06-44-00/201).

 S 414-033
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 AILERON - INSPECTION/CHECK
__________________________
 1.  General_______
 A.  This procedure supplies the data that is necessary to examine the ailerons for wear. It does not supply the data that is necessary to access, remove, or install any of the aileron components. Refer to the aileron Removal/Installation procedure for this data.
 TASK 27-11-21-206-001
 2.  Examine the Aileron for wear____________________________
 A.  Access
 (1)  
Location Zones
 568 Aileron (Left)
 668 Aileron (Right)

 B.  
Procedure

 S 226-002
 (1)  Use the supplied data (Fig. 601) to examine the aileron and its components for too much wear.
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MAINTENANCE MANUAL

B-B
HINGES 1,2, AND 5 A-A
Aileron Wear Limits
Figure 601 (Sheet 1)

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MAINTENANCE MANUAL

E-E

Aileron Wear Limits
Figure 601 (Sheet 2)

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