CONTROL UNITS
CONTROL WHEEL

TO GET THE CORRECT CABLE TENSION, PERMIT A MINIMUM OF ONE HOUR AT A CONSTANT AMBIENT
TABLE I
TEMPERATURE OF |5`F FOR THE AIRFRAME TEMPERATURE TO BECOME STABLE

THE CABLE LOADS MUST NOT BE MORE THAN +10/0 POUNDS OF THE NOTED TABLE I VALUES WHEN YOU ADJUST THE SYSTEM
FOR THE NECESSARY REGULAR CHECKS WITHOUT THE SYSTEM DISCREPANCY REPORTS, THE CABLE TENSIONS CAN CHANGE +15/-30 POUNDS FROM THE TABLE I VALUES. FOR CABLE TENSION CHECKS THAT ARE THE RESULT OF THE SYSTEM DISCREPANCY REPORTS, THE TENSIONS CAN CHANGE |15 POUNDS FROM THE TABLE I VALUES. WHEN YOU ADJUST THE CABLES, TABLE I VALUES MUST BE MET WITH

THE CABLE LOADS MUST NOT BE MORE THAN |15 POUNDS OF THE TABLE I VALUES WHEN YOU ADJUST THE SYSTEM
FOR THE NECESSARY REGULAR CHECKS WITHOUT THE SYSTEM DISCREPANCY REPORTS, THE CABLE TENSIONS CAN CHANGE +15/-30 POUNDS FROM THE TABLE I VALUES. FOR CABLE TENSION CHECKS THAT ARE THE RESULT OF THE SYSTEM DISCREPANCY REPORTS, THE TENSIONS CAN CHANGE |15 POUNDS FROM THE TABLE I VALUES. WHEN YOU ADJUST THE CABLES, TABLE I VALUES MUST BE MET WITH

Aileron System Cable and Tension Location
Figure 406

90 70 50 30 -10 -30 -40 1 +10 110 TEMP `F  93 84 75 70 61 53 49 46 44 202 184 165 148 131 113 96 77 66 CABLE TENSION (POUNDS)2 3 133 124 115 107 82 74 68 99 90 AND AB AND ACBB 4 5 AND ABSB CABLES AA CABLES ABSA CABLES ACBA 2 3 

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (2)  
Access Panel 7218 Access Panel, LH 7418 Access Panel, RH 8101 Removable Skin Panel - Aileron Lower Surface, LH 8103 Removable Skin Panel - Aileron Lower Surface, LH 8110 Removable Skin Panel - Aileron Lower Surface, LH 8113 Removable Skin Panel - Aileron Lower Surface, LH 8801 Removable Skin Panel - Aileron Lower Surface, RH 8803 Removable Skin Panel - Aileron Lower Surface, RH 8810 Removable Skin Panel - Aileron Lower Surface, RH 8813 Removable Skin Panel - Aileron Lower Surface, RH 8104 Aileron Access Panel (Removable Upper Surface), LH 8105 Aileron Access Panel (Removable Upper Surface), LH 8106 Aileron Access Panel (Removable Upper Surface), LH 8107 Aileron Access Panel (Removable Upper Surface), LH 8804 Aileron Access Panel (Removable Upper Surface), RH 8805 Aileron Access Panel (Removable Upper Surface), RH 8806 Aileron Access Panel (Removable Upper Surface), RH 8807 Aileron Access Panel (Removable Upper Surface), RH

 F.
Procedure

 S 014-001
 (1)  
Remove the access panels on the lower wing surface at the balance panel.

 S 034-047

 (2)  
Disconnected the aileron from the balance panel:

 (a)  
Remove the retaining bolts of the aft balance panel seal (Fig. 402).

 (b)  
Remove the retaining strip.

 (c)  
Remove the retainer bolt and the hinge pins from the aft balance panel hinge.

 S 014-017
 (3)  
Remove the aileron access panels at the four hinge locations (Fig. 406).

 S 024-018

 (4)  
Remove the aileron:

 (a)  
Lift up the aileron trailing edge.

 (b)  
Remove the attach bolt of the aileron control rod (Fig. 404).

 (c)  
Disconnect the balance tab pushrods from the wing hinge fitting (Fig. 401).

 (d)  
Disconnect the bonding jumpers at number 1 and 4 hinge locations.

 (e)  
Hold the aileron.

 (f)  
Remove the cotter pins and nuts from the hinge bolts at the four hinge locations.

 (g)  
Remove the hinge bolts.

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 ú ú  ú 03.101 ú BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.  Page 409Jul 12/02 

A
737-300/400/500MAINTENANCE MANUAL
 (h)  Remove the aileron from the wing.
　
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