B.  
References

 (1)  
27-11-11/401, Ailerons

 (2)  
27-11-21/401, Aileron Balance Tab

(3)  
AMM 12-31-61/201, Wing Lower Surface Access Doors and Panels

(4)  
AMM 12-31-71/201, Wing Upper Surface Access Doors and Panels

 C.  
Access

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

 (2)  
Access Panel 8103 Removable Skin Panel - Aileron Lower Surface, LH 8113 Removable Skin Panel - Aileron Lower Surface, LH 8105 Aileron Access Panel (Removable Upper Surface), LH 8803 Removable Skin Panel - Aileron Lower Surface, RH 8813 Removable Skin Panel - Aileron Lower Surface, RH 8805 Aileron Access Panel (Removable Upper Surface), RH

 D.  
Remove the Aileron Tab Control Rods

 S 014-012
 (1)  
Do this task to remove the two aileron access panels at hinge locations 2 and 3 on the lower wing surface adjacent to the leadingedge of the aileron: "Aileron Removal" (AMM 12-31-61/201,AMM 12-31-71/201 and AMM 27-11-11/401).

 (2)  
Remove the retaining bolts of the aft balance panel seal.

 (3)  
Remove the retaining strip.

 (4)  
Remove the hinge pin retainer bolt.

 (5)  
Remove the hinge pins from the aft balance panel.

 S 034-013
 S 034-014
 S 034-015
 S 034-016
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-11-34
 ALL  ú ú 02.1 Page 401 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
AILERON 
SEE  A  AILERON HINGE POINT (4 LOCATIONS)  SEE B ADJUSTABLE TAB CONTROL RODS 

ROD ATTACH BOLTS FWD  INBD  TAB MASTS  AILERON BALANCE TAB 
A 
ROD END 
ROD ATTACH BOLT  ROD BARREL ROD PLUG  JAMNUT (TORQUE TO 100-140 JAMNUT (TORQUE TO 100 POUND-INCHES) POUND-INCHES)  ADJUSTABLE TAB CONTROL ROD 
B 
Aileron Tab Control Rods Installation Figure 401 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-11-34
 ALL  ú ú 01 Page 402 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 014-017
 (6)
Remove the aileron hinge access panel at the hinge location 2.

 S 024-018

 (7)  
Remove the control rods (Fig. 401):

 (a)  
Lift up the aileron trailing edge.

 (b)  
Remove the two nuts, bolts, and washers that connect the control rods to the forward fittings.

 (c)  
Remove the three screws that attach the forward part of the tab fairing to the tab.

 (d)  
Remove the tab fairing.

 (e)  
Remove two nuts, bolts, and washers that connect the control rods to the tab mast.

 (f)  
Remove the hinge bolts of the aileron tab.

 (g)  
Remove the tab to be clear of the aileron.

 (h)  
Carefully remove the control rods from the aileron.

 S 974-009
 (8)  Write down the lengths of the control rods.
 TASK 27-11-34-404-002
 3.  Aileron Tab Control Rods Installation (Fig. 401)_____________________________________
 A. Special Tools and Equipment
 (1)  
F80222-1 Aileron Tab Alignment Protractor

 B.
References

 (1)  
27-11-34/601, Aileron Tab Control Rods

 (2)  
27-11-11/401, Ailerons

 (3)  
27-11-00/501, Aileron and Aileron Trim Control System

 C.
Access

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

 (2)  
Access Panel 8103 Removable Skin Panel - Aileron Lower Surface, LH 8113 Removable Skin Panel - Aileron Lower Surface, LH 8105 Aileron Access Panel (Removable Upper Surface), LH 8803 Removable Skin Panel - Aileron Lower Surface, RH 8813 Removable Skin Panel - Aileron Lower Surface, RH 8805 Aileron Access Panel (Removable Upper Surface), RH
　
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