Aileron Installation
Figure 401 (Sheet 1)

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MAINTENANCE MANUAL

Aileron Installation
Figure 401 (Sheet 2)

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MAINTENANCE MANUAL

 S 034-007
 (2)  
Disconnect the PCA input rods from the PCA input-levers (AMM 27-11-20/201).

 S 034-008

 (3)  
Disconnect the PCA's from the aileron (1) at the rod end (AMM 27-11-20/201).

 S 034-036

 (4)  
AIRPLANES WITH TWO BONDING JUMPERS AT HINGE 1;
 Disconnect the bonding jumpers (2, 3) from hinge 1.

 S 034-035

 (5)  
AIRPLANES WITH ONLY ONE BONDING JUMPER AT HINGE 1;
 Disconnect the single bonding jumper from hinge 1.

 S 034-038

 (6)  
Disconnect bonding jumpers (2, 3) from hinge 5.

 S 034-010

 (7)  
Disconnect the hinges from the aileron (1).

 S 024-011

 (8)  
Remove the aileron.

 NOTE: If it is necessary, the trailing edge flaps can be operated
____ after the aileron has been removed. Make sure that there are no loose components near the flaps before they are operated.
 S 034-012
 (9)  Remove the aileron sling from the aileron.
 TASK 27-11-21-424-013
 3. Install the Aileron
___________________
 A. General
 (1)  
This procedure contains only the data that is necessary to install the aileron. Refer to AMM 27-11-21/601 for the applicable wear-limit data.

 B.
Equipment

 (1)  
Aileron Sling - B27012-1

 C.
Consumable Materials

 (1)  
D00633 Grease, Corrosion Preventive - BMS 3-33 (recommended)

 (2)  
D00015 Grease, Corrosion Preventive - BMS 3-24 (optional)

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 (3)
D00013 Grease, Corrosion Preventive - MIL-G-23827 (optional)

 D.
Parts

 (1)  
Refer to the AIPC for more data on the components that are contained in the tables that follow:

 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 1 | Aileron | 27-11-21 | 01 | 140,145 | | | 2 | Jumper | | | 35 | | | 3 | Jumper | | | 40 | | | 4 | Bolt Retainer | | | 80 | | | 5 | Bolt | | | 15 | | | 6 | Washer | | | 25 | | | 7 | Nut | | | 30 | | | 8 | Bolt Retainer | | | 85 | | | 9 | Washer | | | 95 | | | 10 | Nut | | | 100 | | | 11 | Bushing | | | 105 | | | 12 | Washer | | | 95 | | | 13 | Bolt | | | 90 | | | 14 | Washer | | | 125 | | | 15 | Nut | | | 130 | | | 16 | Bushing | | | 135 | | | 17 | Washer | | | 120 | | | 18 | Bolt | | | 110,115 | 2.......….......…...................................…..........….....….........1
 (2)  GUN 003-999;
 Refer to the table that follows:

 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 19 | Control Rod | 27-18-01 | 01 | 60 | | | 20 | Screw | | | 20 | | | 21 | Bushing | | | 25 | | | 22 | Washer | | | 30 | | | 23 | Washer | | | 33 | | | 24 | Nut | | | 35 | 2......…........…...................................…..........…......…........1
　
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