(b)
 Remove the nut (74), the bolt (73) and the locking plate (72).

 (c)
 Remove and discard the cotter pin (82) from the locking cap (81).

 (d)
 Remove the locking cap (81), the nut (80) and the washer (79).

 (11)
 For hinge No. 5, remove the nut (106), the bolt (97), the washers

 (98) and (105), and the bonding strap (99).

 (12)
 For hinge No.s 4 and 5, do the steps that follow:

 (a)
 Remove the nut (107), the bolt (95), the washers (96) and (108), and the bonding strap (90).

 (b)
 Remove the bolt (94) and the locking plate (93).

 (c)
 Remove and discard the cotter pin (104) from the locking cap (103).

 (d)
 Remove the locking cap (103), the nut (102) and the washer (101).

 (13)
 Make sure that the aileron is supported by the crane and remove the hinge pins (61) and (92). Move the aileron aft and away from the wing and put it on the trestle.

 (14)
 If the aileron is to be replaced, loosen the adjuster assemblies and remove the LIFTING FRAME ASSEMBLY (AILERON) from the aileron.

 Subtask 27-14-41-020-052-A
 B. Removal of the Bushes from the Hinges
 (1)
 For the hinge No. 1, remove the bush (78).

 (2)
 For the hinge No.s 2 and 3, remove the bushes (70) and (78).

 (3)
 For the hinge No.s 4 and 5, remove the bushes (91) and (100).

R 1EFF : 004-049, 053-099, 101-149, 151-199, 1 27-14-41Page 417 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C ALL

 TASK 27-14-41-400-001
 Installation of the Aileron
 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
 NOTICES ARE IN POSITION.

 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
_______
 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.

 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.

 -MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific crane
 No specific safety barriers
 No specific warning notice
 No specific access platform 3.8 m (12 ft. 6 in.)

R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
 (8.00 to 75.00 lbf.ft) SL90-313-5625 1 TOOL - INSTALLATION, TAB WASHERS STA-LOK NSA5454 SL90-313-7500 1 TOOL - INSTALLATION, TAB WASHERS STA-LOK NSA5454 SL90-315-5625 1 WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 SL90-315-7500 1 WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 98D27104000001 1 GUIDE CONE - AILERON 98D27104001000 1 LIFTING FRAME ASSEMBLY (AILERON) B. Consumable Materials

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-022  USA MIL-PRF-81322 GRADE 2
 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE
 (Ref. 20-31-00)

 Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 11-026 GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
 Material No. 15-007  AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
 Material No. 19-003  USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)

 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R 65 cotter pins 27-14-05 20 -080 R 82 cotter pin 27-14-05 31A-110 R 104 cotter pin 27-14-05 31A-110
 D. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-22-00-400-001  Installation of STA-LOK Nuts and Lockwashers
 20-28-00-912-004  Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
　
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