-
for the left wing, remove 575AT, 575JB, 575KB, 575LB, 575MB

 -
for the right wing, remove 675AT, 675JB, 675KB, 675LB, 675MB.

 4. Procedure
_________
 (Ref. Fig. 605/TASK 57-51-00-991-004)
 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.
 Subtask 57-51-00-020-078
 A. Removal of the Aileron Hinge Pins
 (1)
 One at a time, remove the five hinge pins from the LH aileron and replace them with the SLAVE PIN - AILERON (98D27104004000) (Ref. TASK 27-14-41-000-001).

 (2)
 One at a time, remove the five hinge pins from the RH aileron and replace them with the SLAVE PIN - AILERON (98D27104004000) (Ref. TASK 27-14-41-000-001).

 1EFF : ALL 1 57-51-00Page 625 1 1 Aug 01/02R 1 1 1CES 1

 Aileron Hinge Pins Figure 605/TASK 57-51-00-991-004
 1EFF : 1 1R 1CES  ALL  1 11 1 57-51-00 Page 626 Aug 01/02

 Subtask 57-51-00-110-054

 B. Preparation for Inspection
 (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the hinge pins.
 Subtask 57-51-00-220-051
 C. Inspection
 (1) Examine the hinge pins for:
 -damage
 -scatches and/or scores
 -correct condition of the surface protection.
 NOTE : If necessary, refer to the ASRM (Ref. ASRM 575100) for the

____
 correct repair procedure.

 Subtask 57-51-00-420-070
 D. One at a time, remove the five slave bolts from each aileron and replace them with the hinge pins (Ref. TASK 27-14-41-400-001).
 5. Close-up
________ Subtask 57-51-00-410-053
 A. Close Access
 (1) Install the access panels:
 -for the left wing, install 575AT, 575JB, 575KB, 575LB, 575MB
 -for the right wing, install 675AT, 675JB, 675KB, 675LB, 675MB. Subtask 57-51-00-865-055
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 16CE1, 16CE2, 5CV, 15CE1, 15CE2, 7CV.
 1EFF : ALL 1 57-51-00Page 627 1 1 Aug 01/02R 1 1 1CES 1

 Subtask 57-51-00-942-053
 C. Removal of Equipment
 (1)
 Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER from the flap/slat control lever.

 (2)
 Remove the warning notice(s).

 (3)
 Remove the access platform(s).

 (4)
 Remove the safety barriers.

 (5)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 1EFF : ALL 1 57-51-00Page 628 1 1 Aug 01/02R 1 1 1CES 1

 TASK 57-51-00-220-003
 Detailed Visual Inspection of Outer Wing Trailing Edge Aileron Inboard and Outboard Actuator Fittings
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 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
__________________
 Refer to the MPD TASK: 575121-01
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific safety barriers No specific warning notices No specific access platform 3 m (9 ft. 10 in.) 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-026 GB DEF-STAN 68-148/1
　
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