R  **ON A/C 001-099, 101-149, 151-199, 201-299,
R  57-51-00-991-025 Fig. 626 **ON A/C ALL
 3. Job Set-up
__________
 Subtask 57-51-00-941-080

 A. Safety Precautions
 (1)
 Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.

 (2)
 Put warning notices to tell persons not to operate the flaps or slats.

 (3)
 Put the safety barriers in position.

 Subtask 57-51-00-865-105

 B. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
 Subtask 57-51-00-010-081
 C. Get Access
 (1)
 Put the access platform in position below the applicable aileron, zone 575(675).

 (2)
 Remove the access panels:

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

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

 4. Procedure
_________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 626/TASK 57-51-00-991-025)
 **ON A/C ALL
 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.

 Aileron Hinge Pins
 Figure 626/TASK 57-51-00-991-025

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-51-00Page A658 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 57-51-00-020-081

 A. Remove Items for Inspection
 (1) One at a time, remove the five hinge pins from each aileron and replace them with the slave bolts (Ref. TASK 27-14-41-000-001).
 Subtask 57-51-00-110-090
 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 57-51-00-220-081
 C. Inspection
 (1) Examine the hinge pins for:
 -damage
 -scratches and/or scores
 -corrosion
 -correct condition of the surface protection.
 NOTE : If necessary, refer to the ASRM (Ref. ASRM 575100) for the

____
 correct repair procedure.

 Subtask 57-51-00-420-079
 D. Install items after Inspection.
 (1) One at a time, remove the five slave bolts from each aileron and replace with the hinge pins (Ref. TASK 27-14-41-400-001).
 5. Close-up
________ Subtask 57-51-00-410-082
 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.

R 1EFF : ALL 1 57-51-00Page A659 1 1 Nov 01/04 1 1 1CES 1 Subtask 57-51-00-865-106

 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 16CE1, 16CE2, 5CV, 15CE1, 15CE2, 7CV.
 Subtask 57-51-00-942-081
 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.

R 1EFF : ALL 1 57-51-00Page A660 1 1 Nov 01/04 1 1 1CES 1 TASK 57-51-00-210-003

 General Visual Inspection of Outer Wing, Bottom Skin Lower Surface, Aft of Rear Spar Between Rib 1 and Rib 9 Excluding Areas Covered by Flap Track 2...
 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
　
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