(2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the slat/flap control lever.

 Subtask 57-53-00-865-097
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-214,
 Subtask 57-53-00-010-068
 D. Get Access
 (Ref. Fig. 618/TASK 57-53-00-991-019)

 (1) Put the access platform below the applicable wing trailing edge at flap track 4, zone 533 (633).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page A617 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

 Outboard Flap
 Figure 618/TASK 57-53-00-991-019

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 57-53-00Page A618 1201-214, 1May 01/05 1 1 1CES 1

 (2)
 Remove the applicable access panels (Ref. TASK 57-55-11-000-001):

 -
for the left wing, remove 533AT, 533CB

 -
for the right wing, remove 633AT, 633CB.

 (3)
 Remove the outboard flap leading edge panel 5 (Ref. TASK 27-54-62-000-003).

R **ON A/C 106-149, 215-299, 401-499,
 Subtask 57-53-00-010-068-A
 D. Get Access
 (Ref. Fig. 618A/TASK 57-53-00-991-019-A)

 (1)
 Put the access platform below the applicable wing trailing edge at flap track 4, zone 533 (633).

 (2)
 Remove the applicable access panels (Ref. TASK 57-55-11-000-001):

 -
for the left wing, remove 533AT, 533CB

 -
for the right wing, remove 633AT, 633CB.

 (3)
 Remove and keep the rubber grommets from the applicable inspection holes.

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 4. Procedure
_________
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-214,

 (Ref. Fig. 618/TASK 57-53-00-991-019) R **ON A/C 106-149, 215-299, 401-499,
 (Ref. Fig. 618A/TASK 57-53-00-991-019-A)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page A619 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

 Outboard Flap
 Figure 618A/TASK 57-53-00-991-019-A12 (SHEET 1)

R 1EFF : 106-149, 215-299, 401-499, 1 57-53-00Page A620 1 1 Aug 01/05 1 1 1CES 1

 Outboard Flap
 Figure 618A/TASK 57-53-00-991-019-A22 (SHEET 2)

R 1EFF : 106-149, 215-299, 401-499, 1 57-53-00Page A621 1 1 Aug 01/05 1 1 1CES 1

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,

 Subtask 57-53-00-110-067
 A. Preparation for Inspection
 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) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the external surfaces of:
 -
the outboard flap upper and lower skins

 -
the attachment fitting.

 Subtask 57-53-00-210-067
 B. Inspection
 (1) Make a detailed inspection of:
 -
the external parts of the pendulum support that you can see

 -
the lower skin around the pendulum support. Make sure the inner and

 outer doubler is fully inspected.
 Make sure that:

 -
there is no corrosion

 -
there are no cracks

 -the surface protection is in the correct condition.
 NOTE : If necessary, refer to the ASRM (Ref. ASRM 575321) for the
____
 correct repair procedure.

 5. Close-up
________
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-214,
 Subtask 57-53-00-410-067
 A. Close Access
 (Ref. Fig. 618/TASK 57-53-00-991-019)

 (1) Make sure that the work area is clean and clear of tool(s) and other items.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-53-00Page A622 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

 (2)
 Install the leading edge panel 5 (Ref. TASK 27-54-62-400-003).
　
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