(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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