-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 lower skin

 -
the attachment structure of the outboard flap support.

 Subtask 57-53-00-210-055
 B. Inspection
 (1) Make a detailed inspection of the outboard flap support at track 3, including:
 -RIB5
 -
the fitting assembly and attachment structure, internal and external

 -
the inner and outer doubler.
 Make sure that:

 -
there is no corrosion

 -
there are no cracks

 -the protective treatment is in the correct condition.
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 Outboard Flap
 Figure 606A/TASK 57-53-00-991-007-A12 (SHEET 1)

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 Outboard Flap
 Figure 606A/TASK 57-53-00-991-007-A22 (SHEET 2)

R 1EFF : 057-099, 101-149, 151-199, 201-299, 1 57-53-00Page 639 1401-499, 1Aug 01/05 1 1 1CES 1 NOTE : If necessary, refer to the ASRM (Ref. ASRM 575321) for the

____
 correct repair procedure.

 5. Close-up
________
 **ON A/C 001-049, 051-056,
 Subtask 57-53-00-410-054
 A. Close Access
 (Ref. Fig. 606/TASK 57-53-00-991-007)

 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

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

 (3)
 Install the applicable access panels (Ref. TASK 57-55-11-400-001):

 -
for the left wing, install 532AT, 532CB

 -
for the right wing, install 632AT, 632CB.

 **ON A/C 057-099, 101-105, 151-199, 201-214,
 Subtask 57-53-00-410-054-A
 A. Close Access
 (Ref. Fig. 606A/TASK 57-53-00-991-007-A)

 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the applicable access panels (Ref. TASK 57-55-11-400-001):

 -
for the left wing, install 532AT, 532CB

 -
for the right wing, install 632AT, 632CB.

 (3)
 Install the new inspection hole covers as follows:

 (a)
 Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) clean the external surfaces around the applicable inspection holes.

 (b)
 Use BONDING AND ADHESIVE COMPOUNDS (Material No. 08-061A) cut to the correct dimensions, to make new covers for the applicable inspection holes.

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 (c) Install the new covers on the applicable inspection holes.

R **ON A/C 106-149, 215-299, 401-499,
 Subtask 57-53-00-410-054-B
 A. Close Access
 (Ref. Fig. 606A/TASK 57-53-00-991-007-A)

 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the applicable access panels (Ref. TASK 57-55-11-400-001):

 -
for the left wing, install 532AT, 532CB

 -
for the right wing, install 632AT, 632CB.

 (3) Install the rubber grommets in the applicable inspection holes. R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 57-53-00-865-062
 B. Make sure that this(these) circuit breaker(s) is(are) closed: 6CV, 8CV.
 Subtask 57-53-00-860-105
 C. Aircraft Maintenance Configuration
 (1) Fully retract the flaps (Ref. TASK 27-50-00-866-009).
 Subtask 57-53-00-942-055

 D. Removal of Equipment
 (1)
 Remove the warning notice(s).

 (2)
 Remove the access platform(s).

 (3)
 Remove the safety barriers.

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

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 TASK 57-53-00-220-004

 Special Detailed Inspection of Outboard Flap Support at Track 3, including RIB5, Fitting Assembly and Attachment Structure, Internal and External, LH/RH
　
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