(2)
Put the safety barriers in position.
Subtask 57-53-00-860-052
B. Aircraft Maintenance Configuration
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1) Fully extend the flaps (Ref. TASK 27-50-00-866-008).
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(2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever on the panel 114VU.
Subtask 57-53-00-865-109
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
Subtask 57-53-00-010-075
D. Get Access
(1)
Put the access platform in position below the inboard rib of the outboard flap at zone 587(687).
(2)
Remove the flap kink-seals (Ref. TASK 27-54-61-000-002).
(3)
Remove and discard the covers from the inspection holes on the inboard rib.
(4)
Make sure that the applicable inspection holes are clear of unwanted material.
(5)
Put the spark-proof lamp adjacent to the inspection area.
4. Procedure
_________ (Ref. Fig. 624/TASK 57-53-00-991-028) 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 57-53-00-110-071
A. Preparation for inspection
(1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the inspection holes.
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Outboard Flap - Inboard Rib - Inspection Area
Figure 624/TASK 57-53-00-991-028
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Subtask 57-53-00-280-061
B. Inspection
(1) Do a special detailed inspection of the internal surface of the inboard rib, the interconnection strut attachment bracket, the lever and the roller (Ref. NTM 575327 PART 9).
NOTE : If necessary, refer to the ASRM (Ref. ASRM 575300) for the
____ correct repair procedure. If the defect is not included in this repair, you must request a procedure from Airbus Industrie. ________
5. Close-up
Subtask 57-53-00-410-074
A. Close Access
(1)
Remove the spark-proof lamp from the inspection area.
(2)
Use BONDING AND ADHESIVE COMPOUNDS (Material No. 08-061A), cut to the correct dimensions, to make new covers for the inspection holes.
(3)
Install the new covers on the inspection holes.
(4)
Install the flap kink-seals (Ref. TASK 27-54-61-400-006).
(5)
Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 57-53-00-865-110
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 57-53-00-860-053
C. Aircraft Maintenance Configuration
(1)
Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.
(2)
Retract the flaps (Ref. TASK 27-50-00-866-009).
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Subtask 57-53-00-942-078
D. Removal of Equipment
(1)
Remove the access platform(s).
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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TASK 57-53-00-210-002
Detailed Visual Inspection of Outboard Double Slotted Flap, Internal Support Fitting at Track 3, Including Attachment Bracket, Drive Bracket ....
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