Subtask 57-53-00-860-062
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) Extend the flaps fully (Ref. TASK 27-50-00-866-008).
(2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever on the panel 114VU.
Subtask 57-53-00-865-119
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 57-53-00-010-080
D. Get Access
(1) Put the access platform in position below the flap track 4 at zone 533(633).
(2) Remove the access panel 533AT (633AT) and the flap track 4 fairing 533CB (633CB) (Ref. TASK 57-55-11-000-004).
(3) Remove the access panel 587BB (687BB) in the bottom skin at track 4.
(4) Put the spark-proof lamp adjacent to the inspection area.
4. Procedure_________
(Ref. Fig. 629/TASK 57-53-00-991-033)
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 57-53-00-110-084
A. Preparation for Inspection
R R R R R (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean internally and externally: - the pendulum support - the internal support fitting.
Outboard Flap - Track 4 Support Attachments - Inspection Area Figure 629/TASK 57-53-00-991-033
1EFF : 301-399, 1 57-53-00Page B603 1 1 Nov 01/04R 1 1 1CES 1
Subtask 57-53-00-280-063
B. Inspection
R (1) Do a special detailed inspection (Ref. NTM 57-53-33 PART 9), R internally and externally of:
-
the internal support fitting at track 4
-
the pendulum support
-
the drive bracket
-
the attachment structure.
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 57-53-00-410-079
A. Close Access
(1)
Remove the spark-proof lamp from the inspection area.
(2)
Install the access panel 587BB (687BB).
(3)
Install the flap track 4 fairing 533CB (633CB) and access panel 533AT (633AT) (Ref. TASK 57-55-11-400-004).
(4)
Make sure that the work area is clean and clear of tool(s) and other items.
(5) Remove the access platform(s).
Subtask 57-53-00-865-120
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 57-53-00-860-063
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). Subtask 57-53-00-942-083
D. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : 301-399, 1 57-53-00Page B605 1 1 Nov 01/04R 1 1 1CES 1
TASK 57-53-00-210-005
Detailed Visual Inspection of Outboard Double Slotted Flap, Drive Linkage and Drive Fitting at Track 4, LH/RH
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
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
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.
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