(3)
Remove the access panels 475CL, 485CL, 476CR, 486CR.
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 618/TASK 57-51-00-991-019)
**ON A/C ALL
Subtask 57-51-00-110-072
A. Preparation for Inspection
(1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the bottom wing skin lower surface, aft of the rear spar, under the pylon fairing.
Subtask 57-51-00-280-050
B. Inspection
(1) Do a special detailed inspection of the outer wing bottom skin lower surface, aft of the rear spar under the pylon fairing (Ref. NTM 57-51-63 PART 6).
NOTE : If necessary, refer to the ASRM (Ref. ASRM 575100) 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 57-51-00-410-071
A. Close Access
(1)
Install the applicable aft fixed fairing (Ref. TASK 54-54-00-400-001).
(2)
Install the access panels 475CL, 485CL, 476CR, 486CR.
Outer Wing Bottom Skin
Figure 618/TASK 57-51-00-991-019
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-51-00Page A610 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 57-51-00-942-070
B. Removal of Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the warning notice(s).
(3)
Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER from the flap/slat control lever.
(4)
Remove the safety barriers.
(5)
Remove the access platform(s).
(6)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 57-51-00Page A611 1 1 May 01/04R 1 1 1CES 1
TASK 57-51-00-220-012
Special Detailed Inspection of Outer Wing Bottom Skin Lower Surface Aft of the Rear Spar Around the Flap Track 2 Forward Fittings
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
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.
1. Reason for the Job
__________________
Refer to the MPD TASK: 575164-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific non metallic scraper No specific safety barriers No specific warning notices No specific access platform 2.5 m (8 ft. 2 in.) 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-026 GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
1EFF : ALL 1 57-51-00Page A612 1 1 May 01/04R 1 1 1CES 1
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
57-55-11-000-001 Removal of the Flap Track Fairings Nos. 2, 3 and 4 R 57-55-11-000-004 Removal of the Flap Track Fairings Nos. 2, 3 and 4 57-55-11-400-001 Installation of the Flap Track Fairings Nos. 2, 3 and
4 R 57-55-11-400-004 Installation of the Flap Track Fairings Nos. 2, 3 and R 4
NTM 57-51-64 PART 6
ASRM 575100 (for corrective action)
57-51-00-991-020 Fig. 619
3. Job Set-up
__________
Subtask 57-51-00-941-070
A. Safety Precautions
(1)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
(2)
Put the safety barriers in position.
(3)
Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.
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