A. Safety Precautions
(1) Put the warning notices in the cockpit to tell persons not to operate the flaps or slats.
(2) Put the safety barriers in position.
Subtask 57-46-00-860-054
B. Aircraft Maintenance Configuration
(1)
Fully extend the slats (Ref. TASK 27-80-00-866-004).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever.
R (3) Put the access platform below the applicable wing leading edge at R slat 5, zone 515(615).
Subtask 57-46-00-865-060
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
4. Procedure_________
(Ref. Fig. 603/TASK 57-46-00-991-007)
Subtask 57-46-00-110-058
A. Preparation for Inspection
(1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING AGENTS (Material No. 11-026) to clean the slat 5 skin connections in the area of the lower girder at the track ribs 11 and 12.
Subtask 57-46-00-280-052
R B. Inspection
R R R (1) Do a special detailed inspection of the slat 5 skin connections in the area of the lower girder (ribs 11 and 12) (Ref. NTM 57-46-04 PART 9).
R R R R NOTE : If necessary, refer to the ASRM (Ref. ASRM 574000) 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 57-46-00-865-061
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 57-46-00-860-055
R R B. Aircraft Maintenance Configuration
(1) Make sure that the work area is clean and clear of tool(s) and other items.
R R (2) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.
R (3) Fully retract the slats (Ref. TASK 27-80-00-866-005).
Subtask 57-46-00-942-061
C. 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.
1EFF : ALL 1 57-46-00Page 615 1 1 Aug 01/00R 1 1 1CES 1
Details of the Slat 5 Skin Connections in the area of the Lower Girder (Track Ribs 11 and 12) Figure 603/TASK 57-46-00-991-007- 12 (SHEET 1)
Details of the Slat 5 Skin Connections in the area of the Lower Girder (Track Ribs 11 and 12) Figure 603/TASK 57-46-00-991-007- 22 (SHEET 2)
TASK 57-46-00-200-007
Detailed Visual Inspection of Slat 5 Trailing Edge, Lower Face, 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.
1. Reason for the Job
__________________
Refer to the MPD TASK: 574605-01
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 safety barriers
No specific warning notices
No specific adjustable access platform 3.5 m (11 ft. 6 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00) C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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