B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-026 GB DEF-STAN 68-148/1 R SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R 27-80-00-866-004 27-80-00-866-005 NTM 57-45-04 PART 9 ASRM 574000 57-45-00-991-007 Extending the Slats on the GroundRetracting the Slats on the Ground (for corrective action)Fig. 603
3. Job Set-up__________
Subtask 57-45-00-941-055
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.
Subtask 57-45-00-860-054
B. Aircraft Maintenance Configuration
(1) Extend the slats fully (Ref. TASK 27-80-00-866-004).
R (2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever.
R R (3) Put the adjustable access platform below the applicable wing leading edge at slat 4, zone 522(622).
Subtask 57-45-00-865-060
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 57-45-00-991-007)
Subtask 57-45-00-110-058
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 4 skin connection in the area of the lower girder at track ribs 9 and 10.
Subtask 57-45-00-280-051
R B. Inspection
R R (1) Do a special detailed inspection of the slat 4 skin connections in the area of the lower girder (ribs 9 and 10) (Ref. NTM 57-45-04 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 57-45-00-865-061
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 57-45-00-860-055
R B. Aircraft Maintenance Configuration
R R R (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat control lever.
R (2) Retract the slats fully (Ref. TASK 27-80-00-866-005).
Subtask 57-45-00-942-061
C. Removal of Equipment
(1)
Remove the warning notice(s).
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
(3)
Remove the access platform(s).
(4)
Remove the safety barriers.
(5)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 57-45-00Page 615 1 1 Aug 01/00R 1 1 1CES 1
Details of the Slat 4 Skin Connections in the area of the Lower Girder (Ribs 9 and 10) Figure 603/TASK 57-45-00-991-007- 12 (SHEET 1)
Details of the Slat 4 Skin Connections in the area of the Lower Girder (Ribs 9 and 10) Figure 603/TASK 57-45-00-991-007- 22 (SHEET 2)
TASK 57-45-00-200-007
Detailed Visual Inspection of Slat 4 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
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