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B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 08-061A D DAN 220 ALUMINIUM FOIL ADHESIVE TAPE (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R 27-50-00-866-008 27-50-00-866-009 27-54-62-000-003 27-54-62-400-003 27-55-11-000-001 57-55-11-400-001 NTM 57-53-05 PART 9 ASRM 5753000 57-53-00-991-018 Extension of the Flaps on the GroundRetraction of the Flaps on the GroundRemoval of the Leading Edge Panels 2 and 5 on the Outboard FlapInstallation of the Leading Edge Panels 2 and 5 on the Outboard FlapRemoval of the Instrumentation Position Pick-Off UnitInstallation of the Flap Track Fairings Nos. 2, 3 and 4(for corrective action) Fig. 617
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3. Job Set-up__________
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Subtask 57-53-00-941-072
A. Safety Precautions
R R (1) Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
(2) Put the safety barriers in position.
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Subtask 57-53-00-860-115
B. Aircraft Maintenance Configuration
(1)
Extend the flaps fully (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the
slat/flap control lever. R
Subtask 57-53-00-865-093
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 57-53-00-010-067
D. Get Access
(Ref. Fig. 617/TASK 57-53-00-991-018)
(1)
Put the access platform below the applicable wing trailing edge at flap track 4, zone 533 (633).
(2)
Remove the access panel 533AT (633AT) and the flap track 4 fairing 533CB (633CB) (Ref. TASK 27-55-11-000-001).
(3)
Remove the outboard flap leading edge panel 5 (Ref. TASK 27-54-62-000-003).
(4)
Remove and discard the covers from the inspection holes on the front spar.
(5)
Make sure that the applicable inspection holes are clear of unwanted material.
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Outboard Flap - Front Spar Splices and Attachment Areas
Figure 617/TASK 57-53-00-991-018
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4. Procedure_________
R (Ref. Fig. 617/TASK 57-53-00-991-018)
R 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.
R
Subtask 57-53-00-280-057
A. Inspection
(1) Do a special detailed inspection of the front spar splices and the attachment areas, internally and externally (Ref. NTM 57-53-05 PART 9).
NOTE : If necessary, refer to the ASRM (Ref. ASRM 5753000) for the____ correct repair procedure. If the defect is not included in this repair, you must request a procedure from Airbus Industrie.
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5. Close-up________
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Subtask 57-53-00-410-066
A. Close Access (Ref. Fig. 617/TASK 57-53-00-991-018)
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Use BONDING AND ADHESIVE COMPOUNDS (Material No. 08-061A) cut to the correct dimensions, to make new covers for the inspection holes.
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(3)
Install the new covers on the inspection holes.
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