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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 
R
 3. Job Set-up__________ 
R
 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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R

 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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R

 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. 
R
 5. Close-up________ 
R
 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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