R  Subtask 57-52-00-010-072  
R  D. Get Access  
R  (1) Put the access platform in position below the Rib 12 of the inboard  
R  flap at zone 581(681).  
R  (2) Remove and discard the covers to the inspection holes in the lower  
R  skin each side of the Rib 12.  
R  (3) Make sure that the applicable inspection holes are clear of unwanted  
R  material.  
R  (4) Put the spark-proof lamp adjacent to the inspection area.  
R  4. Procedure_________  
R  (Ref. Fig. 621/TASK 57-52-00-991-021)  
R  CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING_______  
R  EDGE:  
R  - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.  
R  - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.  
R  - MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY.  
R  INCORRECT INSTALLATION CAN CAUSE DAMAGE.  
R  Subtask 57-52-00-280-059  
R  A. Inspection  
R  (1) Do a special detailed inspection of the internal support brackets of  
R  the pylon aft fairing attachment LH/RH (Ref. NTM 575230 PART 9).  
R  NOTE : If necessary, refer to the ASRM (Ref. ASRM 575200) for the____  
R  correct repair procedure. If the defect is not included in  
R  this repair, you must request a procedure from Airbus  
R  Industrie.
R Inboard Flap - Pylon Fairing Internal Support Brackets - Inspection Area R Figure 621/TASK 57-52-00-991-021
 1EFF : 301-399, 1 57-52-00Page A625 1 1 May 01/04 1 1 1CES 1
R  5. Close-up________  
R  Subtask 57-52-00-410-074  
R  A. Close Access  
R  (1) Remove the spark-proof lamp from the inspection area.  
R  (2) Make sure that the work area is clean and clear of tool(s) and other  
R  items.  
R  (3) Use BONDING AND ADHESIVE COMPOUNDS (Material No. 08-061A), cut to the  
R  correct dimensions, to make new covers for the inspection holes.  
R  (4) Install the new covers on the inspection holes.  
R  Subtask 57-52-00-865-098  
R  B. Remove the safety clip(s) and the tag(s) and close this(these) circuit  
R  breaker(s):  
R  6CV, 8CV.  
R  Subtask 57-52-00-860-064  
R  C. Aircraft Maintenance Configuration  
R  (1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat  
R  control lever.  
R  (2) Retract the flaps (Ref. TASK 27-50-00-866-009).  
R  Subtask 57-52-00-942-073  
R  D. Removal of Equipment  
R  (1) Remove the access platform(s).  
R  (2) Remove the safety barriers.  
R  (3) Remove the warning notice(s).  
R  (4) Remove the ground support and maintenance equipment, the special and  
R  standard tools and all other items.
R  TASK 57-52-00-210-005  
R  Detailed Visual Inspection of Inboard Double Slotted Flap, End Rib, Including  
R  Interconnection Strut Attachment Bracket and Lever, LH/RH  
R  WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU_______  
R  START A TASK ON OR NEAR:  
R  - THE FLIGHT CONTROLS  
R  - THE FLIGHT CONTROL SURFACES  
R  - THE LANDING GEAR AND THE RELATED DOORS  
R  - COMPONENTS THAT MOVE.  
R  WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING_______  
R  GEAR.  
R  CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:_______  
R  - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.  
R  - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.  
R  - MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY.  
R  INCORRECT INSTALLATION CAN CAUSE DAMAGE.  
R  1. Reason for the Job__________________  
R  Refer to the MPD TASK: 575231-01  
R  2. Job Set-up Information______________________  
R  A. Fixtures, Tools, Test and Support Equipment  
R  ------------------------------------------------------------------------------- 
R  REFERENCE  QTY DESIGNATION  
 
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