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R  PANEL DESIGNATION IDENT. LOCATION 
R  -------------------------------------------------------------------------------
R  49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 
R  121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 
R  Subtask 57-52-00-010-066 
R  D. Get Access 
R  (1) Put the access platform in position below the zone 581(681). 
R  (2) Remove the applicable access panel: 
R  - for the left wing, remove 581AT 
R  - for the right wing, remove 681AT. 
R  (3) Remove the inboard flap seals (Ref. TASK 27-54-61-000-005). 
R  (4) Put the spark-proof lamp adjacent to the inspection area. 
R  4. Procedure_________ 
R  (Ref. Fig. 615/TASK 57-52-00-991-015) 
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 57-52-00-110-069 
R  A. Preparation for Inspection 
R  (1) Use a MISCELLANEOUS (Material No. 19-003), made moist with CLEANING 
R  AGENTS (Material No. 11-026) to clean the external surface of the 
R  trunnion attachment bracket. 

R 1EFF : 301-399, 1 57-52-00Page 691 1 1 May 01/04 1 1 1CES 1R Inboard Flap - Trunnion and Attachment Bracket - Inspection Area R Figure 615/TASK 57-52-00-991-015

R 1EFF : 301-399, 1 57-52-00Page 692 1 1 May 01/04 1 1 1CES 1

R Subtask 57-52-00-210-059

R  B. Detailed Visual Inspection of Inboard Double Slotted Flap, Trunnion 
R  Attachment Bracket, LH/RH. 
R  (1) Do an inspection of the external surface of the trunnion attachment 
R  bracket and the inboard trunnion, where it can be seen. Make sure 
R  that: 
R  - there is no damage 
R  - there is no corrosion 
R  - there are no cracks or scores 
R  - the surface protection is in the correct condition. 
R  NOTE : If necessary, refer to the ASRM (Ref. ASRM 575200) for the____ 
R  correct repair procedure. 
R  5. Close-up________ 
R  Subtask 57-52-00-410-066 
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) Install the inboard flap seals (Ref. TASK 27-54-61-400-007). 
R  (4) Install the applicable access panel: 
R  - for the left wing, install 581AT 
R  - for the right wing, install 681AT. 
R  Subtask 57-52-00-865-085 
R  B. Remove the safety clip(s) and the tag(s) and close this(these) circuit 
R  breaker(s): 
R  6CV, 8CV. 
R  Subtask 57-52-00-860-051 
R  C. Aircraft Maintenance Configuration 
R  (1) Fully retract the flaps (Ref. TASK 27-50-00-866-009). 

R 1EFF : 301-399, 1 57-52-00Page 693 1 1 May 01/04 1 1 1CES 1

R  Subtask 57-52-00-942-067 
R  D. Removal of the 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 1EFF : 301-399, 1 57-52-00Page 694 1 1 May 01/04 1 1 1CES 1

R  TASK 57-52-00-220-009 
R  Special Detailed Inspection of Inboard Double Slotted Flap, Trunnion Attachment 
R  Bracket, including Inboard Trunnion, 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. 
　
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