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时间:2011-03-27 12:50来源:蓝天飞行翻译 作者:航空
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R  49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1  6CV  B07 
R  121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2  8CV  Q21

 

R  Subtask 57-52-00-010-072 
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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