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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 (1) Fully extend the flaps (Ref. TASK 27-50-00-866-008).
R (2) Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is R installed on the flap/slat control lever on the panel 114VU.


R  Subtask 57-52-00-865-093 
R  C. Open, safety and tag this(these) circuit breaker(s): 
R  -------------------------------------------------------------------------------
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 57-52-00-010-070 
R  D. Get Access 
R  (1) Put the access platform in position below the flap track 2 at zone 
R  531(631). 
R  (2) Remove the applicable flap track fairings (Ref. TASK 57-55-11-000-
R  004): 
R  - for the left wing, remove 531AT, 531CB 
R  - for the right wing, remove 631AT, 631CB. 
R  (3) Remove the flap kink-seals (Ref. TASK 27-54-61-000-002). 
R  (4) Put the spark-proof lamp adjacent to the inspection area. 
R  4. Procedure_________ 
R  (Ref. Fig. 619/TASK 57-52-00-991-019) 
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 57-52-00-210-061 
R  A. Inspection. 
R  (1) Do an inspection of the carriage attachment bracket. Make sure 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  - the attachment bolts are tight.

 

R Inboard Flap - Track 2 Carriage Attachment Bracket - Inspection Area R Figure 619/TASK 57-52-00-991-019
 1EFF : 301-399, 1 57-52-00Page A615 1 1 May 01/04 1 1 1CES 1


R  NOTE : If necessary, refer to the ASRM (Ref. ASRM 575200) for the____ 
R  correct repair procedure. 
R  5. Close-up________ 
R  Subtask 57-52-00-410-072 
R  A. Close Access 
R  (1) Install the flap kink-seals (Ref. TASK 27-54-61-400-006). 
R  (2) Remove the spark-proof lamp from the inspection area. 
R  (3) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (4) Install the applicable flap track fairings (Ref. TASK 57-55-11-400-
R  004): 
R  - for the left wing, install 531AT, 531CB 
R  - for the right wing, install 631AT, 631CB. 
R  Subtask 57-52-00-865-094 
R  B. Remove the safety clip(s) and the tag(s) and close this(these) circuit 
R  breaker(s): 
R  6CV, 8CV. 
R  Subtask 57-52-00-860-060 
R  C. Aircraft Maintenance Configuration 
R  (1) Fully retract the flaps (Ref. TASK 27-50-00-866-009). 
R  Subtask 57-52-00-942-071 
R  D. Removal of Equipment 
R  (1) Remove the safety barriers. 
R  (2) Remove the access platform(s). 
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 57-52-00-210-004 
R  Detailed Visual Inspection of Inboard Double Slotted Flap, Attachment Bracket 
R  of Pylon Aft Fairing, Including Surrounding Skin, 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. 
 
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