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时间:2011-03-27 12:40来源:蓝天飞行翻译 作者:航空
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R  - COMPONENTS THAT MOVE. 
R  1. Reason for the Job__________________ 
R  Refer to the MPD TASK: 573900-01 
R  2. Job Set-up Information______________________ 
R  A. Fixtures, Tools, Test and Support Equipment 
R  -------------------------------------------------------------------------------
R  REFERENCE  QTY DESIGNATION 
R  -------------------------------------------------------------------------------
R  No specific  plastic probe 
R  No specific  safety barriers 
R  No specific  warning notices 
R  No specific  access platform 4.0 m (13 ft. 1 in.) 
R  98D27803500001  1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER 
R  B. Referenced Information 
R  -------------------------------------------------------------------------------
R  REFERENCE  DESIGNATION 
R  -------------------------------------------------------------------------------
R  57-39-00-991-002  Fig. 601

 

R  3. Job Set-up__________ 
R  Subtask 57-39-00-941-051 
R  A. Safety Precautions 
R  (1) Put the safety barriers in position. 
R  (2) Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) 
R  on the flap/slat control lever. 
R  (3) Put warning notices in the cockpit to tell persons not to operate the 
R  flaps or slats. 
R  (4) Put the access platformin position below the applicable wing-tip, 
R  zone 534(634). 
R  4. Procedure_________ 
R  (Ref. Fig. 601/TASK 57-39-00-991-002) 
R  Subtask 57-39-00-210-051 
R  A. Inspection 
R  (1) Examine the drain holes in: 
R  - the opposite corners of the access panel 534AB(634AB) 
R  - the bottom of the wing-tip fence 
R  - the lower surface of the wing adjacent to the wing-tip glazing 
R  panel. 
R  (2) Make sure that they are not blocked. 
R  (3) If a hole in the access panel is blocked, remove the access panel. 
R  (4) For all the holes, remove all unwanted material from around the 
R  holes. Use a plastic probe to remove the blockage from the holes. 
R  (5) If you removed the access panel, install it when the blockage is 
R  clear.

 

R R  Wing-Tip Drains Figure 601/TASK 57-39-00-991-002
 1EFF : 1 1 1CES  ALL  1 111 57-39-00 Page 603 Nov 01/03


R 5. Close-up
________

R  Subtask 57-39-00-942-051 
R  A. Removal of Equipment 
R  (1) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (2) Remove the warning notice(s). 
R  (3) Remove the safety barriers. 
R  (4) Remove the access platform(s). 
R  (5) Remove the ground support and maintenance equipment, the special and 
R  standard tools and all other items.

 

 LEADING EDGE AND LEADING EDGE DEVICES - DESCRIPTION AND OPERATION
_________________________________________________________________
 1. General
_______

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 001)
 **ON A/C 301-399,
 (Ref. Fig. 001A)
 **ON A/C ALL
 The leading edge is forward of the front spar of the wing box, between the wing root and the wing tip. The leading edge has a fixed structure and five devices which are movable control surfaces.
 2. Component Location
__________________
 The fixed structure (Ref. 57-41-00) is between RIB1 and RIB27.

 The five movable devices are:
 -Slat 1, inboard of the engine pylon (Ref. 57-42-00)
 -Slats 2 thru 5, outboard of the engine pylon (Ref. 57-43-00), (Ref. 57-44-00), (Ref. 57-45-00) and (Ref. 57-46-00).
 3. Description
___________
 A. Leading edge
 The leading edge is a fixed structure of ribs and riblets to which nose skins are attached. The structure is strengthened by sub-spars. The five slats are connected, through the slat tracks, to the fixed structure.
 These systems are also installed in the leading edge:
 -
the drive mechanism for the slats (Ref. 27-84-00)

 -
the ducting for the engine bleed air (Ref. 36-11-00)


 -electrical, hydraulic and pneumatic installations
 -
the environment protection system, between the wing root and RIB12 (Ref. 36-14-00)
 
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