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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  A. Fixtures, Tools, Test and Support Equipment 
R  -------------------------------------------------------------------------------
R  REFERENCE  QTY DESIGNATION 
R  -------------------------------------------------------------------------------
R  No specific  low pressure air supply 
R  No specific  safety barriers 
R  No specific  warning notices 
R  No specific  5.0 mm (0.2 in.) dia. non-metallic probe 
R  No specific  9.50 mm (0.375 in.) dia. soft rubber tube 
R  No specific  adjustable 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  57-29-00-991-003  Fig. 601 
R  57-29-00-991-004  Fig. 602


R 3. Job Set-up
__________

R  Subtask 57-29-00-941-052 
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 adjustable access platform position below the applicable 
R  drain-holes in the access panels and the bottom skin of the wing, 
R  zones 521(621) and 522(622). 
R  4. Procedure_________ 
R  (Ref. Fig. 601/TASK 57-29-00-991-003, 602/TASK 57-29-00-991-004) 
R  Subtask 57-29-00-210-052 
R  A. Inspection of the Drain Holes and Hoses 
R  (1) Examine the outer wing drain holes and make sure that they are not 
R  blocked. 
R  (a) If a hole is blocked, remove the applicable access panel. 
R  (b) Remove all unwanted material from around the hole. Use a 5.0 mm 
R  (0.2 in.) dia. non-metallic probe to remove the blockage from the 
R  hole. 
R  (2) Examine the drain hole(s) in the dry bay(s) and make sure that they 
R  are not blocked. 
R  (a) If a hole is blocked, remove all unwanted material from around 
R  the hole. Use a 5.0 mm (0.2 in.) dia. non-metallic probe to 
R  remove the blockage from the hole. 
R  (3) To examine the drain holes of the slat-track cans, do the steps that 
R  follow: 
R  (a) Put the end of a 9.50 mm (0.375 in.) dia. soft rubber tube into 
R  each drain hose.

 

R R  Outer-Wing Drains Figure 601/TASK 57-29-00-991-003
 1EFF : 1 1 1CES  ALL  1 111 57-29-00 Page 603 Nov 01/03

 

R R  Slat-track Cans and Dry Bay Drains Figure 602/TASK 57-29-00-991-004
 1EFF : 1 1 1CES  ALL  1 111 57-29-00 Page 604 Nov 01/03

 

R  (b) Use a low pressure air supply to blow through the tube. 
R  (c) If the hose is not clear, remove all unwanted material. 
R  (4) Find the cause of the blockage. 
R  (5) If you removed an access panel, install it. 
R  5. Close-up________ 
R  Subtask 57-29-00-942-052 
R  A. Removal of Equipment 
R  (1) Remove the warning notice(s). 
R  (2) Remove the safety barriers. 
R  (3) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
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.

 

 WING TIP - DESCRIPTION AND OPERATION
____________________________________
 1. Component Location
__________________
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 wingtip assembly is attached to the outboard end of the wingbox, at
 RIB27.
 The wingtip assembly includes:

 -
the wingtip

 -
the wingtip fence.


 2. Component Description
_____________________
 A. Wingtip
 The structure of the wingtip is made of aluminum alloy. The wingtip
 
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