A320飞机维护手册 AMM WINGS 机翼5(41)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

R  new lockwasher (10). 
R  (e) Loosely install the lockwasher (10) and the locknut (9). 
R  (f) Put the locking device (12) in position on the spherical bearing 
R  (11). If necessary, adjust the position of the spherical bearing 
R  (4) so that the locking device (12) engages correctly. 
R  (g) Install the new tab-washer (14) on the screw (13). 
R  (h) Apply SPECIAL MATERIALS (Material No. 05-002) to the threads of 
R  the screw (13). 
R  (i) Install the screw (13). 
R  (j) TORQUE the screw (13) to between 1.6 and 1.8 m.daN (11.79 and 
R  13.27 lbf.ft). 
R  (k) Use the WRENCH - BEARING, FLAP TO CARRIAGE TRACK 2 
R  (98D27507541000) to torque the locknut (9) to between 8.0 and 
R  10.0 m.daN (58.99 and 73.74 lbf.ft). 
R  (l) Safety the locknut (9) with the lockwasher (10).

 

R R  (m) Do a no-load Breakaway Torque of the spherical bearing (11) to 0.75 m.daN (66.37 lbf.in) maximum. 
R R  (n) Apply a bead of SEALANTS (Material No. 09-002) around the lock nut (9). 
R R  (o) Apply STRUCTURE PAINTS (Material No. 16-003) to the bead seal around the locknut (9). 
R R  (p) Apply red STRUCTURE PAINTS (Material No. 16-016), as shown, to the spherical bearing (11). 
R  Subtask 57-53-21-410-050-A 
R  C. Close Access 
R R  (1) Make sure that the work area is clean and clear of tool(s) and other items. 
R  (2) Install the outboard flap (Ref. TASK 27-54-62-400-002). 
R  **ON A/C ALL
 Subtask 57-53-21-865-052
 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
 Subtask 57-53-21-710-050
 E. Operational Test
 (1) Do an operational test of the flap system (Ref. TASK 27-54-00-710-001).
 5. Close-up________
 Subtask 57-53-21-942-050
 A. Removal of Equipment
 (1) Remove the safety barriers.
 (2) Remove the warning notice(s).

 

 (3)
 Remove the access platform(s).

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 

 FAIRINGS - 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,
R  (Ref. Fig. 001A) **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 002) **ON A/C 301-399,
R  (Ref. Fig. 002A) **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Fairings are installed on the outer wing to seal: - the flap track drive mechanisms - the engine pylon and its systems. **ON A/C 301-399,
 Fairings are installed on the outer wing to seal: - the flap track drive mechanisms - the flap tab hinges - the engine pylon and its systems.

 

 Fairings Figure 001 
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1201-299, 401-499, 1 1CES  1 111 57-55-00 Page 2 Aug 01/05

 

R  Flap Track Fairings - Tracks 2, 3 and 4 
R  Figure 001A 
R 1EFF :  301-399,  1  57-55-00 Page 3 
1  1  May 01/04
 1  1
 1CES  1

 

 Fairings Figure 002 
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1201-299, 401-499, 1 1CES  1 111 57-55-00 Page 4 Aug 01/05

 

R  Movable Fairings - Tracks 2, 3 and 4 
R  Figure 002A
 1EFF :  301-399,  1  57-55-00 Page 5 
1  1  May 01/04
 1  1
 1CES  1

 

 **ON A/C ALL
 2. Component Description
_____________________
 A. Forward Fixed Fairings
 The forward fixed fairings are made of a thermo-plastic. A silicon rubber seal is riveted to the top edge, and touches the outer wing bottom skin. A steel slider-spigot near the forward end, attaches to the bottom skin.
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
 B. Flap Track Fairings
 The flap track fairings 2, 3 and 4 are attached to fittings (Ref. 57-26-00) on the bottom surface of the wing.
 The flap track fairings are:
 -
the fixed fairing

 -
the movable fairing.

 A steel swivel link near the forward end of the fixed fairing attaches the fairing to the wing bottom skin.
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM WINGS 机翼5(41)