• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 13:53来源:蓝天飞行翻译 作者:admin
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

 


 4. Procedure
_________
 (Ref. Fig. 402/TASK 27-41-42-991-001) Subtask 27-41-42-420-050
 A. Installation of the Cable Tension Regulator
 (1) Install the regulator (8) as follows:
 (a) Put the regulator (8) together with the shims (12) in position at the structure interface.
 NOTE : Make sure that the shims (12) are installed at the
____ positions identified during the removal.
 (b)
 Make sure that the cables (22) are correctly installed in the pulley (21).

 (c)
 Install the bolts (11), the washers (13) and the nuts (14) to attach the regulator (8) to on structure.


 (2) Install the rocker assembly (15) in the regulator (8).
 (a) Put the rocker assembly (15) in position on the cables (22) near to the regulator (8).
 NOTE : Make sure that the cables (22) are correctly installed in
____ the grooves of the pulleys (21).
 (b)
 Put the spacers (23) in position and install the screw (25) and the bolt (24).

 (c)
 Install the washers (26) and the nuts (27).

 (d)
 TORQUE the nuts (27) to 0.1 m.daN (8.84 lbf.in) and safety them with the cotter pins (28).


 1EFF : ALL 1 27-41-42Page 414 1 1 May 01/04R 1 1 1CES 1


 (e)
 Put the bolt (20) through the regulator (8), the bushes (19) and the rocker assembly (15).

 (f)
 Install the washer (18) and the nut (17) on the bolt (20).

 (g)
 TORQUE the nut (17) to 0.8 m.daN (70.79 lbf.in) and safety it with the cotter pin (16).


 (3)
 Connect the springs (10) to the bolts (9).

 (4)
 Adjust the turnbuckles (31) until you can easily install the RIGGING PIN - THS MECHANICAL CONTROL (98D27407532000) through the rocker assembly (15) of the regulator.

 

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 401/TASK 27-41-42-991-002)
 **ON A/C 301-399,

 (Ref. Fig. 401A/TASK 27-41-42-991-002-A)
 **ON A/C ALL

 (5) Install the cover (2) on the regulator (8).
 (a)
 Put the cover (2) in position on the regulator (8).

 (b)
 Install the bolts (5) and the washers (6) at the connection of the cover (2) and the cover assembly (1).

 (c)
 Install the bolts (3) and the washers (4) at the connection of the cover (2) and the regulator (8).


 Subtask 27-41-42-080-050
 B. Removal of the Rigging Pins
 (1)
 Remove the rigging pin OU190360 from the mechanical input of the THS actuator.

 (2)
 Remove the rigging pin 98D27407532000 from the regulator.

 (3)
 Remove the PITCH TRIM CONTROL LOCKING (98D27403500000) from the pitch trim control wheel.

 


 Subtask 27-41-42-865-051
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 15CE1, 16CE1, 19CE1, 19CE2, 19CE3
 Subtask 27-41-42-220-051
 D. Check Procedure
 (1)
 Do a check of the cable tensions (Ref. TASK 27-41-00-220-002).

 (2)
 Make sure that the locking clips (30) are correctly installed in the turnbuckles (31).

 

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 401/TASK 27-41-42-991-002)
 **ON A/C 301-399,

 (Ref. Fig. 401A/TASK 27-41-42-991-002-A)
 **ON A/C ALL

 5. Close-up
________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 27-41-42-410-050
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the access panel 311AL and close the access door 312AR.

 (3)
 Remove the access platform(s).

 


 (4) Install the floor panels 241FF, 241BF (Ref. TASK 53-32-12-400-002).
 (5) Remove the warning notice(s). 
R  **ON A/C 301-399, 
R  Subtask 27-41-42-410-050-A 
R  A. Close Access 
R  (1) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (2) Install the access panel 311AL and close the access door 312AR. 
R  (3) Remove the access platform(s). 
R  (4) Install the floor panels 231BG, 231JG (Ref. TASK 53-22-12-400-001). 
R  (5) Remove the warning notice(s).

 

R **ON A/C ALL


 TASK 27-41-42-000-002
 Removal of the Springs of the Cable Tension Regulator
 
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 FLIGHT CONTROLS 飞行操纵3(110)