• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 13:47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

 (i) Put the bolt (15) through the connection of the forked lever (17) and the eye-end (18). Do not install the washer (28) and the nut (29) at this time.
 (j) Safety the eye-end (18) with the securing plate (20).
 (k) Fully tighten the screws (22). 
R R  (l) Apply the SPECIAL MATERIALS (Material No. 05-005D) at the heads of the screws (22). 
R R  (3) Connect the forked lever (17) of the artificial feel unit (4) to the solenoid 16CA (3) as follows:
 (a) Install the washer (28) and the nut (29) on the bolt (15).
 (b) Safety the nut (29) with a new cotter pin (30). 
R R R  (c) Apply a thin layer of the SPECIAL MATERIALS (Material No. 05-002) to the interface of the artificial feel unit (4) at the shaft (31). 
R  (4) Install the cover (6) on the artificial feel unit (4) as follows: 
R R  (a) Put the cover (6) over the shaft (31) in its correct position it on the artificial feel unit (4).
 (b) Install the screws (7) and the washers (8) in the cover (6). 
R R  (c) Apply the SPECIAL MATERIALS (Material No. 05-005D) to the heads of the screws (7).

 

R R  (5) Connect the lever arm (11) to the artificial feel unit (4) as follows:
 (a) Install the bush (10) in the lever arm (11). 
R R  (b) Move the artificial feel unit (4) at the universal joint (5). Put the shaft (31) in position at the lever arm (11). 
R  (c) Support the artificial feel unit (4).
 (d) Align the bolt hole in the lever arm (11) with the bolt hole in the shaft (31).
 (e) Install the bolt (9), the washer (12) and the nut (13).
 (f) TORQUE the nut (13) to 0.8 m.daN (70.79 lbf.in).
 (g) Safety the nut (13) with a new cotter pin (14).
R  (6) Remove the blanking caps and connect the electrical connector (26) to the receptacle (25) of the solenoid 16CA (3). 
R R  (7) Make sure that the cable of the electrical connector (26) does not rub on the spar box of the vertical stabilizer (1).
 Subtask 27-23-17-080-050
 D. Removal of the Rigging Pins (Ref. Fig. 401/TASK 27-23-17-991-002)
 (1) Remove the PIN - RIGGING (98D27207547000) (51) from the rudder cable quadrant.
 (2) Remove the PIN - RIGGING (98D27207548000) (50) from the bellcrank of the rudder control unit.
 Subtask 27-23-17-865-051
 E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CC1, 5CC2, 14CC1, 14CC2, 15CC

 

 Subtask 27-23-17-860-053
 F. Preparation for the Test
 (1)
 On the overhead panel 23VU, push the FLT CTL/FAC 1 pushbutton switch and the OFF legend goes off.

 (2)
 On the overhead panel 24VU, push the FLT CTL/FAC 2 pushbutton switch and the OFF legend goes off.


 Subtask 27-23-17-710-050
 G. Do an operational test of the artificial feel loads of the rudder
 (Ref. TASK 27-23-00-710-001).

 5. Close-up
________ Subtask 27-23-17-410-050-A
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the access panel 325BL at the trailing edge of the vertical stabilizer (Ref. TASK 55-33-13-410-002).

 (3)
 Install the rudder fairing 325AL (Ref. TASK 53-55-12-400-001).

 (4)
 Close the access door 312AR.

 (5)
 Remove the warning notice(s).

 (6)
 Remove the access platform(s).

 


 ARTIFICIAL FEEL AND TRIM UNIT - REMOVAL/INSTALLATION
____________________________________________________
 TASK 27-23-41-000-001
 Removal of the Artificial Feel and Trim Unit
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
 START A TASK ON OR NEAR:

 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS


 -COMPONENTS THAT MOVE.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific blanking caps
 No specific circuit breaker(s) safety clip(s)
 No specific warning notices
 No specific access platform 11.0 m (36 ft. 1 in.)
 6137-013 1 PIN - LOCKING
 98D27207547000 1 PIN - RIGGING
 
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2(105)