• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-22 06:40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


 TASK 27-92-41-000-003 Removal of the Dampers WARNING : MAKE SURE THAT THE SIDE STICK ASSEMBLY STAYS IN THE VERTICAL POSITION
_______ DURING THE MAINTENANCE PROCEDURES. IF NOT THERE IS A RISK OF SKYDROL LEAKAGE. SKYDROL CAN CAUSE INJURY AND/OR DAMAGE.
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific string 98D27303001001 1 HOLDER - SIDE STICK
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-92-41-000-001 Removal of the Side Stick Assembly 19VU (18VU) 27-92-41-991-004-A Fig. 405
 3. Job Set-up
__________ Subtask 27-92-41-010-052
 A. Remove the side stick assembly (Ref. TASK 27-92-41-000-001). Subtask 27-92-41-480-053
 B. Install the side stick assembly on the HOLDER - SIDE STICK
 (98D27303001001).

 1EFF : ALL 1 27-92-41Page 423 1 1 May 01/03R 1 1 1CES 1


 4. Procedure
_________
 (Ref. Fig. 405/TASK 27-92-41-991-004-A) Subtask 27-92-41-020-052
 A. Removal of the Side Stick Damper
 (1)
 Cut and discard the cotter pins (50) from the nuts (51).

 (2)
 Remove the nuts (51) and the washers (52).

 (3)
 Remove the bolts (54), the damper (53) and (55) and hold it in the vertical position

 (4)
 Fully compress the damper (53) and (55) and hold it in this position with a string


 1EFF : ALL 1 27-92-41Page 424 1 1 May 01/03R 1 1 1CES 1


 Dampers Figure 405/TASK 27-92-41-991-004-A
 1EFF : 1 1R 1CES  ALL  1 11 1 27-92-41 Page 425 May 01/03

 

 TASK 27-92-41-400-003 Installation of the Dampers WARNING : MAKE SURE THAT THE SIDE STICK ASSEMBLY STAYS IN THE VERTICAL POSITION
_______ DURING THE MAINTENANCE PROCEDURES. IF NOT THERE IS A RISK OF SKYDROL LEAKAGE. SKYDROL CAN CAUSE INJURY AND/OR DAMAGE.
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 1.6 m (5 ft. 3 in.)
 B. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
cotter pins 27-92-41 01D-080
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External
 Power 27-92-41-000-001 Removal of the Side Stick Assembly 19VU (18VU) 27-92-41-400-001 Installation of the Side Stick Assembly 19VU (18VU) 27-92-41-991-004-A Fig. 405
 1EFF : ALL 1 27-92-41Page 426 1 1 May 01/03R 1 1 1CES 1


 3. Job Set-up
__________ Subtask 27-92-41-860-057
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).

 (2)
 Make sure that the access platform is in position at the access door

 822.

 (3)
 Make sure that the access door 822 is open.

 (4)
 On the battery power center 105VU:

 -make sure that the protective cover is removed.

 (5)
 Make sure that the side stick assembly is installed on the HOLDER -SIDE STICK (98D27303001001) (Ref. TASK 27-92-41-000-001).


 4. Procedure
_________ (Ref. Fig. 405/TASK 27-92-41-991-004-A) Subtask 27-92-41-420-052
 A. Installation of the Side Stick Damper
 (1)
 Remove the string from the damper (55).

 (2)
 Clean the component interface and/or the adjacent area.

 (3)
 Do an inspection of the component interface and/or the adjacent area.

 (4)
 Install the damper (55) on the side stick assembly and the bolts (54).
 
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9(46)