• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-26 09:15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

R 122VU AIR BLEED/X FEED VALVE/NORM 1HV Z20
 Subtask 36-12-11-860-050
 B. Aircraft Maintenance Configuration
 (1)
 Put the warning notice in position:

 -in the cockpit on the AIR COND Overhead Control Panel 30VU to tell persons not to push in the APU BLEED pushbutton switch.

 (2)
 Put the access platform(s) 2.1 m (6.88 ft.) or 3.6 m (11.81 ft.) in position at the AFT cargo-compartment door or the access door 312AR.


 Subtask 36-12-11-010-050
 C. Get Access
 (1)
 Open the AFT cargo-compartment door (Ref. TASK 52-30-00-860-001) or the access door 312AR.

 (2)
 In the AFT cargo compartment remove the partition panel 161DW.


 4. Procedure
_________
 (Ref. Fig. 401/TASK 36-12-11-991-001)
 Subtask 36-12-11-020-050

 A. Removal of the Spring Rods
 NOTE : The removal procedure for all spring rods is the same.

____
 (1)
 Remove and discard the cotter pin (4).

 (2)
 Remove and retain the castle nut (3) and the washer (2).

 (3)
 Hold the spring rod (5),(7) and (8) and remove the bolt (1) from the


 structure bracket and the bolt (6) from the duct bracket.

 (4)
 Retain the bolts (1) and (6).

 (5)
 Remove the spring rod (5),(7) and (8).

 


 Spring Rods (FR65, FR68, FR72 and FR74)
 Figure 401/TASK 36-12-11-991-001
 1EFF :  ALL  1  36-12-11 Page 403 
1  1  Feb 01/98
 1  1
 1CES  1

 


 TASK 36-12-11-400-001


 Installation of the Spring Rods (FR65, FR68, FR72 and FR74)
 WARNING : MAKE SURE THAT THE PNEUMATIC SYSTEM IS DEPRESSURIZED BEFORE YOU START

_______
 WORK ON THE PNEUMATIC SYSTEM.

 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(s) 2.1 m (6.88 ft.) or 3.6 m (11.81 ft.) No specific warning notice R
R B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-30-00-860-002  Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 36-12-11-991-001 Fig. 401
 3. Job Set-up
__________
 Subtask 36-12-11-860-051

 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the warning notice is in position:

 -in the cockpit on the AIR COND Overhead Control Panel 30VU to tell persons not to push in the APU BLEED pushbutton switch.

 (2)
 Make sure that the access platform(s) 2.1 m (6.88 ft.) or 3.6 m


 (11.81 ft.) is in position at the AFT cargo-compartment door or the access door 312AR.


 Subtask 36-12-11-865-051

 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AIR BLEED/X FEED/VALVE/BAT 2HV D13 121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41 122VU AIR BLEED/X FEED VALVE/NORM 1HV Z20
 Subtask 36-12-11-210-050
 C. Inspection of the Spring Rod
 (1)
 Make sure that the spring rod is not damaged and does not have corrosion.

 (2)
 Make sure that the piston part of the spring rod moves freely in the cylinder part.

 (3)
 Make sure that you can see the threaded end of the spring rod through the inspection hole.


 4. Procedure
_________ (Ref. Fig. 401/TASK 36-12-11-991-001) Subtask 36-12-11-420-050
 A. Installation of the Spring Rods
 NOTE : The installation procedure for all spring rods is the same.

____
 (1)
 Correctly install the spring rod (5),(7) and (8) between the structure and the duct bracket.

 (2)
 Install the bolt (1) to the structure bracket and the bolt (6) to the duct bracket.

 (3)
 Install the retained washer (2) and the castle nut (3).

 (4)
 Safety the castle nut (3) with the cotter pin (4).
 
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 PNEUMATIC 气源 2(74)