• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-26 23:38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

 (b) Push the door aft wards and into the door frame.
 (3) Fully lower the outer control handle (1), (the door moves down).
 (a) Make sure that : - the door is fully closed and flush with the fuselage, - the outer control handle (1) is in the correct position in its housing and flush with the door. - the flap (3) is flush with the door.
 (4) Closing of the passenger/crew door from the inside. (Ref. Fig. 202/TASK 52-10-00-991-043) 
R R  (a) With one hand, hold the assist handle (16), on the door frame, to have a safe position in front of the open door. 
R R R  (b) With the other hand, push the pushbutton (11) of the door stay mechanism and at the same time pull the support arm (15) to release the door from the fuselage. 
R R  (c) Use the assist handle (14) on the door to pull the door into the door frame.
 (d) Fully lower the inner control handle (12) (the door moves down).

 1EFF : ALL 1 52-10-00Page 207 1 1 May 01/02 1 1 1CES 1


R (e) Make sure that the door is fully closed and the indicator plate

 (13) shows LOCKED.
 ________

5. Close-up
 Subtask 52-10-00-862-051
 A. De-energize the ground service network
 (Ref. TASK 24-42-00-862-001)

 Subtask 52-10-00-942-050
 B. Close Access
 (1)
 Remove the access platform(s).

 (2)
 Make sure that the work area is clean and clear of tool(s) and other items.


 1EFF : ALL 1 52-10-00Page 208 1 1 Feb 01/02 1 1 1CES 1


 TASK 52-10-00-860-001 Special Precautions before Work on the Passenger/Crew Door
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) 701-2978000 1 PIN - RIGGING 98D52103500000 1 SAFETY PIN - SLIDE ARMING
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External
 Power 52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-991-002 Fig. 203 52-10-00-991-003 Fig. 204
 3. Job Set-up
__________ Subtask 52-10-00-861-050
 A. Aircraft Maintenance Configuration
 (1) Energize the ground service network
 (Ref. TASK 24-42-00-861-001)

 Subtask 52-10-00-010-074
 B. Get Access
 (1) Open the applicable passenger/crew door (Ref. TASK 52-10-00-010-001).
 1EFF : ALL 1 52-10-00Page 209 1 1 Feb 01/02R 1 1 1CES 1


 Subtask 52-10-00-865-065
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU EIS/SLIDES/ARM AND WARN/FLT 15WN P11 121VU EIS/SLIDES/ARM AND WARN/GND 13WN P10 121VU EIS/SDAC1 AND 2/DOOR/DET/PAX 48WV P05
 4. Procedure
_________
 Subtask 52-10-00-481-052
 A. Special Precautions
 (1)
 Make sure that the emergency control handle is in the DISARMED position and that the SAFETY PIN - SLIDE ARMING (98D52103500000) (1) is in position. (Ref. Fig. 203/TASK 52-10-00-991-002)

 (2)
 Disarm the percussion mechanism of the door damper and emergency operation cylinder. (Ref. Fig. 204/TASK 52-10-00-991-003)

 (a)
 Open the applicable passenger/crew door (Ref. TASK 52-10-00-010-001).

 (b)
 Install the PIN - RIGGING (701-2978000) (2).

 (c)
 Remove and discard the lockwire from the knurled screw (1).

 (d)
 Loosen the knurled screw (1).

 (e)
 Push the striker lever aft to disarm it.

 (f)
 Tighten the knurled screw (1).

 


R 5. Close-up
________
R Subtask 52-10-00-865-091
R A. Remove the safety clip(s) and the tag(s) and close this(these) circuit R breaker(s):
R -------------------------------------------------------------------------------R PANEL DESIGNATION IDENT. LOCATION R -------------------------------------------------------------------------------R 121VU EIS/SLIDES/ARM AND WARN/FLT 15WN P11 R 121VU EIS/SLIDES/ARM AND WARN/GND 13WN P10 R 121VU EIS/SDAC1 AND 2/DOOR/DET/PAX 48WV P05
 
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 DOORS 舱门1(70)