3. Job Set-up
__________ Subtask 52-13-14-860-057
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position.
(2)
Make sure that the aft passenger/crew door is open (Ref. TASK 52-10-00-010-001).
(3)
Make sure that the special precautions are obeyed (Ref. TASK 52-10-00-860-001).
Subtask 52-13-14-865-071
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------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
Subtask 52-13-14-220-055
C. Preparation for Installation
(1)
Clean the component interface and/or the adjacent area.
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition. (Ref. TASK 52-13-14-220-001)
4. Procedure
_________ Subtask 52-13-14-420-060
A. Installation of the Telescopic Rod
(Ref. Fig. 402/TASK 52-13-14-991-008)
(1) Install the spacer (9), the washer (8), the bolt (7), the washer (13) and the nut (14).
1EFF : ALL 1 52-13-14Page 416 1 1 Nov 01/00R 1 1 1CES 1
(2)
TORQUE the nut (14) to between 0.35 and 0.7 m.daN (30.97 and 61.94 lbf.in).
(3)
Install the cotter pin (15).
(4)
Install the bushes (16) and (17) on the fork (6).
(5)
Install the washer (11), the bushes (4), the end of the door damper and emergency-operation cylinder (5), the washer (15), the fork (6), the bolt (10) and the nut (2).
(6)
TORQUE the nut (2) to between 1 and 1.7 m.daN (88.49 and 150.44 lbf.in).
(7)
Install the cotter pin (1).
5. Close-up
________ Subtask 52-13-14-410-072
A. Installation of the Door Support-Arm Lining
(1) Install the door support-arm lining (Ref. TASK 25-23-46-400-002).
(a) For the left passenger/crew door: 832FZ, 832GZ.
(b) For the right passenger/crew door: 842FZ, 842GZ. Subtask 52-13-14-865-072
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 13WN, 15WN, 48WV
Subtask 52-13-14-410-073
C. Close Access
(1)
Obey the special precautions after you do work on the door (Ref. TASK 52-10-00-860-002).
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
(3)
Close the passenger/crew door (Ref. TASK 52-10-00-410-001), 832, 842.
(4)
Remove the access platform(s).
1EFF : ALL 1 52-13-14Page 417 1 1 Nov 01/00R 1 1 1CES 1
R R Door-Damper and Emergency-Operation Cylinder Figure 403/TASK 52-13-14-991-001
1EFF : 1 1 1CES ALL 1 111 52-13-14 Page 418 Feb 01/05
CYLINDER - DOOR DAMPER AND EMERGENCY OPERATION - ADJUSTMENT/TEST
________________________________________________________________
TASK 52-13-14-820-002
Adjustment of the Percussion Bellcrank Finger of the Door Damper and Emergency Operation Cylinder of the AFT 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) No specific access platform 3.50 m (11 ft. 6 in.) 98D52103500000 1 SAFETY PIN - SLIDE ARMING
B. Referenced Information
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門2(101)
