(a)
Remove the nuts (124), the washers (123) and the bolts (130) from the operation lever (122).
(b)
Disassemble the operation lever (122), the circlip (121) and the washers (120) from the release shaft (117).
(4)
Remove the release lever (105) from the release shaft (117) as follows:
(a)
Remove the nut (106), the washers (104) and the bolt (103) from the release lever (105).
(b)
Disassemble the release lever (105) and the washers (107) from the release shaft (117).
(5)
Remove the release shaft (117) from the structure as follows:
(a)
Remove the nut (111), the washers (110) and the bolt (113) from the lever (112).
(b)
Hold the lever (112) and remove the release shaft (117) from the structure.
(6)
Remove the bearing brackets (108) and (118) from the structure as follows:
(a)
Remove the bearings (109) and (119) from the bearing brackets
(108) and (109).
(b)
Remove the nuts (114) and (133), the washers (115) and (134) and the bolts (116) and (135) from the bearing brackets (108) and (118).
(c)
Remove the bearing brackets (108) and (118) from the structure.
1EFF : 301-399, 1 52-22-22Page 432 1 1 May 01/04 1 1 1CES 1
TASK 52-22-22-400-004 Installation of the Release Shaft Assembly
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 3.2 m (10 ft. 6 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
131 cotter pin 52-22-22 05 -110
1EFF : 301-399, 1 52-22-22Page 433 1 1 May 01/04 1 1 1CES 1
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-23-47-000-012 Removal of the Door Linings of the LH FWD Emergency Exit Door, zone 231
25-23-47-000-013 Removal of the Door Linings of the RH FWD Emergency Exit Door at zone 251 or RH AFT at zone 252 or LH AFT at zone 232.
25-23-47-400-012 Installation of the Door Linings of the LH FWD Emergency Exit Door, zone 231
25-23-47-400-013 Installation of the Door Linings of the RH FWD Emergency Exit Door at zone 251, or RH AFT at zone 252, or LH AFT at zone 232.
52-22-00-010-001 Opening of the Emergency Exit Doors from the Passenger Compartment 52-22-00-410-001 Closing of the Emergency Exit Doors from the Passenger Compartment
52-22-00-720-001 Check of Door Unlocking from Inside/Outside in Armed Position and of Slide Release Mechanism Arming/Disarming, Functional Check ofSlide Cable Movement
52-22-00-860-003 Special Precaution before Maintenance on the Door Damper and Emergency Operation Cylinder 52-22-00-860-004 Special Precaution after Maintenance on the Door Damper and Emergency Operation Cylinder
3. Job Set-up
__________
Subtask 52-22-22-865-060
A. 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
1EFF : 301-399, 1 52-22-22Page 434 1 1 May 01/04 1 1 1CES 1 Subtask 52-22-22-860-053
B. Aircraft Maintenance Configuration
(1)
Make sure that the applicable emergency exit door (referred to as door) is opened as required (Ref. TASK 52-22-00-010-001).
(2)
Make sure that the access platform is in position below the partly opened door.
(3) 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3(143)
