C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
39 cotter pin 52-22-04 04 -220 47 cotter pin 52-22-02 01 -070 73 cotter pin 52-22-04 06 -070A 87 cotter pin 52-22-04 06 -070A
1EFF : 301-399, 1 52-22-11Page 414 1 1 May 01/05 1 1 1CES 1 D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004 25-23-47-400-012 25-23-47-400-013 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-Installation of the Door Linings of the LH FWD Emergency Exit Door, zone 231Installation 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.
52-22-00-410-001 52-22-00-710-001 Closing of the Emergency Exit Doors from the Passenger CompartmentOperational Check of Door Locking /Unlocking and Opening/Closing from Inside and Outside with Door Latching/Unlatching and Functional Check of Hand Force
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
52-22-00-820-002 52-22-00-860-003 52-22-00-860-004 52-71-00-820-001 Adjustment of the Emergency Exit DoorSpecial Precaution before Maintenance on the Door Damper and Emergency Operation CylinderSpecial Precaution after Maintenance on the Door Damper and Emergency Operation CylinderAdjustment of the Proximity Switches (11WV1, 11WV2, 15WV1, 15WV2) of the Locking Hook of the Pax/Crew Doors with the CHECKING TOOL-DOOR
52-22-11-991-001 52-22-11-991-002 52-22-11-991-003 52-22-11-991-004 Fig. 401Fig. 402Fig. 403Fig. 404
1EFF : 301-399, 1 52-22-11Page 415 1 1 May 01/04 1 1 1CES 1
3. Job Set-up
__________
Subtask 52-22-11-865-051
A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU COM/CIDS/DEU B/ESS 153RH G03 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 52-22-11-860-051
B. Aircraft Maintenance Configuration
(1)
Make sure that the replacement emergency exit door (referred to as door) is in the subsequent condition:
-
the inboard handle is in the unlocked position,
-
the outboard handle is aligned with the door contour,
-
the slide release lever is in the disarmed position.
(2)
Make sure that the special precautions for the door damper and emergency operation cylinder are completed (Ref. TASK 52-22-00-860-003).
4. Procedure
_________
Subtask 52-22-11-910-050
A. Preparation for the Replacement Components
(1)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Apply COMMON GREASE (Material No. 04-004) to all movable parts
(4)
Attach the SLING - PASSENGER DOOR (98A52108004001) as follows: (Ref. Fig. 401/TASK 52-22-11-991-001)
(a) Attach the sling (5) to the crane, minimum capacity 90 kg (198.4 lb.), and put it in position at the door.
1EFF : 301-399, 1 52-22-11Page 416 1 1 May 01/04 1 1 1CES 1
(b)
If necessary, remove and discard the self-adhesive patches (1) from the plastic plugs (2) of the replacement door.
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM DOORS 艙門3(83)
