(f)
Put the first clamp (25) to the mark at the wire harness (18).
(g)
Attach the clamps (25) with the bolts (27), the washers (26), the spacers (28) and the nuts (30) on the fuselage frame (29).
(h)
Connect the connector (24) of the wire harness (18) to the receptacle (23) at the fuselage frame (refer to the subsequent table):
----------------------------------------------------------| DOOR | CONNECTOR | RECEPTACLE | FRAME | CABLE LOOM | __________________________________________________________
| FWD LH | 2821VC-A | 2821VC | FR35 | 4251VB |
| FWD RH | 2820VC-A | 2820VC | FR35 | 4250VB |
| AFT LH | 6721VC-A | 6721VC | FR47.2| 4253VB |
| AFT RH | 6720VC-A | 6720VC | FR47.2| 4252VB |
----------------------------------------------------------Subtask 52-22-11-820-052
G. Adjustment Procedure
(1)
Adjust the door to the correct position in the fuselage (Ref. TASK 52-22-00-820-002).
(2)
Make sure that the proximity sensors 19WV, 21WV and 61WV are correctly adjusted (Ref. TASK 52-71-00-820-001).
Subtask 52-22-11-720-050
H. Test Procedure
(1)
Do a opertional test (Ref. TASK 52-22-00-710-001) to make sure that the locking mechanism is correctly adjusted.
(2)
Do a functional test (Ref. TASK 52-22-00-720-001) to make sure that the slide release mechanism is correctly adjusted.
1EFF : 301-399, 1 52-22-11Page 422 1 1 May 01/04 1 1 1CES 1
5. Close-up
________ Subtask 52-22-11-410-050
A. Close Access
(1)
Install the insulation mat on the inner side of the door and attach it with the VELCRO tapes.
(2)
Install the the door Lining (Ref. TASK 25-23-47-400-012) and (Ref. TASK 25-23-47-400-013) on the replacement door.
Subtask 52-22-11-865-052
B. Make sure that this(these) circuit breaker(s) is(are) closed:
13WN, 15WN, 48WV, 153RH
Subtask 52-22-11-410-051
C. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Do the special precaution for the door damper and emergency operation cylinder (Ref. TASK 52-22-00-860-004).
(3)
Close applicable the door (Ref. TASK 52-22-00-410-001).
(4)
Remove the access platform(s).
1EFF : 301-399, 1 52-22-11Page 423 1 1 May 01/04 1 1 1CES 1 DOOR - EMERGENCY EXIT - INSPECTION/CHECK
________________________________________
TASK 52-22-11-200-001
Detailed Visual Inspection of the Internal Structure of the Forward Emergency Exit Doors
1. Reason for the Job
__________________
Refer to the MPD TASK: 522202-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific lint-free cloth No specific masking paper No specific masking tape No specific wooden or plastic scraper
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-002 USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00)
Material No. 15-005 AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
Material No. 15-006 AIB TN 10138 TYPE I GRADE 3 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
1EFF : 301-399, 1 52-22-11Page 601 1 1 May 01/04 1 1 1CES 1
C. 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.
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(86)