(4)
Disassemble the roller (90) as follows:
(a)
Remove the cotter pin (93) and discard it.
(b)
Loosen the nut (94) and remove it.
1EFF : ALL 1 52-13-31Page 419 1 1 Feb 01/04R 1 1 1CES 1
Door Stop Fittings Figure 406/TASK 52-13-31-991-008
1EFF : 1 1R 1CES ALL 1 11 1 52-13-31 Page 420 May 01/98
Roller Fitting Figure 407/TASK 52-13-31-991-009
1EFF : 1 1R 1CES ALL 1 11 1 52-13-31 Page 421 Feb 01/04
(c)
Remove the washer (95).
(d)
Remove the bolt (96), the roller assembly (97), the spacer (98) and the fitting (90).
Subtask 52-13-31-020-059
G. Removal of the Fittings of the Guide Arms
(Ref. Fig. 408/TASK 52-13-31-991-010)
(1)
Disengage the guide arms (100) and (101) (Ref. TASK 52-11-12-000-003).
(2)
Loosen the nuts (102) and remove them.
(3)
Remove the bolts (106) and the washers (103).
(4)
Remove the fitting pivots (105) and (108).
(5)
Remove the serrated plates (107) (104).
1EFF : ALL 1 52-13-31Page 422 1 1 Feb 01/04R 1 1 1CES 1
Fittings of the Guide Arms Figure 408/TASK 52-13-31-991-010
1EFF : 1 1R 1CES ALL 1 11 1 52-13-31 Page 423 May 01/98
TASK 52-13-31-400-002
Installation of the Stop Fittings, the Buffer, the Guide Fittings, the Rollers, the Door Stop Fittings, the Roller Fittings and the Guide Arm Fittings
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 3.5 m (11 ft. 6 in.) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-047 C Z-11.904
ANTI COR. COMPOUND(HIGH TEMP.SILICONE SEALANT)
(Ref. 20-31-00)
Material No. 09-005 USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00)
Material No. 11-004 USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
1EFF : ALL 1 52-13-31Page 424 1 1 May 01/05 1 1 1CES 1 C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
71 cotter pin 53-46-04 82A-100 83 lock plate 52-13-11 21 -040 83 lock plate 52-13-11 21A-040 93 cotter pin 52-13-11 21 -100 93 cotter pin 52-13-11 21A-100
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-23-45-400-005 Installation of the Door Frame Linings at the Right
AFT Passenger/Crew Door
25-23-45-400-008 Installation of the Door Frame Linings at the Left
AFT Passenger/Crew Door
25-23-46-400-002 Installation of the Door Linings at the AFT Passenger/Crew Doors R 25-62-44-400-001 Installation of the Escape-Slide Pack-Assembly 52-10-00-080-001 Removal of the Passenger/Crew Door Ballast Weight (98D52103501000) for Escape Slide 52-10-00-080-001 Removal of the Passenger/Crew Door Ballast Weight
(98D52103501000) for Escape Slide/Raft 52-10-00-410-001 Closing of the Passenger/Crew Door 52-10-00-860-001 Special Precautions before Work on the Passenger/Crew
Door 52-10-00-860-002 Special Precautions after Work on the Passenger/Crew
Door
52-11-00-820-001 Adjustment of the FWD Passenger/Crew Door
52-11-12-400-003 Installation of the Guide Arms
52-13-31-220-001 Detailed Visual Inspection of the Rollers
52-13-31-991-002 Fig. 402
52-13-31-991-005 Fig. 403
52-13-31-991-006 Fig. 404
52-13-31-991-007 Fig. 405
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3(2)
