Door Hoist Fittings Figure 401/TASK 52-13-11-991-002
1EFF : 1 1R 1CES ALL 1 11 1 52-13-11 Page 405 May 01/98
Subtask 52-13-11-020-054
B. Disconnection of the Upper and Lower Guide Arms
(1) Disconnect the guide arms on the door side (Ref. TASK 52-13-12-000-
002).
Subtask 52-13-11-020-055
C. Disconnection of the Door Damper and Emergency-Operation Cylinder
(Ref. Fig. 402/TASK 52-13-11-991-004)
(1) Remove and discard the cotter pin (27).
(2) Remove the nut (28) and the washer (29).
(3) Remove the bolt (33), the lockwasher (32) and the spacer (30).
(4) Disengage the telescopic rod (31) from the eyebolt (26) and fold it
back to the support arm (19).
(5) Remove the eyebolt (26).
(a) Remove the cotter pin (41).
(b) Remove the nut (42) and the washer (43).
(c) Remove the nut (48) and the bolt (44).
(d) Remove the flange (47).
(e) Remove the eyebolt (26) with the washer (46) and the bush (45).
R Subtask 52-13-11-020-056-A
R D. Disconnection of the Support Arm
R (Ref. Fig. 403/TASK 52-13-11-991-005)
R (1) Remove the screws (51) and the washers (52).
R (2) Disconnect the bonding leads (53).
R (3) Remove and discard the cotter pins (56).
R (4) Remove the nuts (57) and the washers (58).
R (5) Make sure that the bolts (60) move smoothly.
1EFF : ALL 1 52-13-11Page 406 1 1 Feb 01/01 1 1 1CES 1
Door Damper and Emergency-Operation Cylinder Figure 402/TASK 52-13-11-991-004
1EFF : 1 1R 1CES ALL 1 11 1 52-13-11 Page 407 May 01/98
Door Attachment to the Support Arm
Figure 403/TASK 52-13-11-991-005
1EFF : ALL 1 52-13-11 Page 408
1 1 Feb 01/98
1 1
1CES 1
R R (6) Adjust the tension of SLING - PASSENGER DOOR (98A52108004001) (10), if necessary.
R R (7) Remove the bolts (60), the washers (61) and the washers sets (62) from the connection links (59).
R R R (8) Disengage and remove the door assy from the upper and lower connection links (59) with the SLING - PASSENGER DOOR (98A52108004001).
Subtask 52-13-11-020-057
E. Removal of the Sling (Ref. Fig. 401/TASK 52-13-11-991-002)
(1) Remove the sling (10) from the hoist fittings.
(2) Remove the hoist fittings (2) from the door and attach them to the sling (10).
(3) Install the blanking plugs (1) in the hoisting points.
5. Close-up________
Subtask 52-13-11-481-050
A. Installation of the Safety Barrier
(1) Install the safety barrier in the opening of the removed door (Ref. TASK 52-00-00-481-001).
1EFF : ALL 1 52-13-11Page 409 1 1 Feb 01/01 1 1 1CES 1 TASK 52-13-11-400-001
Installation 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 two shims (thickness 0.2 mm (0.0078 in))
No specific dynamometer 10 daN (22.4808 lbf)
No specific positioning templates 70 mm (2.7559 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) 98DNSA20206120 1 RIGGING PIN 98D52103006000 1 PIN - RIGGING 98D52103501000 1 BALLAST WEIGHT - PASSENGER CREW DOOR
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)
Material No. 08-007A SEALANT, HIGH TEMP. (Ref. 20-31-00) Material No. 09-005 USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00) 中國航空網 www.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(77)
