(e)
Remove the bushes (34) from the guide fitting (33).
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Guide Arm Attachment
Figure 403/TASK 52-22-11-991-003
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1 1 May 01/04
1 1
1CES 1
(3)
Disconnect the sliding sleeve (50) from the door attachment fitting
(46)
as follows:
(Ref. Fig. 404/TASK 52-22-11-991-004)
(a)
Remove and discard the cotter pin (47) from the nut (48).
(b)
Remove the nut (48), the washers (49) and the bolt (53) from the fork-end of the sliding sleeve (50).
(c)
Remove the spacer sleeve (54) and disconnect the fork end of the sliding sleeve (50) from the traverse (55).
(4)
Disconnect the support arm from the door as follows : (Ref. Fig. 404/TASK 52-22-11-991-004)
(a)
Remove the lower hinge bolt (82) from the control lever (88) as follows:
(b)
Remove the upper hinge bolt (68) from the lifting lever (74) as follows:
1_ Remove and discard the cotter pin (87) from the nut (86),
2_ Remove the nut (86) and the washer (83) from the hinge bolt
(82),
3_ Remove the hinge bolt (82) with the bracket (90), the washers
(83), the bushes (84) and the adjustment washers (80) from the
fork-end (85).
NOTE : Make sure to write down the quantity and the sequence____
of the washers (83) and the adjustment washers (80).
1 Remove and discard the cotter pin (73) from the nut (72),
_ 2 Remove the nut (72) and the washer (69) from the hinge bolt
_ (68),
3 Remove the hinge bolt (68) with the bracket (89), the washers
_ (69), the bushes (70) and the adjustment washers (66) from the fork-end (71).
NOTE : Make sure to write down the quantity and the sequence
____ of the washers (69) and the adjustment washers (66).
(5) Carefully disengage the connection forks (62) and (76) of the support arm from the lifting lever (74) and the control lever (88).
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(6)
Carefully remove the door from the fuselage and put it in the correct
fixture.
(7)
Remove the spacer tube (65) from the connection fork (62) of the support arm as follows:
(a)
Remove the journal pin (61) from the connection fork (62).
(b)
Remove the washers (63), the adjustment washers (64) and the spacer tube (65) from connection fork (62).
(8)
Remove the spacer tube (79) from the connection fork (76) of the support arm as follows:
(a)
Remove the journal pin (75) from the connection fork (76).
(b)
Remove the washers (77), the adjustment washers (78) and the spacer tube (79) from the connection fork (76).
(9)
Remove the traverse (55) from the door attachment fitting (46) as follows:
(a)
Remove and discard the cotter pin (41) from the castle nut (42).
(b)
Remove the nut (42) and the washer (43) from the traverse (55).
(c)
Remove the nuts (51), the bolts (57) with the washers (56) and the flange (52) from the traverse (55).
(d)
Remove the traverse (55) together with the bush (44) from the door attachment fitting (46).
5. Close-up
________ Subtask 52-22-11-860-052
A. Put the system back to the serviceable condition.
(Ref. Fig. 401/TASK 52-22-11-991-001)
(1)
Loosen the fasteners (6) of the sling (5) from the eye-ends of the hoisting lugs (4).
(2)
Remove the hoisting lugs (4) from the hoist fittings (3) and install the plastic plugs (2) again.
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Support Arm Attachment Figure 404/TASK 52-22-11-991-004- 12 (SHEET 1)
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Support Arm Attachment Figure 404/TASK 52-22-11-991-004- 22 (SHEET 2)
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Installation of the Emergency Exit Doors
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
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本文鏈接地址：A320飛機維護手冊 AMM DOORS 艙門3(82)
