(4)
Safety the correct installed door handle shaft (14) as follows:
(a)
Put the lock device (30) into the slot of door handle shaft (14).
(b)
Attach the lock device (30) with the screws (29) on the door structure (17).
(5)
Install the control rod (57) on the shaft lever (25) as follows:
(a)
Put the upper fork-end of the control rod (57) in position and install the bolt (58), the washers (59) and the nut (60).
(b)
Tighten the nut (60) and safety it with the new cotter pin (61).
(6)
Install the connection rod (45) on the Maltese-cross latch (32) as follows:
(a)
Put the upper fork-end of the control rod (45) in position and install the bolt (49), the washers (48) and the nut (47).
(b)
Tighten the nut (47) and safety it with the new cotter pin (46).
(7) Installation of the Door Handle R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 52-32-21-820-059
D. Adjustment of the Door Handle and the related Linkage Mechanism
(1)
Adjust the door handle to make sure that its skin offset is correct (Ref. TASK 52-32-11-820-002).
(2)
Adjust the linkage mechanism to make sure that the latching and locking mechanism operate satisfactory (Ref. TASK 52-32-11-820-002).
(3)
Make sure that the gap between the target and the sensor of the proximity switch 34WV is correctly adjusted (Ref. TASK 52-71-00-820-004).
R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-32-21Page B436 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 52-32-21-720-056
E. Test Procedure
(1)
Make sure that the door handle mechanism is correctly lubricated (Ref. TASK 12-22-52-640-002).
(2)
Do a functional test to make sure that the force necessary to operate the door handle is correct (Ref. TASK 52-32-00-720-001).
(3)
Make sure that the proximity switch 28WV operates satisfactory (Ref. TASK 52-32-00-710-001).
5. Close-up
________ Subtask 52-32-21-865-076
A. Make sure that this(these) circuit breaker(s) is(are) closed:
1MJ, 3801GX, 3802GX, 3803GX.
**ON A/C 001-049, 053-099, 101-149, 201-299, 301-399,
Subtask 52-32-21-410-060
B. Close Access **ON A/C 001-049, 053-099, 101-105, 201-220,
(Ref. Fig. 403/TASK 52-32-21-991-019) **ON A/C 106-149, 221-299, 301-399,
(Ref. Fig. 403A/TASK 52-32-21-991-019-B) **ON A/C 001-049, 053-099, 101-149, 201-299, 301-399,
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Put the access panel (1) in position to the inner skin of the cargo door and attach it with the screws (3) and (4) and the washers (2).
R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-32-21Page B437 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1
(3) Apply STORAGE PRESERVATION (Material No. 15-005) or STORAGE PRESERVATION (Material No. 15-006) to all the components of the door handle and the related linkage mechanism and to the adjacent cargo door structure.
(4) Install the protection plug (5) in the rear edge member at FR56 and apply a bead of SEALANTS (Material No. 09-016).
(5) Install the access panel 826AR on the cargo door.
(6) Remove the actuator safety locks and close the cargo door (Ref. TASK 52-30-00-860-002).
(7) Remove the access platform(s).
R **ON A/C 151-199, 401-499,
Subtask 52-32-21-410-060-A
B. Close Access
R **ON A/C 151-199,
(Ref. Fig. 403B/TASK 52-32-21-991-019-A)
R **ON A/C 401-499,
R (Ref. Fig. 403C/TASK 52-32-21-991-019-C)
R **ON A/C 151-199, 401-499,
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Put the access panel (1) in position to the inner skin of the cargo door and attach it with the screws (3) and (4) and the washers (2).
(3) Apply STORAGE PRESERVATION (Material No. 15-005) or STORAGE PRESERVATION (Material No. 15-006) to all the components of the door handle and the related linkage mechanism and to the adjacent cargo door structure.
R 1EFF : 001-049, 053-099, 101-149, 151-199, 1 52-32-21Page B438 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 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5(135)
