**ON A/C 051-052,
R (Ref. Fig. 401A/TASK 52-32-11-991-005-B) **ON A/C 151-199, 401-499,
(Ref. Fig. 401B/TASK 52-32-11-991-005-A) **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
R (Ref. Fig. 402/TASK 52-32-11-991-006) **ON A/C 151-199, 401-499,
(Ref. Fig. 402A/TASK 52-32-11-991-006-A) **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
R (Ref. Fig. 403/TASK 52-32-11-991-004) **ON A/C 151-199, 401-499,
(Ref. Fig. 403A/TASK 52-32-11-991-004-A) **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
R (Ref. Fig. 404/TASK 52-32-11-991-007) **ON A/C 151-199, 401-499,
(Ref. Fig. 404A/TASK 52-32-11-991-007-A)
Installation of the Cargo Door Sling
Figure 403/TASK 52-32-11-991-004
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 52-32-11Page 418 1301-399, 1May 01/05 1 1 1CES 1
Installation of the Cargo Door Sling
Figure 403A/TASK 52-32-11-991-004-A
R 1EFF : 151-199, 401-499, 1 52-32-11Page 419 1 1 Aug 01/05 1 1 1CES 1
Gaps on AFT Cargo-Compartment Door
Figure 404/TASK 52-32-11-991-007
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 52-32-11Page 420 1301-399, 1May 01/05 1 1 1CES 1
Gaps on AFT Cargo-Compartment Door
Figure 404A/TASK 52-32-11-991-007-A
R 1EFF : 151-199, 401-499, 1 52-32-11Page 421 1 1 Aug 01/05 1 1 1CES 1
R **ON A/C 001-049, 053-099, 101-149, 201-299, 301-399,
Subtask 52-32-11-910-050
A. Preparation for the Installation
(1)
Clean the component interface and/or the adjacent area.
(2)
Examine the door frame of the fuselage for the correct condition.
(3)
Examine the bushes in the piano hinges of the fuselage for possible damage. If necessary, replace the applicable piano hinges halves.
(4)
Make sure that the hinge pins (24) are clean and in the correct condition.
(5)
Apply SEALANTS (Material No. 09-005) to the countersink of the screws (22).
(6)
Prepare the shims (29) as follows:
(a)
Put the shims (29) and the end fitting (30) in posotion to the fuselage.
(b)
Measure the offset between the end fittings (30) and the remaining piano hinge halves of the fuselage.
(c)
Prepare the shims (29) until the end fittings (30) are align with the remaining piano hinge halves.
NOTE : A tolerance of 0.2 mm (0.0078 in.) is permitted.
____
(d) Apply SEALANTS (Material No. 09-005) to the mating surface of the shim (29) and the fuselage.
(7) Apply COMMON GREASE (Material No. 04-011) to the bolt (18). Subtask 52-32-11-420-050
B. Installation of the Cargo Door
(1)
Move the replacement cargo door into its correct installation position.
(2)
Make sure that you align the piano hinge half of the cargo door with the piano hinge half of the fuselage.
R 1EFF : 001-049, 053-099, 101-149, 201-299, 1 52-32-11Page 422 1301-399, 1May 01/05 1 1 1CES 1
(3)
Install the hinge pins (24) with the EXTRACTOR - HINGE PINS, CARGO DOOR (98D52307523000) to connect the two parts of the piano hinge.
(4)
Adjust the lateral gaps between the cargo door and the fuselage as follows:
(a)
Make sure that the door handle is in the UNLOCKED position.
(b)
Close the cargo door carefully with the crane and put the door handle in the LOCKED position.
(c)
Make sure that the lateral gaps 'A' thru 'D' are correct.
(d)
Measure the gaps 'G' between the piano hinge of the cargo door and the piano hinge of the fuselage.
(e)
Pull out the hinge pins (24) approximately 150 mm (5.9055 in.) and install the correct washers (25), (26), (27), (28). Refer to the subsequent table for the selection of the correct washers. Do this between FR54 and FR54A.
Table for Selection of Washers (Item 25 thru Item 28)
GAP 'G' IN mm (in.) | ITEM 25 | ITEM 26 | ITEM 27 | ITEM 28 | THICKNESS --------------------------|---------|---------|---------|---------|------------
0.0 (0.000) - 0.3 (0.011) | -| -| -| _ | _
0.3 (0.011) - 0.4 (0.015) | 1 | -| -| _ | 0.3 (0.011)
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5(22)
