(13)
 of the cargo door as follows:

 (a)
 If removed, install the bushes (22) and (23) into the actuator attachment fitting (13).

 (b)
 Put the piston eye end (18) to the actuator attachment fitting

 (13) and install the bolt (14) with the washer (15).

 (c)
 If you cannot install the bolt (14) easily, you must adjust the length of the door actuator (Ref. TASK 52-32-11-820-004).

 (d)
 Install the washer (15) and the nut (16) on the bolt (14).

 (e)
 TORQUE the nut (16) to between 1.0 and 1.35 m.daN (88.49 and

 119.46 lbf.in) and safety it with the new cotter pin (17).

 (f)
 Install the bonding jumpers (10) with the bolts (12), the washers

 (11) and the nuts (9) at the actuator attachment fitting (13) (Ref. TASK 20-28-00-912-004).

 (11)
 Install the wire harness 4613VB (21) to the ceiling lining and connect the connector (20) to the receptacle (19)(Ref. TASK 52-32-24-400-001).

 (12)
 If you install the bonding jumpers (8) at the cargo door, install them with the bolts (6) and the washers (7) to the upper fuselage at FR53 and FR55A (Ref. TASK 20-28-00-912-004).

 (13) Do the Preparation for Installation Procedure. (Ref. Para. A.). R **ON A/C 151-199, 401-499,
 Subtask 52-32-11-910-050-A
 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.

R 1EFF : 051-052, 151-199, 401-499, 1 52-32-11Page 428 1 1 Aug 01/05 1 1 1CES 1

 (5)
 Apply COMMON GREASE (Material No. 04-011) to the bushes of all piano hinges and to the hinge pins (24).

 (6)
 Apply SEALANTS (Material No. 09-005) to the countersink of the screws (31).

 (7) Apply COMMON GREASE (Material No. 04-011) to the bolt (14). Subtask 52-32-11-420-050-A
 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 half of the fuselage.

 (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 FR57 and FR57A.

 Table for Selection of Washers (Item 25 thru Item 28)
R 1EFF : 151-199, 401-499, 1 52-32-11Page 429 1 1 Aug 01/05 1 1 1CES 1

 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)
 0.4 (0.015) - 0.5 (0.020) | -| 1 | -| _ | 0.4 (0.015)
 0.5 (0.020) - 0.6 (0.024) | -| -| 1 | _ | 0.5 (0.020)
 0.6 (0.024) - 0.7 (0.028) | 2 | -| -| _ | 0.6 (0.024)
 0.7 (0.028) - 0.8 (0.031) | 1 | 1 | -| _ | 0.7 (0.028)
 0.8 (0.031) - 0.9 (0.035) | -| 2 | -| _ | 0.8 (0.031)
 0.9
 (0.035) - 1.0 (0.039) | -| 1 | 1 | _ | 0.9 (0.035)

 1.0
 (0.039) - 1.1 (0.043) | -| -| 2 | _ | 1.0 (0.039)

 1.1 (0.043) - 1.2 (0.047) | 1 | 2 | -| _ | 1.1 (0.043)
 1.2 (0.047) - 1.3 (0.051) | 1 | 1 | 1 | _ | 1.2 (0.047)
 1.3 (0.051) - 1.4 (0.055) | 1 | -| 2 | _ | 1.3 (0.051)
 1.4 (0.055) - 1.5 (0.059) | -| 1 | 2 | _ | 1.4 (0.055)
 1.5 (0.059) - 1.6 (0.063) | -| -| 3 | _ | 1.5 (0.059)
 1.6 (0.063) - 1.7 (0.067) | 2 | -| 2 | _ | 1.6 (0.063)
 1.7 (0.067) - 1.8 (0.071) | 1 | 1 | 2 | _ | 1.7 (0.067)
　
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(25)