(c)
Remove the lower eye end of the connection rod (27) from the fork end of the vent door lever (21).
(2)
Disconnect the teleflex controls (19) from the drift pin levers (20) as follows:
(a)
Remove and discard the cotter pins (18) from the nuts (17).
(b)
Remove the nuts (17), the washers (15), the bushes (16) and the bolts (14) from the drift pin levers (20).
(c)
Remove the eye ends of the teleflex controls (19) from the fork end of the drift pin levers (20).
1EFF : 051-052, 1 52-32-21Page 466 1 1 Aug 01/05R 1 1 1CES 1
INTENTIONALLY BLANK
R 1 1
52-32-21Page 467
1 1 Aug 01/05 1 1 1CES 1
Safety Shaft Installation
Figure 406/TASK 52-32-21-991-005- 12 (SHEET 1)
1EFF : 051-052, 1 52-32-21Page 468
1 1 Aug 01/05R 1 1
1CES 1
Safety Shaft Installation
Figure 406/TASK 52-32-21-991-005- 22 (SHEET 2)
1EFF : 051-052, 1 52-32-21Page 469
1 1 Aug 01/05R 1 1
1CES 1
(3)
Disconnect the linkage (3) from the link lever (10) as follows:
(a)
Remove and discard the cotter pin (7) from the nut (6).
(b)
Remove the nut (6), the washer (5), the bush (4) and the bolt (1) from the link lever (10).
(c)
Remove the lower eye end of the linkage (3) from the fork end of the link lever (10).
(4)
Disassemble the different components from the safety shaft (11) as follows:
(a)
Remove the nuts (9), the washers (8) and the tapered pins (2) from the safety cams (12),(13).
(b)
Remove the nuts (9), the washers (8) and the tapered pins (2) from the link lever (10), the drift pin levers (20) and the vent door lever (21).
(c)
Move the vent door lever (21) and the link lever (10) from the end of the safety shaft (11).
(5)
Remove the safety shaft (11) from the cargo door structure as follows:
(a) Move the safety shaft (11) slowly in the forward direction through the lateral cutout of the cargo door.
NOTE : Support the safety cams (12),(13) and the drift pin levers
____ (20) during this movement.
(b) Remove the safety cams (12),(13) and the drift pin lever (20) while you remove the safety shaft (11) from the sliding bearing (of each frame forkend).
1EFF : 051-052, 1 52-32-21Page 470 1 1 Aug 01/05R 1 1 1CES 1
TASK 52-32-21-400-004
Installation of the Safety Shaft Assembly
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 3.5 m (11 ft. 6 in.)
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. 15-005 AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
Material No. 15-006 AIB TN 10138 TYPE I GRADE 3 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
7 cotter pin 52-32-21 03 -420 18 cotter pin 52-32-21 20B-010 26 cotter pin 52-32-21 07 -040
1EFF : 051-052, 1 52-32-21Page 471 1 1 Aug 01/05R 1 1 1CES 1
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the
Yellow Electric Pump 52-32-00-720-001 Functional Test of the AFT Cargo-Compartment Door 52-32-11-820-002 Adjustment of the Door Mechanism 52-32-21-991-005 Fig. 406
3. Job Set-up
__________
Subtask 52-32-21-860-053
A. Aircraft Maintenance Configuration
中國航空網(wǎng) 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(91)
