(5)
 If necessary, remove the flanged bushes (3),(6) and (13) from the structure bracket.

R 1EFF : 051-052, 1 52-32-21Page 495 1 1 Aug 01/05 1 1 1CES 1

 (6) Remove the spring sleeve (23) from the structure bracket as follows:
 (a)
 Remove the spring (24) from the spring sleeve (23).

 (b)
 Release the retaining ring (9) from the pin (20).

 (c)
 Remove the pin (20) together with the spacers (21) and the spring sleeve (23) from the cargo door.

R 1EFF : 051-052, 1 52-32-21Page 496 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL

 TASK 52-32-21-400-006
 Installation of the Interlock Mechanism
 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. 19-010  USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
R 1EFF : ALL 1 52-32-21Page 497 1 1 Aug 01/05 1 1 1CES 1 C. Expendable Parts

 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
8 cotter pin 52-32-21 14 -060 10 cotter pin 52-32-21 14 -130 28 tab washer 52-32-21 15 -080 252 cotter pin 52-32-21 39 -040 252 cotter pin 52-32-21 40 -040 253 cotter pin 52-32-21 39 -260 253 cotter pin 52-32-21 40 -260 257 cotter pin 52-32-21 39 -040 257 cotter pin 52-32-21 40 -040 258 cotter pin 52-32-21 39 -040 258 cotter pin 52-32-21 40 -040 274 tab washer 52-32-21 39 -180 274 tab washer 52-32-21 40 -180
 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 52-32-11-820-002 Adjustment of the Door Mechanism
R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 52-32-21-991-008 Fig. 408
 **ON A/C 051-052,
 52-32-21-991-008-A Fig. 408A
R 1EFF : ALL 1 52-32-21Page 498 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL

 3. Job Set-up
__________ R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 52-32-21-860-057
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the FWD cargo-compartment door (referred to as cargo door) is opened and safetied with the actuator safety locks. (Ref. TASK 52-30-00-860-001).

 (2)
 Make sure that the access platform is in position below the opened cargo door.

 (3)
 Make sure that the access panel 826AR is removed from the cargo door.

 (4) Make sure that the latching mechanism is in the locked condition. **ON A/C 051-052,
 Subtask 52-32-21-860-057-A
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the AFT cargo-compartment door (referred to as cargo door) is opened and safetied with the actuator safety locks. (Ref. TASK 52-30-00-860-001).

 (2)
 Make sure that the access platform is in position below the opened cargo door.

 (3)
 Make sure that the access panel 826AR is removed from the cargo door.

 (4)
 Make sure that the locking mechanism is in the locked condition.

R 1EFF : ALL 1 52-32-21Page 499 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL

 Subtask 52-32-21-865-066
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
 -------------------------------------------------------------------------------
　
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(98)