INTENTIONALLY BLANK
1 1
52-32-24Page 403
1 1 Feb 01/99 1 1 1CES 1
Wirnig Harness 4613VB
Figure 401/TASK 52-32-24-991-001- 12 (SHEET 1)
1EFF : ALL 1 52-32-24 Page 404
1 1 Feb 01/99
1 1
1CES 1
Wirnig Harness 4613VB
Figure 401/TASK 52-32-24-991-001- 22 (SHEET 2)
1EFF : ALL 1 52-32-24 Page 405
1 1 Feb 01/99
1 1
1CES 1
TASK 52-32-24-400-001 Installation of the Wiring Harness 4613VB
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 98D52307515000 1 SAFETY LOCK - ACTUATOR, CARGO DOORS
B. 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 52-32-13-400-001 Installation of the Lining and Insulation 52-32-24-991-001 Fig. 401
3. Job Set-up
__________ Subtask 52-32-24-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the cargo door is opened (Ref. TASK 52-30-00-860-001) and safetied with the SAFETY LOCK - ACTUATOR, CARGO DOORS (98D52307515000).
(2)
Make sure that the access platform in position below the opened cargo door.
1EFF : ALL 1 52-32-24Page 406 1 1 Feb 01/99 1 1 1CES 1 Subtask 52-32-24-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/HYD POWER/Y 3803GX N30 122VU DOORS/CARGO 1MJ T12 123VU Y HYD/ELEC/PUMP 3802GX AB06 123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
4. Procedure
_________
Subtask 52-32-24-420-050
A. Installation of the Wiring Harness 4613VB
(Ref. Fig. 401/TASK 52-32-24-991-001)
(1)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
If removed, assemble the clamps (4), (8) and (16) together with the sleeves (7) and (13) on the wiring harness (1).
(4)
Do an inspection of the component interface and/or the adjacent area.
(5)
Put the clamp (4) in position to the door angle (2) and attach it with the bolt (5) and the nut (3).
(6)
Connect the electrical wires of the wiring harness (1) to the termial
block (6) as follows: -------------------------------------------------------| WIRE NO | TERMINAL NO | | WIRE NO | TERMINAL NO | -------------------------------------------------------| 2552-1105 | 4K | | 2552-1112 | 3H | | 2552-1106 | 4J | | 2552-1113 | 3G | | 2552-1107 | 4H | | 2552-1114 | 3F | | 2552-1108 | 4G | | 3154-5862B | 2G | | 2552-1109 | 4F | | 3152-5862R | 2A | | 2552-1110 | 3E | | 5235-1010B | 1G | | 2552-1111 | 3J | | 5235-1010R | 1A |
1EFF : ALL 1 52-32-24Page 407 1 1 Feb 01/99 1 1 1CES 1
(7)
Put the clamp (8) to the actuator fitting bracket (10) and attach it with the bolt (9) and the washer (11) and the nut (12).
(8)
Measure a distance of 590.0 mm (23.2283 in.) from the door lining to set the clamp (16) in its installation position.
(9)
Put the clamp (16) in position to the bolt (17) of the fitting (18) and attach it with the washer (15) and the nut (14).
(10)
Put the spacer (20), the clamp (21), the spacer (22) and the clamp
(25) in position to the ceiling lining (19).
(11)
Install the screw (23) and the washer (24) on the ceiling panel (19).
(12)
Remove the blanking caps from the electrical connectors.
(13)
Make sure that the electrical connectors are clean and in the correct condition.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM DOORS 舱门6(15)
