(1)
Clean the component interface and/or the adjacent area.
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Put the double check valve (6) in position on the bracket (7).
(4)
Install the washer (8) and the nut (9) on the double check valve (6).
(5)
Remove the blanking caps from the line ends and from the ports of the double check valve (6).
(6)
Make sure that the hydraulic line end-fittings are serviceable.
(7)
Apply HYDRAULIC FLUIDS (Material No. 02-003) to the treads of the line end fittings.
(8)
Connect the hydraulic lines (1), (2) and (10) on the related ports of the double check valve (6).
1EFF : ALL 1 52-36-13Page 408 1 1 Feb 01/02R 1 1 1CES 1
(9) TORQUE the union nuts of the hydraulic lines (1), (2) and (10) to between 1.5 and 1.7 m.daN (11.06 and 12.53 lbf.ft).
(10) Tighten the nut (9) correctly.
(11) Put the spray cover halves (3) and (5) on the hydraulic connections and attach both halves with new tie-wraps (4).
Subtask 52-36-13-860-050
B. Preparation for the Test
(1) Remove the warning notices from the ground service panel and the overhead panel of the cockpit.
(2) Pressurize the reservoir of the Yellow hydraulic system (Ref. TASK 29-14-00-614-002).
(3) Pressurize the Yellow hydraulic system (Ref. TASK 29-24-00-863-001).
(4) Connect the PTU isolation coupling (Ref. TASK 29-23-00-860-002).
Subtask 52-36-13-865-052
C. Make sure that this(these) circuit breaker(s) is(are) closed: 1MJ, 3801GX, 3802GX, 3803GX
Subtask 52-36-13-710-050
D. Operational Test
R (1) Remove the actuator safety locks and close the cargo door (Ref. TASK 52-30-00-860-002).
R R (2) Open and close the cargo door five times to bleed the door hydraulic system (Ref. TASK 52-36-00-600-001).
R R (3) Make sure that the cargo door is fully opened and the actuator safety locks are installed after the bleeding procedure.
R R (4) Examine the hydraulic connections of the double check valve 3717GM to make sure that there are no leaks.
1EFF : ALL 1 52-36-13Page 409 1 1 Feb 01/02 1 1 1CES 1
5. Close-up
________
**ON A/C 001-049, 051-099, 101-149, 201-299,
Subtask 52-36-13-410-050
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the spillage container from the double check valve 3717GM.
(3)
Install the ceiling panel 151AC in the AFT cargo compartment (Ref. TASK 25-55-11-400-002).
(4)
Remove the actuator safety locks and close the cargo door (Ref. TASK 52-30-00-860-001).
(5) Remove the access platform(s). R **ON A/C 151-199, 401-499,
Subtask 52-36-13-410-050-A
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the spillage container from the double check valve 3717GM.
(3)
Install the ceiling panel 151EC in the AFT cargo compartment (Ref. TASK 25-55-11-400-002).
(4)
Remove the actuator safety locks and close the cargo door (Ref. TASK 52-30-00-860-001).
(5)
Remove the access platform(s).
1EFF : ALL 1 52-36-13Page 410 1 1 Aug 01/05 1 1 1CES 1 1EFF : 301-399, 1 52-36-13Page 411 1 1 May 01/04 1 1 1CES 1 VALVE - MANUAL SELECTOR (2501MJ,2504MJ) - REMOVAL/INSTALLATION
R **ON A/C 301-399,
R Subtask 52-36-13-410-050-B
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Remove the spillage container from the double check valve 3717GM.
R (3) Install the partition panel 151AW in the AFT cargo compartment
R (Ref. TASK 25-55-11-400-001).
R (4) Remove the actuator safety locks and close the cargo door (Ref. TASK
R 52-30-00-860-001).
R (5) Remove the access platform(s).
______________________________________________________________
TASK 52-36-15-000-001
Removal of the Manual Selector Valve 2501MJ/2504MJ
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6(119)
