(3)
Make sure that the Green hydraulic system is depressurized and put it in the maintenance configuration. (Ref. TASK 29-00-00-864-001).
(4)
Make sure that the reservoir of the Green hydraulic system is depressurized (Ref. TASK 29-14-00-614-001).
(5)
Make sure that the left main door of the main gear is open (Ref. TASK 32-12-00-010-001).
(6)
Make sure that the access door 197CB is open.
(7)
Make sure that the access platform is in position.
(8)
Make sure that the container is in position below the manifold.
(9)
Make sure that the isolation coupling of the Power Transfer Unit (PTU) is disconnected (Ref. TASK 29-23-00-860-001).
Subtask 29-11-34-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/LOW/LVL/IND 1832GQ N32 121VU HYDRAULIC/HYD/QTY/IND 1831GQ P35 121VU HYDRAULIC/G HYD/PUMP ENG1/CTL 1701GK R35 121VU HYDRAULIC/G HYD/PUMP ENG1/MONG 1702GK R34
4. Procedure
_________
R **ON A/C 001-049, 051-058, 101-101,
(Ref. Fig. 401/TASK 29-11-34-991-001)
R **ON A/C 059-099, 102-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 29-11-34-991-001-A) **ON A/C ALL
Subtask 29-11-34-420-050
A. Installation of the Fluid Sampling Valve
(1)
Clean the component interface and/or the adjacent area.
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Remove the blanking plugs from the fluid sampling valve (1) and the manifold.
(4)
Apply HYDRAULIC FLUIDS (Material No. 02-003) to the threads of the fluid sampling valve (1) and to the new O-ring (2).
(5)
Put the O-ring (2) in position on the fluid sampling valve (1).
(6)
Install the fluid sampling valve (1) on the manifold.
(7)
TORQUE the fluid sampling valve (1) to between 1.763 and 1.877 m.daN
(13.00 and 13.84 lbf.ft).
(8)
Make sure that the protective cap of the fluid sampling valve is tight.
(9)
Safety the protective cap to the valve body and the valve body to the manifold with lockwire MISCELLANEOUS (Material No. 19-010).
Subtask 29-11-34-790-050
B. Test
(1)
Pressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-002).
(2)
Make sure that the fluid level in the reservoir of the Green hydraulic system is correct. Add fluid as necessary (Ref. TASK 12-12-29-611-001).
(3)
Pressurize the Green hydraulic system (Ref. TASK 29-10-00-863-001).
(4)
Examine the connection of the fluid sampling valve (1) and the manifold and make sure that there are no leaks.
(5)
Depressurize the Green hydraulic system (Ref. TASK 29-10-00-864-001).
5. Close-up
________ Subtask 29-11-34-860-052
A. Put the aircraft back to the serviceable condition.
(1)
Connect the isolation coupling of the power transfer unit (PTU) (Ref. TASK 29-23-00-860-002).
(2)
Remove the container.
(3)
Remove the warning notices from the cockpit and the ground service panel.
Subtask 29-11-34-410-051
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the main door of the main gear (Ref. TASK 32-12-00-410-001).
(3)
Close the access door 197CB. Subtask 29-11-34-865-052
C.
Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1831GQ, 1832GQ, 1701GK, 1702GK.
1EFF : ALL 1 29-11-34Page 410 1 1 Feb 01/01R 1 1 1CES 1
CHECK VALVE - ENGINE 1 THRUST REVERSER (3010KM1) - REMOVAL/INSTALLATION
_______________________________________________________________________ TASK 29-11-35-000-001 Removal of the Engine 1 Thrust Reverser Check Valve (3010KM1) WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
WARNING : DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS FOR A SHORT TIME AFTER
_______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY.
CAUTION : DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC
_______ FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS.
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 HYDRAULIC POWER 液压2(45)
