-------------------------------------------------------------------------------
12-12-29-611-001 Fill the Hydraulic Fluid Reservoir with a Hand Pump 20-29-00-911-002 Removal/Installation of an O-ring (Hydraulic Systems) 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 29-13-00-710-002 Operational Test of the Yellow Hydraulic System 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
the Ground Connector 29-24-00-864-001 Depressurize the Yellow Hydraulic System 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 71-13-00-010-040 Opening of the Fan Cowl Doors 71-13-00-410-040 Closing of the Fan Cowl Doors 29-13-36-991-001 Fig. 401
3. Job Set-up
__________
Subtask 29-13-36-860-051-A
A. Aircraft Maintenance Configuration
(1)
Make sure that the Yellow hydraulic system is depressurized (Ref. TASK 29-24-00-864-001).
(2)
Make sure that the Yellow hydraulic reservoir is depressurized (Ref. TASK 29-14-00-614-001).
(3)
Make sure that the warning notice is in position to tell persons not to pressurize the Yellow hydraulic system: - on the ground service panel 198CB.
1EFF : ALL 1 29-13-36Page 406 1 1 Feb 01/05R 1 1 1CES 1
R (4) Make sure that the warning notice is in position on the access door
R 195BB to tell persons not to pressurize the Yellow hydraulic
R reservoir.
R (5) Make sure that an access platform is in position at the engine.
R (6) Make sure that the left fan-cowl door 447AL is open (Ref. TASK 71-13-
R 00-010-040).
R Subtask 29-13-36-941-052-A
R B. Safety Precautions
R (1) On the ENG panel 115VU:
R - make sure that the ENG 2 switch is in the OFF position
R - make sure that the warning notice is in position to tell persons
R not to start the engine.
R (2) Make sure that the engine 2 shutdown occurred not less than 5 minutes
R before you do this procedure.
R (3) Make sure that the warning notice is in position to tell persons not
R to pressurize the Yellow hydraulic system:
R - on the HYD section of the panel 40VU.
R (4) On the ENG section of the panel 50VU:
R - make sure that the ON legend of the ENG/FADEC/GND/PWR 2 pushbutton
R switch is off.
R (5) Make sure that the warning notice is in position to tell persons not
R to energize the FADEC system.
R (6) Make sure that a container is below the check valve.
4. Procedure_________
(Ref. Fig. 401/TASK 29-13-36-991-001)
Subtask 29-13-36-420-051
A. Installation of the Check Valve
(1) Apply HYDRAULIC FLUIDS (Material No. 02-003) to the new O-ring (3).
(2) Install the O-ring (3) on the check valve (1) (Ref. TASK 20-29-00-
911-002).
(3) Remove the blanking plug from the panel (4).
(4) Install the check valve (1) on the panel (4).
R R (5) TORQUE the check valve (1) to between 12.9 and 14.2 m.daN (95.13 and 104.71 lbf.ft).
(6) Remove the blanking plug from the disconnected hose (2).
(7) Connect the hose (2) to the check valve (1).
R R (8) TORQUE the coupling nut to between 9.7 and 10.7 m.daN (71.53 and 78.90 lbf.ft).
Subtask 29-13-36-942-052-A
B. Preparation for the Test
(1) Do the EIS start procedure (Ref. TASK 31-60-00-860-001).
(2) On the ECAM control panel: - push the HYD key and make sure that, on the lower ECAM DU, the HYD page comes into view.
(3) Pressurize the Yellow hydraulic reservoir (Ref. TASK 29-14-00-614-002).
(4) On the HYD page: - make sure that the Yellow pressure is 206 +13.5 -13.5 bar (2987.7766 +195.8008 -195.8008 psi).
Subtask 29-13-36-710-050
C. Operational Test
(1) Do an operational test of the Yellow hydraulic system (Ref. TASK 29-13-00-710-002).
(2) During the dry motoring, make sure that there are no leaks from the check valve.
(3) Make sure that the level of hydraulic fluid in the Yellow reservoir is correct. If necessary, fill the reservoir (Ref. TASK 12-12-29-611-001).
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 HYDRAULIC POWER 液壓4(25)
