B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-12-29-611-001 Fill the Hydraulic Fluid Reservoir with a Hand Pump 12-12-29-611-002 Fill the Hydraulic Fluid Reservoir with a Hydraulic
Service Cart 29-00-00-870-010 Ram Air Turbine System Bleeding Procedure 29-00-00-910-002 Safety Procedures of the 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
29-00-00-991-013 Fig. 201
3. Job Set-up
__________
Subtask 29-00-00-860-071
A. Aircraft Maintenance Configuration
WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
R (1) Obey the hydraulic safety procedures (Ref. TASK 29-00-00-910-002).
(2)
Make sure that the replaced component is correctly installed.
(3)
Make sure that the hydraulic reservoir of the Blue hydraulic system is depressurized (Ref. TASK 29-14-00-614-001).
(4)
Open the access door 195BB.
Subtask 29-00-00-865-073
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU HYD/HYD PWR/B WARN/& CTL 2702GJ C12 123VU B HYD/ELEC PUMP 2701GJ AB09
4. Procedure
_________ (Ref. Fig. 201/TASK 29-00-00-991-013) Subtask 29-00-00-870-064
A. Bleeding Procedure of the Blue Hydraulic System Upstream of the Blue E-Pump
CAUTION : USE A SECOND WRENCH TO APPLY COUNTERTORQUE TO THE UNION WHEN
_______ YOU DISCONNECT/CONNECT HYDRAULIC LINES ON UNIONS. IF YOU USE THE SECOND WRENCH, YOU WILL NOT LOOSEN OR TIGHTEN THE UNION TOO MUCH.
(1)
Put a container under the Blue E-pump.
(2)
Disconnect the case drain line (2) of the Blue E-pump from the housing (1) of the case drain filter (2084GM).
(3)
Install a blanking plug (4) in the open port of the housing (1).
(4)
Connect the adapter hose (3) to the case drain line (2).
(5)
Put the end of the adapter hose (3) in the container.
(6)
Make sure that the fluid level in the Blue reservoir is correct. Add fluid as necessary (Ref. TASK 12-12-29-611-001) or (Ref. TASK 12-12-29-611-002).
(7)
Slowly pressurize the Blue hydraulic reservoir so that the air or the mixture of hydraulic fluid and air comes out from the adapter hose
(3) and into the container (Ref. TASK 29-14-00-614-002).
(8)
Depressurize the Blue hydraulic reservoir when the hydraulic fluid flows freely without air (Ref. TASK 29-14-00-614-001).
(9)
Disconnect the adapter hose (3) from the case drain line (2).
(10)
Remove the blanking plug (4) from the housing (1).
(11)
Make sure that the hydraulic line end-fittings are serviceable.
(12)
Connect the case drain line (2) to the housing (1).
(13)
TORQUE the nut of the case drain line (2) to between 2.9 and 3.2 m.daN (21.38 and 23.59 lbf.ft).
1EFF : ALL 1 29-00-00Page 242 1 1 May 01/04R 1 1 1CES 1
Installation of the Bleeding Adapter Hose at the Case Drain Filter Housing Figure 201/TASK 29-00-00-991-013
1EFF : ALL 1 29-00-00Page 243 1 1 May 01/04R 1 1 1CES 1
(14)
Keep the reservoir depressurization valve (2087GM) open and fill the reservoir to 7.0 l (1.8491 USgal).
(15)
Pressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-002).
(16) 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 HYDRAULIC POWER 液壓1(58)
