-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
**ON A/C 001-049, 051-058, 101-101,
29-11-32-991-001 Fig. 401 R **ON A/C 059-099, 102-149, 151-199, 201-299, 301-399, 401-499,
29-11-32-991-001-A Fig. 401A
**ON A/C ALL
3. Job Set-up
__________
Subtask 29-11-32-865-050
A. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/G HYD/PUMP ENG1/CTL 1701GK R35 121VU HYDRAULIC/G HYD/PUMP ENG1/MONG 1702GK R34
Subtask 29-11-32-010-050
B. Get Access
(1)
Open the access door 197CB.
(2)
Open one of the main doors of the main gear (Ref. TASK 32-12-00-010-001).
Subtask 29-11-32-860-050
C. Aircraft Maintenance Configuration
WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
(1)
Obey the hydraulic safety procedures (Ref. TASK 29-00-00-910-002).
(2)
Put the warning notices in position to tell persons not to pressurize the Green hydraulic system:
-in the cockpit on the overhead panel,
- on the ground service panel of the Green hydraulic system.
(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)
Depressurize the reservoir of the Green hydraulic system (Ref. TASK 29-14-00-614-001).
(5)
Put the access platform in position at the main door of the main gear.
(6)
Put a container below the HP manifold of the Green hydraulic system.
(7)
Disconnect the isolation coupling of the power transfer unit (PTU) (Ref. TASK 29-23-00-860-001).
4. Procedure
_________
**ON A/C 001-049, 051-058, 101-101,
(Ref. Fig. 401/TASK 29-11-32-991-001) R **ON A/C 059-099, 102-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 29-11-32-991-001-A)
**ON A/C ALL
Subtask 29-11-32-020-050
A. Removal of the Pressure Relief Valve
(1)
Remove the nut (9), the bolt (6) and the washer (7) and disconnect the bonding jumper (8).
(2)
Hold the pressure relief valve (1) and remove the bolts (2) and the washers (3).
(3)
Remove the pressure relief valve (1).
Pressure Relief Valve
Figure 401/TASK 29-11-32-991-001
R 1EFF : 001-049, 051-058, 101-101, 1 29-11-32Page 404 1 1 May 01/05 1 1 1CES 1
Pressure Relief Valve Figure 401A/TASK 29-11-32-991-001-A
R 1EFF : 059-099, 102-149, 151-199, 201-299, 1 29-11-32Page 405 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
(4)
Remove the bobbins (5) (Ref. TASK 20-23-21-911-001).
(5)
Install blanking plugs in the ports of the pressure relief valve and the HP manifold. (1).
1EFF : ALL 1 29-11-32Page 406 1 1 May 01/99R 1 1 1CES 1
TASK 29-11-32-400-001
Installation of the Pressure Relief Valve of the Green Hydraulic System
(1063GM)
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific container
No specific warning notices
No specific access platform 3.0 m (9 ft. 10 in.)
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R Material No. 02-003 F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)
Material No. 09-013 USA MIL-PRF-81733 TYPE I CLASS A
CORROSION INHIBITING BRUSH CONSISTENCY
(Ref. 20-31-00)
Material No. 16-003 F ASNB70720
COATING (OBSOLETE USE 16-021) (Ref. 20-31-00)
中國航空網 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2(38)
