Component Location
Figure 001
1EFF : ALL 1 29-17-00 Page 2
1 1 Feb 01/98
1 1
1CES 1
Seal Drain System - Schematic
Figure 002
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 29-17-00Page 3 1 1 May 01/05 1 1 1CES 1
Seal Drain System - Schematic
Figure 002A
R 1EFF : 151-199, 301-399, 401-499, 1 29-17-00Page 4 1 1 Aug 01/05 1 1 1CES 1 The FWD collector tank is in the Yellow hydraulic compartment and is attached between FR40 and FR41. The components which drain into the FWD collector tank are:
-
Electric Pump, Blue System
-
Electric Pump, Yellow System
-Power Control Unit (PCU), Slats
-
Air Relief Valve, Green System Reservoir
-
Air Relief Valve, Yellow System Reservoir.
The AFT collector tank is in the main hydraulic compartment. It is attached to the right side of the keelbeam, forward of FR46. The components which drain into it are:
-
Power Control Unit (PCU), Flaps
-
Power Transfer Unit (PTU)
-Constant Speed Motor/Generator (CSM/G)
-Air Relief Valve, Blue System Reservoir.
The components of the system are connected with silicon hoses and aluminium pipes. The system is designed so that fluid drains into the collector tanks under the influence of gravity.
SEAL DRAIN SYSTEM - SERVICING
_____________________________ TASK 29-17-00-680-001 Drain the Collector Tank WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
1.
Reason for the Job
__________________
Refer to the MPD TASK: 291000-18
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific 1 CONTAINER 3 L(3/4 USGAL)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-00-00-910-002 Safety Procedures of the Hydraulic System 32-12-00-010-001 Open the Main Gear Doors for Access 32-12-00-410-001 Close the Main Gear Doors after Access 29-17-00-991-001 Fig. 301
3. Job Set-up
__________ Subtask 29-17-00-010-050
A. Get Access
(1)
Open the access door 196BB of the belly fairing.
(2)
Open the right main door of the main gear (Ref. TASK 32-12-00-010-001).
Subtask 29-17-00-860-050
B. 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 CONTAINER 3 L(3/4 USGAL) in position below the collector tank.
4. Procedure
_________ (Ref. Fig. 301/TASK 29-17-00-991-001) Subtask 29-17-00-680-050
A. Drain the Collector Tank
(1)
Disconnect the hose (1) and the grommet (2) from the collector tank (4).
(2)
Remove the clamp (3) from the collector tank (4).
(3)
Remove the collector tank (4).
(4)
Drain the hydraulic fluid from the collector tank (4) into the container.
(5)
Clean the component interface and/or the adjacent area.
(6)
Do an inspection of the component interface and/or the adjacent area.
(7)
Put the collector tank (4) in position.
(8)
Install the clamp (3).
(9)
Make sure that the hydraulic line end-fittings are serviceable.
Collector Tank
Figure 301/TASK 29-17-00-991-001
1EFF : ALL 1 29-17-00 Page 303
1 1 Nov 01/04
1 1
1CES 1
(10)
Connect the hose (1) and the grommet (2) to the collector tank (4).
(11)
Remove the container.
5. Close-up
________ Subtask 29-17-00-410-050
A. Close Access
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM HYDRAULIC POWER 液壓5(64)
