(2)
Remove the nuts (6), the washers (5), the bolts (3), and disconnect the bonding strips (4) and (19).
(3)
Remove the nuts (17) and the bolts (16).
(4)
Remove the nuts (10) and the bolts (9).
(5)
Loosen the nuts (13) (Ref. Detail C).
(6)
Remove the nuts (30), the bonding lug (31) and the drive assembly (32).
(7)
Remove the screws (2).
(8)
Engage the line (14) into the line (15) and the line (11) into the line (7).
(9)
Remove the valve (20). Remove and discard the O-ring (21) and the O-rings (12).
(10) Put blanking plugs on the disconnected line ends.
R 1EFF : 106-149, 221-228, 231-299, 301-399, 1 28-25-43Page 406 1401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C ALL
TASK 28-25-43-400-001
Installation of the Defuel/Transfer Valve (11QM)
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific access platform 1.65 m (5 ft. 5 in.)
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
Material No. 01-001 USA ASTM-D-1655-93 (JET A-1) FUEL, TURBO (Ref. 20-31-00) R Material No. 04-017 USA A-A-59173 SILICONE GREASE (Ref. 20-31-00) Material No. 09-001 USA MIL-S-8802 TYPE I CLASS A FUEL TANK SEALANTPOLYSULFIDE (Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
12 O-rings 28-25-05 03 -060 12 O-rings 28-25-05 03A-060 21 O-ring 28-25-05 03 -050 21 O-ring 28-25-05 03A-050
1EFF : ALL 1 28-25-43Page 407 1 1 Aug 01/04 1 1 1CES 1 D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-003 Pressure Refuel with Automatic Control
28-25-00-650-001 Pressure Defuel
28-25-00-710-002 Operational Test of the Defuel System
28-25-53-000-001 Removal of the Center-Tank Defuel/Transfer
Valve-Actuator (11QU)
28-25-53-400-001 Installation of the Center-Tank Defuel/Transfer
Valve-Actuator (11QU)
32-12-00-010-001 Open the Main Gear Doors for Access
32-12-00-410-001 Close the Main Gear Doors after Access
57-17-11-000-001 Removal of the Covers 147AZ (148AZ)
57-17-11-400-001 Installation of the Covers 147AZ (148AZ)
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-220, 229-230,
28-25-43-991-001 Fig. 401
R **ON A/C 106-149, 221-228, 231-299, 301-399, 401-499,
28-25-43-991-001-A Fig. 401A
**ON A/C ALL
3. Job Set-up
__________
Subtask 28-25-43-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the center tank is defueled (Ref. TASK 28-25-00-650-001).
(2)
On the refuel/defuel control panel 800VU, make sure that:
-
the MODE SELECT switch is set to OFF,
-
the OPEN warning light is off.
(3)
Make sure that the access platform is in position under the main door of the right main gear.
1EFF : ALL 1 28-25-43Page 408 1 1 Aug 01/05 1 1 1CES 1
(4)
Make sure that the main door of the right main gear is open (Ref. TASK 32-12-00-010-001).
(5)
Make sure that the manhole cover 148AZ is removed (Ref. TASK 57-17-11-000-001).
(6)
Make sure that the valve actuator 11QU is removed (Ref. TASK 28-25-53-000-001).
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-220, 229-230,
(Ref. Fig. 401/TASK 28-25-43-991-001) R **ON A/C 106-149, 221-228, 231-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 28-25-43-991-001-A) R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-220, 229-230,
Subtask 28-25-43-420-050
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(jī)維護(hù)手冊 AMM FUEL 燃油4(79)
