Installation of the Magnetic-Level-Indicator Assembly 56QM thru 63QM
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
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 safety barriers
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 01-001 USA ASTM-D-1655-93 (JET A-1)
FUEL, TURBO (Ref. 20-31-00) Material No. 04-012 USA VV-P-236
PURE MINERALVASELINE OR PETRO- LATUM (Ref. 20-31-00) Material No. 09-007 USA MIL-S-4383
BRUSHABLE FUEL RESISTANT COATING (Ref. 20-31-00) Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-43-21Page 413 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
FOR FIN 56QM, 57QM
4 O-ring 28-43-05 20 -050
5 O-ring 28-43-05 20 -060
FOR FIN 58QM, 60QM
4 O-ring 28-43-05 21 -090
5 O-ring 28-43-05 21 -100
FOR FIN 59QM, 61QM
4 O-ring 28-43-05 24 -090
5 O-ring 28-43-05 24 -100
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-003 Pressure Refuel with Automatic Control
20-28-00-912-002 Electrical Bonding of Components With Conductive Bolts and Screws in the Tanks
28-10-00-910-001 28-10-00-910-002 Safety Procedures When You Do Work in a Fuel TankAccess to the Fuel Tanks and the Work Areas
28-25-00-650-001 Pressure Defuel
28-25-00-650-003 To Drain Remaining Fuel from the Wing Tanks and the Center Tank
28-25-00-869-001 Fuel Transfer
28-43-21-991-002 57-27-11-000-001 Magnetic-Level-Indicator Assembly 56QM thru 63QMRemoval of the Access Panel (540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB,
57-27-11-400-001 640DB, 640EB, 640FB, 640GB)Installation of the Access Panel (540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB, 640AB, 640BB,
640CB, 640DB, 640EB, 640FB, 640GB)
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3. Job Set-up
__________
Subtask 28-43-21-941-053
A. Safety Precautions
WARNING : OBEY THE SAFETY PROCEDURES WHEN YOU DO WORK IN A FUEL TANK.
_______
(1)
You must obey the fuel safety procedures (Ref. TASK 28-10-00-910-001) when you do work in a fuel tank.
(2)
Make sure that the safety barriers are in position.
Subtask 28-43-21-860-051
B. Aircraft Maintenance Configuration
(1)
Make sure that the applicable fuel tank is defueled (Ref. TASK 28-25-00-650-001).
(2)
Make sure that the remaining fuel has been drained from the applicable fuel tank (Ref. TASK 28-25-00-650-003).
(3)
Make sure that the access platform is below the applicable zone 540(640).
(4)
Make sure that the applicable access panel is removed (Ref. TASK 28-10-00-910-002), (Ref. TASK 57-27-11-000-001).
-
FOR 56QM
remove 540AB
-
FOR 57QM
remove 640AB
-
FOR 58QM
remove 540BB
-
FOR 59QM
remove 640BB
-
FOR 60QM
remove 540DB
-
FOR 61QM
remove 640DB
-
FOR 62QM
remove 540GB
-
FOR 63QM
remove 640GB
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-43-21Page 415 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM FUEL 燃油6(46)
