R (c) Remove the coupling cap (8) from the coupling (1).
R NOTE : The coupling cap (8) will hang by the chain (9) from the____
R shroud-ring (5).
R (d) Remove the bolt (7) that attaches the attachment tag (10) to the
R shroud-ring (5).
R NOTE : The attachment tag (10) will stay connected to the chain____
R (9).
R (e) Remove the coupling cap (8) together with the chain (9).
R (f) Hold the element assembly (4) and remove the remaining bolts (7)
R and the washers (6).
R (g) Put a container below the coupling (1).
R (h) Carefully remove the shroud-ring (5) and the element assembly
R (4), and drain the fuel that remains into the container. Remove
R the container.
R (i) Remove the laminated shim(s) (3).
R (j) Remove and discard the O-ring (2).
R (k) On the refuel/defuel panel 800VU:
R 1_ Put the LEFT/RIGHT REFUEL VALVES switch in the NORM position
R and lower the guard.
R 2_ Put the MODE SELECT switch in the OFF position and lower the
R guard.
R (l) Close the access door 192MB.
TASK 28-25-41-400-006 Installation of the Refuel/Defuel Coupling Element Assembly 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. 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
No specific access platform 4.0 m (13 ft. 1 in.) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
1EFF : ALL 1 28-25-41Page 432 1 1 May 01/05 1 1 1CES 1 B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 01-001 Material No. 04-012 Material No. 11-026 Material No. 19-003
R C. Expendable Parts
USA ASTM-D-1655-93 (JET A-1)
FUEL, TURBO (Ref. 20-31-00)
USA VV-P-236
PURE MINERALVASELINE OR PETRO- LATUM (Ref. 20-31-00)
GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
R -------------------------------------------------------------------------------R FIG.ITEM |DESIGNATION |IPC-CSN R -------------------------------------------------------------------------------
R 2 O-ring 28-25-41 03A-040 R 3 shim 28-25-41 03A-030
R D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-003 28-00-00-910-001 28-25-41-991-003 Pressure Refuel with Automatic ControlFuel Safety ProceduresFig. 402
R **ON A/C 051-051,
R 28-25-41-991-004 Fig. 403
R **ON A/C ALL
R 28-25-41-991-006 Fig. 404
1EFF : ALL 1 28-25-41Page 433 1 1 May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
28-25-41-991-007 Fig. 405
**ON A/C 051-051,
28-25-41-991-007-A Fig. 405A
**ON A/C ALL
3. Job Set-up
__________
Subtask 28-25-41-941-061
A. Safety Precautions
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
(1) You must obey the fuel safety procedures (Ref. TASK 28-00-00-910-001) when you do work on the fuel system.
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FUEL 燃油4(66)
