_______ SAFE PRESSURE OF 50psi (3.45bar).
(2) Start the pump on the fuel tanker/pump unit.
1EFF : ALL 1 28-25-00Page 445 1 1 May 01/05 1 1 1CES 1
(3)
On the ECAM lower DU:
(a)
Make sure that the fuel quantities increase. NOTE : Refer to the fuel tables for the maximum capacity of each
____ fuel tank and for the total fuel capacity (Ref. TASK 12-11-28-650-007).
(b)
When each tank has the correct fuel quantity put its REFUEL VALVES switch to the SHUT position.
(4)
When the fuel tank quantities are correct stop the pump on the fuel tanker/pump unit.
(5)
On the refuel/defuel control panel 800VU:
(a)
Put the MODE SELECT switch to the OFF and guarded position.
(b)
Put the applicable REFUEL VALVES switch(es) to the NORM and guarded position.
(6)
On the ECAM lower DU:
-make sure that the fuel quantities are correct.
5. Close-up
________
Subtask 28-25-00-860-068
A. Aircraft Maintenance Configuration
(1)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(2)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 28-25-00-410-073
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Disconnect the hose coupling of the fuel tanker at the aircraft refuel/defuel coupling.
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(3) Install the refuel/defuel coupling-cap on the applicable refuel/defuel coupling.
(4) Disconnect these bonding/ground cables: - between the aircraft and the fuel tanker/pump unit - if applicable, between the fuel tanker/pump unit and the ground - if applicable, between the aircraft and the ground.
(5) Close the access door 192MB.
R **ON A/C 051-051,
R Subtask 28-25-00-410-073-A
R B. Close Access
R R (1) Make sure that the work area is clean and clear of tool(s) and other items.
R R (2) Disconnect the hose coupling of the fuel tanker at the aircraft refuel/defuel coupling.
R R (3) Install the refuel/defuel coupling-cap on the applicable refuel/defuel coupling.
R R R R (4) Disconnect these bonding/ground cables: - between the aircraft and the fuel tanker/pump unit - if applicable, between the fuel tanker/pump unit and the ground - if applicable, between the aircraft and the ground.
R (5) Close the access door 522KB.
R **ON A/C ALL
Subtask 28-25-00-942-080
C. Removal of Equipment
(1) Remove the safety barriers.
(2) Remove the warning notice(s).
(3) Remove the access platform(s).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
1EFF : ALL 1 28-25-00Page 448 1 1 May 01/05 1 1 1CES 1 REFUEL/DEFUEL SYSTEM - ADJUSTMENT/TEST
______________________________________
TASK 28-25-00-710-002
Operational Test of the Defuel System
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 3.6 m (11 ft. 10 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-001 General Refuel/Defuel Safety Procedures 12-11-28-650-003 Pressure Refuel with Automatic Control 12-34-24-869-001 Aircraft Grounding for the Refuel/Defuel Operations 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
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