(7)
Energize the ECAM system (Ref. TASK 31-60-00-860-001).
(8)
On the ECAM control panel, push (in) the FUEL P/BSW.
(9)
On the ECAM lower DU:
-
make sure that the FUEL page is shown
-
make sure that the intercell transfer valves are closed.
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R (10) If the intercell transfer valves are open:
R R (a) Refuel the aircraft until there is a minimum of 1000 kg (2204.6220 lb) of fuel in the wing tank inner cell.
R (b) On panels 49VU and 121VU, open the circuit breakers 1QT and 2QT.
R R NOTE : It is not necessary to install safety clips and tags on____ the circuit breakers.
R (c) After a minimum of 5 seconds, the FQIC will de-energize.
R (d) On panels 49VU and 121VU, close the circuit breakers 1QT and 2QT.
R R (e) After a minimum of 60 seconds, the FQIC will re-energize and cycle the intercell transfer valves.
**ON A/C 301-399,
Subtask 28-25-00-860-075-A
A. Aircraft Maintenance Configuration
(1) Make sure that the aircraft and the fuel tanker/pump unit are grounded correctly (Ref. TASK 12-34-24-869-001) and electrically bonded together correctly.
NOTE : Bonding is essential, grounding is recommended.____
(2) Do a fuel sampling for water contamination check on the fuel in the fuel tanker/pump unit (Ref. TASK 12-32-28-281-001).
(3) Remove the refuel coupling cap 41QM.
(4) Make sure that the coupling of the fuel supply-hose is clean.
(5) Connect the coupling of the fuel supply-hose to the aircraft refuel coupling.
(6) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(7) Energize the ECAM system (Ref. TASK 31-60-00-860-001).
(8) On the ECAM control panel, push (in) the FUEL P/BSW.
R 1EFF : 051-051, 301-399, 1 28-25-00Page 407 1 1 May 01/05 1 1 1CES 1
(9) On the ECAM lower DU:
-make sure that the FUEL page is shown
**ON A/C ALL
Subtask 28-25-00-650-077
B. Fueling CAUTION : DO NOT LET THE REFUEL PRESSURE BE MORE THAN THE MAXIMUM SAFE
_______
PRESSURE OF 50psi (3.45bar).
(1)
Start the pump on the fuel tanker/pump unit.
(2)
Push and hold (in) the manual plunger(s) on the applicable refuel valve(s) 7QU(8QU) or 10QU.
(3)
Monitor the fuel quantity on the ECAM FUEL page.
(4)
When the quantity of fuel in the tank(s) is correct, release (out) the manual plunger(s) on the related refuel valve(s).
(5)
Stop the pump on the fuel tanker/pump unit.
5. Close-up
________ R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 28-25-00-860-076
A. Aircraft Configuration
(1) Disconnect the coupling of the fuel supply-hose from the aircraft refuel/defuel coupling.
CAUTION : MAKE SURE THAT THE HANDLE OF THE REFUEL COUPLING CAP POINTS
_______ AFT WHEN THE CAP IS CLOSED AND LOCKED.
(2) Install the refuel coupling cap 41QM.
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R **ON A/C 051-051,
R Subtask 28-25-00-860-076-A
R A. Aircraft Configuration
R R (1) Disconnect the coupling of the fuel supply-hose from the aircraft refuel/defuel coupling.
R R CAUTION : MAKE SURE THAT THE HANDLE OF THE REFUEL COUPLING CAP POINTS_______ AFT WHEN THE CAP IS CLOSED AND LOCKED.
R (2) Install the applicable refuel coupling cap 101QM(41QM).
R **ON A/C ALL
Subtask 28-25-00-410-084
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) For the left refuel valve 7QU, close the access panel 522JB.
(3) For the right refuel valve 8QU, close the access panel 622JB.
(4) For the center tank refuel valve 10QU, close the RH MLG door 744 (Ref. TASK 32-12-00-410-001).
Subtask 28-25-00-942-083
C. Removal of Equipment
(1) 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.
(2) Remove the safety barriers.
(3) Remove the warning notice(s).
(4) Remove the access platform(s).
