W DOC AIRBUS | AMM A320F

Pressure Refuel with Manual Control


TASK 12-11-28-650-004-A
Pressure Refuel with Manual Control


WARNING: OBEY THE FUEL SAFETY PROCEDURES.
WARNING: STOP THE FUEL TANKER 60 m (196.85 ft) FROM THE AIRCRAFT NOSE WHILE THE WEATHER RADAR OPERATES. DO NOT OPERATE THE FUEL TANKER/PUMP UNIT UNTIL YOU STOP THE OPERATION OF THE WEATHER RADAR.
WARNING: MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START THE REFUEL/DEFUEL PROCEDURE. IN THE SAFETY AREA, DO NOT:
  • SMOKE
  • MAKE SPARKS OR FIRE
  • USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR REFUEL/DEFUEL PROCEDURES.
AIRCRAFT FUEL IS FLAMMABLE.
WARNING: DO NOT SPILL FUEL ON THE ENGINES OR THE BRAKES. IF YOU SPILL FUEL ON ENGINES OR BRAKES THAT ARE HOT, IT CAN CAUSE FIRES.
1. Reason for the Job
NOTE: It is recommended that you keep to one type of fuel. Although approved types can be mixed if necessary to continue operation. Refer to Section 2 of your Flight Manual (Ref. FM Section 2) for a complete list of approved fuels. Refer to Airbus Cold Weather Operations Information and Operations Policy Fueling Procedures for safety precautions with mixed fuel.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
No specific
AR
SAFETY BARRIER(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
192MB
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 12-11-28-650-001-A
General Refuel/Defuel Safety Procedures
TASK 12-11-28-650-002-A
Refuel/Defuel Safety Procedures for use in the Hangar
TASK 12-11-28-650-007-A
Use of Magnetic Level Indicators (MLI)
TASK 12-34-24-869-001-A
Aircraft Bonding and Grounding (Earthing) for the Refuel/Defuel or Oxygen Servicing Operations
TASK 24-41-00-861-002-A
Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01
Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02
Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 28-25-00-650-001-A
Pressure Defuel
TASK 28-25-00-869-001-A
Fuel Transfer
TASK 31-60-00-860-001-A
EIS Start Procedure
TASK 31-60-00-860-002-A
EIS Stop Procedure
F Refuel Safety Area ** ON A/C NOT FOR ALL
F Refuel/Defuel Coupling ** ON A/C NOT FOR ALL
F Refuel Safety Area ** ON A/C NOT FOR ALL
F Refuel/Defuel Coupling ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 12-11-28-941-052-A
A. Safety Precautions
   (1) You must obey the refuel/defuel safety precautions (Ref. AMM TASK 12-11-28-650-001) (Ref. AMM TASK 12-11-28-650-002).
   (2) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE adjacent to the refuel coupling 40QM.
   (3) Make sure that the chocks do not touch the tires. The weight of the fuel can lower the aircraft and catch the chocks.
   (4) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
Subtask 12-11-28-281-052-A
B. Drain the Water from the Fuel
   (1) Make sure that a fuel sampling for water contamination check is done to the fuel in the fuel tanker/pump unit.
Subtask 12-11-28-860-053-A ** ON A/C NOT FOR ALL
C. Aircraft Maintenance Configuration
WARNING: MAKE SURE THAT THE FUEL SUPPLY HOSE IS CORRECTLY CONNECTED TO THE COUPLING BEFORE YOU REFUEL/DEFUEL THE AIRCRAFT. DO NOT CONNECT THE FUEL SUPPLY HOSE IF THERE ARE SIGNS OF DAMAGE TO THE AIRCRAFT COUPLING LUGS OR SLOTS.
WARNING: MAKE SURE THAT YOU BOND THE FUEL TANKER TO THE AIRCRAFT. IF YOU DO NOT, AN ELECTRICAL DISCHARGE CAN OCCUR WHICH CAN CAUSE AN EXPLOSION OR FIRE.
   (1) Obey the local regulations for grounding (earthing) the aircraft. If you must ground (earth) the aircraft:
NOTE: You must bond the fuel tanker to the aircraft. Obey the local regulations for grounding (earthing).
   (2) Bond the fuel tanker to the aircraft (Ref. AMM TASK 12-34-24-869-001).
   (3) Remove the refuel coupling cap 41QM.
   (4) Make sure that the coupling of the fuel-supply hose is clean, then connect it to the aircraft refuel coupling.
   (5) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
   (6) Do the Electronic Instrument System (EIS) (Electronic Centralized Aircraft Monitoring - ECAM only) start procedure (Ref. AMM TASK 31-60-00-860-001).
   (7) On the panel 11VU, push (in) the FUEL pushbutton switch.
Subtask 12-11-28-860-053-B ** ON A/C NOT FOR ALL
C. Aircraft Maintenance Configuration
WARNING: MAKE SURE THAT THE FUEL SUPPLY HOSE IS CORRECTLY CONNECTED TO THE COUPLING BEFORE YOU REFUEL/DEFUEL THE AIRCRAFT. DO NOT CONNECT THE FUEL SUPPLY HOSE IF THERE ARE SIGNS OF DAMAGE TO THE AIRCRAFT COUPLING LUGS OR SLOTS.
WARNING: MAKE SURE THAT YOU BOND THE FUEL TANKER TO THE AIRCRAFT. IF YOU DO NOT, AN ELECTRICAL DISCHARGE CAN OCCUR WHICH CAN CAUSE AN EXPLOSION OR FIRE.
   (1) Obey the local regulations for grounding (earthing) the aircraft. If you must ground (earth) the aircraft:
NOTE: You must bond the fuel tanker to the aircraft. Obey the local regulations for grounding (earthing).
   (2) Bond the fuel tanker to the aircraft (Ref. AMM TASK 12-34-24-869-001).
   (3) Remove the applicable refuel coupling cap 101QM(41QM).
   (4) Make sure that the coupling of the fuel supply-hose is clean, then connect it to the aircraft refuel coupling.
   (5) If you have external power available, energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
   (6) If you have external power available:
Subtask 12-11-28-010-053-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Open access door 192MB.
NOTE: If operating in battery power:
  • Set the MODE SELECT switch to the OFF position and the guard position
  • Airbus recommends you to not to keep the door open longer than necessary because the battery power decreases.
Subtask 12-11-28-010-053-B ** ON A/C NOT FOR ALL
D. Get Access
   (1) Open access door 622KB:
  • Put the doorstay into the doorstay bracket to hold access door 622KB in position.
NOTE: If operating in battery power:
  • Put the MODE SELECT switch to the OFF and guarded position
  • Do not keep the door open longer than necessary because the battery can discharge.
Subtask 12-11-28-860-057-A ** ON A/C NOT FOR ALL
E. Aircraft Maintenance Configuration
   (1) If you do not have ground power available:
WARNING: WHEN YOU REFUEL THE AIRCRAFT WITH BATTERY POWER, IT IS NOT ALWAYS POSSIBLE TO REFUEL TO FULL CAPACITY. THIS IS BECAUSE THE INTERCELL TRANSFER VALVES ARE NOT ALWAYS IN THE CORRECT POSITION.
     (a) On the refuel/defuel control panel (800VU), put the BATT POWER switch to the ON position and release.
NOTE: The HOT BUSS 701PP is energized for ten minutes only (this is to prevent discharge of the aircraft batteries), unless you put the MODE SELECT switch (on the refuel/defuel panel) to REFUEL.
Subtask 12-11-28-860-057-B ** ON A/C NOT FOR ALL
E. Aircraft Maintenance Configuration
   (1) If you do not have ground power available:
     (a) On the refuel/defuel control panel (800VU), put the BATT POWER switch to the ON position and release.
NOTE: The HOT BUSS 701PP is energized for ten minutes only (this is to prevent discharge of the aircraft batteries), unless you put the MODE SELECT switch (on the refuel/defuel panel) to REFUEL.
Subtask 12-11-28-740-051-A ** ON A/C NOT FOR ALL
F. Test of the Refuel Panel 800VU
   (1) Do this test:
ACTION
RESULT
1.On the panel 800VU:
On the panel 800VU:
  • put the TEST switch to the LTS position and hold it there
  • the High (HI) Level (LVL) lights and the DEFUEL/XFR OPEN lights are on and the CKPT and END lights come on
  • the FUEL QTY, PRESELECTED and ACTUAL displays show all 8's.
  • release the TEST switch
  • the lights go back to their initial condition
  • the FUEL QTY, PRESELECTED and ACTUAL displays go back to their initial condition
  • put the TEST switch to the HIGH position and hold it there
  • the HI LVL lights change their condition. If they were on, they will go off. If they were off, they will come on
  • release the TEST switch.
  • the HI LVL lights go back to their initial condition.
Subtask 12-11-28-740-051-B ** ON A/C NOT FOR ALL
F. Test of the Refuel Panel 800VU and 801VU
   (1) Do this test:
ACTION
RESULT
1.On the panel 800VU:
On the panel 800VU and 801VU:
  • put the TEST switch to the LTS position and hold it there
  • the HI LVL lights and the DEFUEL/XFR OPEN lights are on and the CKPT and END lights come on
  • the FUEL QTY, PRESELECTED and ACTUAL displays show all 8's
  • release the TEST switch
  • the lights go back to their initial condition
  • the FUEL QTY, PRESELECTED and ACTUAL displays go back to their initial condition
  • put the TEST switch to the HIGH position and hold it there
  • the HI LVL lights change their condition. If they were on, they will go off. If they were off, they will come on
  • release the TEST switch.
  • the HI LVL lights go back to their initial condition.
Subtask 12-11-28-740-051-C ** ON A/C NOT FOR ALL
F. Do a test of refuel/defule Panel 800VU and 801VU

NOTE: The HI LVL lights of the ACTs that are not installed will not come on during this test.
   (1) Do this test:
ACTION
RESULT
On panel 800VU:
  • Set the TEST switch to the LTS position and hold it there.
On panels 800VU and 801VU:
  • The HI LVL lights, the DEFUEL XFR OPEN light and the AFMS FAULT light come on.

On preselector 5QT:
  • the PRESELECTED and ACTUAL displays show all eights.
  • The CKPT and END lights come on.

On indicator 6QT:
  • The FUEL QTY displays show all eights.
  • Release the TEST switch.
On panels 800VU and 801VU:
  • The HI LVL lights, the DEFUEL XFR OPEN light and the AFMS FAULT light go off.

On preselector 5QT:
  • The CKPT and END lights go off
  • The PRESELECTED and ACTUAL displays show the tank quantities.

On indicator 6QT:
  • The FUEL QTY displays show the tank quantities.
Subtask 12-11-28-740-051-D ** ON A/C NOT FOR ALL
F. Test of the Refuel Panel 800VU and 801VU
   (1) Do this test:

NOTE: The HI LVL lights of the Additional Center Tanks (ACTs) that are not installed will not come on during this test.
ACTION
RESULT
1.On the panel 800VU:
On the panel 800VU and 801VU:
  • put the TEST switch to the LTS position and hold it there
  • the HI LVL lights and the DEFUEL/XFR OPEN lights are on and the CKPT and END lights come on
  • the FUEL QTY, PRESELECTED and ACTUAL displays show all 8's
  • release the TEST switch
  • the lights go back to their initial condition
  • the FUEL QTY, PRESELECTED and ACTUAL displays go back to their initial condition
  • put the TEST switch to the HIGH position and hold it there
  • the HI LVL lights change their condition. If they were on, they will go off. If they were off, they will come on
  • release the TEST switch.
  • the HI LVL lights go back to their initial condition.
4. Procedure
WARNING: MAKE SURE THAT YOU DO THE REFUEL PANEL TEST BEFORE THE REFUEL PROCEDURE OR BEFORE THE FUEL TANK IS 70 PERCENT FULL. DEFECTIVE HIGH-LEVEL SENSORS CAN CAUSE FUEL TO SPILL OVERBOARD.
Subtask 12-11-28-650-054-B ** ON A/C NOT FOR ALL
WARNING: BEFORE YOU DO THIS REFUEL PROCEDURE, MAKE SURE THAT:
  • ALL THE FUEL PUMPS ARE OFF, OR
  • THE FUEL PUMPS ARE ON WITH MODE SEL PUSHBUTTON-SWITCH 48QA IN THE AUTO POSITION.
IF THE FUEL PUMPS ARE ON AND MODE SEL PUSHBUTTON-SWITCH 48QA IS NOT IN THE AUTO POSITION, THERE IS A RISK THAT FUEL WILL SPILL.
CAUTION: BEFORE YOU CLOSE THE CROSSFEED VALVE, MAKE SURE THAT THE FUEL PUMP(S) IS(ARE) OFF. THIS WILL PREVENT DAMAGE TO THE CROSSFEED VALVE.
CAUTION: BEFORE YOU START THE WING TANK PUMPS, MAKE SURE THAT:
  • THERE IS A MINIMUM OF 750 KG (1653 LB) OF FUEL IN THE APPLICABLE WING TANKS
  • THE MODE SEL PUSHBUTTON SWITCH 48QA IS IN THE AUTO POSITION.
THIS WILL PREVENT DRY RUNNING AND SUBSEQUENT DAMAGE TO THE WING AND CENTER TANK PUMPS.
A. Pressure Refuel with Manual Control
NOTE: If it becomes necessary, defuel (Ref. AMM TASK 28-25-00-650-001) or transfer fuel (Ref. AMM TASK 28-25-00-869-001).
   (1) To prevent a fuel spill, on the panel 40VU, make sure that:
  • X FEED P/BSW 4QE is released out (OFF)
  • MODE SEL P/BSW 48QA is in the AUTO position
  • CTR TK PUMP 1 & 2 P/BSW are released out (OFF).
   (2) On the refuel/defuel control panel 800VU:
     (a) Put the MODE SELECT switch to the REFUEL position.
     (b) Put the REFUEL VALVES switch(es) for the applicable fuel tank(s) to the OPEN position.
     (c) Put the REFUEL VALVES switch(es) for the tank(s) which will not be refueled to the SHUT position.
   (3) Before refuel, record actual fuel quantity indicated on preselector 5QT and fuel tanker. When refuel is complete do a discrepancy check.
   (4) Start the pump on the fuel tanker/pump unit.
CAUTION: DO NOT LET THE REFUEL PRESSURE BE MORE THAN THE MAXIMUM PRESSURE OF 50 PSI (3.45 BARS). IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE AIRCRAFT OR EQUIPMENT CAN OCCUR.
   (5) On the refuel/defuel control panel 800VU:
     (a) Make sure that the numbers on the ACTUAL and the FUEL QTY displays increase.
     (b) Monitor the FUEL QTY displays.
NOTE: Refer to the fuel tables for the maximum capacity of each fuel tank and for the total fuel capacity.
NOTE: If necessary, to dispatch with full fuel load, use the ECAM to make sure the outer cell is full. This will prevent the risk of structural damage.
     (c) When each tank has the correct fuel quantity put its REFUEL VALVE switch to the SHUT position.
   (6) When the fuel tank quantities are correct stop the pump on the fuel tanker/pump unit.
   (7) On the refuel/defuel control panel 800VU:
     (a) Put the MODE SELECT switch to the OFF position and put the guard on the switch.
     (b) Put the applicable REFUEL VALVES switch(es) to the NORM position and put the guard(s) on the switch(es).
   (8) If you have ground power available, make sure that the ECAM lower DU shows the correct fuel quantities.
Subtask 12-11-28-650-054-D ** ON A/C NOT FOR ALL
A. Pressure Refuel with Manual Control
CAUTION: BEFORE YOU DO THIS REFUEL PROCEDURE, MAKE SURE THAT:
  • ALL THE FUEL PUMPS ARE OFF, OR
  • THE FUEL PUMPS ARE ON WITH THE MODE SEL PUSHBUTTON SWITCH 4QL IN THE AUTO POSITION.
IF THE FUEL PUMPS ARE ON AND THE MODE SEL PUSHBUTTON SWITCH 4QL IS NOT IN THE AUTO POSITION, THERE IS A RISK THAT FUEL WILL SPILL.
CAUTION: BEFORE YOU CLOSE THE CROSSFEED VALVE, MAKE SURE THAT THE FUEL PUMP(S) IS(ARE) OFF. THIS WILL PREVENT DAMAGE TO THE CROSSFEED VALVE.
CAUTION: BEFORE YOU START THE WING TANK PUMPS, MAKE SURE THAT THERE IS A MINIMUM OF 750 KG (1653 LB) OF FUEL IN THE APPLICABLE WING TANKS. THIS WILL PREVENT DRY RUNNING AND SUBSEQUENT DAMAGE TO THE FUEL PUMPS.
   (1) If it is necessary, defuel (Ref. AMM TASK 28-25-00-650-001) or move fuel (Ref. AMM TASK 28-25-00-869-001).
   (2) To prevent a fuel spill, on panel 40VU, make sure that:
  • X FEED P/BSW 4QE is released out (OFF)
  • MODE SEL P/BSW 4QL is in the AUTO position
  • The CTR TK L and R XFR P/BSW are released out (OFF).
   (3) On the refuel/defuel control panel 800VU:
     (a) Set the MODE SELECT switch to the REFUEL position.
     (b) Set the REFUEL VALVES switch(es) for the applicable fuel tank(s) to the OPEN position.
     (c) Set the REFUEL VALVES switch(es) for the tank(s) which will not be refueled to the SHUT position.
   (4) Before refuel, record actual fuel quantity indicated on preselector 5QT and fuel tanker. When refuel is complete do a check.
   (5) Start the pump on the fuel tanker/pump unit.
CAUTION: DO NOT LET THE REFUEL PRESSURE BE MORE THAN THE MAXIMUM PRESSURE OF 50 PSI (3.45 BARS). IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE AIRCRAFT OR EQUIPMENT CAN OCCUR.
   (6) On the refuel/defuel control panel 800VU:
     (a) Make sure that the numbers on the ACTUAL and the FUEL QTY displays increase.
     (b) Monitor the FUEL QTY displays.
  • Refer to the fuel tables for the maximum capacity of each fuel tank and for the total fuel capacity.
     (c) When each tank has the correct fuel quantity set its REFUEL VALVE switch to the SHUT position.
   (7) When fuel tank quantities are correct stop the pump on the fuel tanker/pump unit.
   (8) On refuel/defuel control panel 800VU:
     (a) Set the MODE SELECT switch to the OFF position and set the guard on the switch.
     (b) Set the applicable REFUEL VALVES switch(es) to the NORM position and set the guard(s) on the switch(es).
   (9) If you have ground power available, make sure that the ECAM lower DU shows the correct fuel quantities.
Subtask 12-11-28-650-054-E ** ON A/C NOT FOR ALL
CAUTION: BEFORE YOU CLOSE THE CROSSFEED VALVE, MAKE SURE THAT THE FUEL PUMP(S) IS(ARE) OFF. THIS WILL PREVENT DAMAGE TO THE CROSSFEED VALVE.
CAUTION: BEFORE YOU DO THIS REFUEL PROCEDURE, MAKE SURE THAT:
  • ALL THE FUEL PUMPS ARE OFF, OR
  • THE FUEL PUMPS ARE ON WITH THE MODE SEL PUSHBUTTON SWITCH 4QL IN THE AUTO POSITION.
IF THE FUEL PUMPS ARE ON AND THE MODE SEL PUSHBUTTON SWITCH 4QL IS NOT IN THE AUTO POSITION, THERE IS A RISK THAT FUEL WILL SPILL.
CAUTION: BEFORE YOU START THE WING TANK PUMPS, MAKE SURE THAT THERE IS A MINIMUM OF 750 KG (1653 LB) OF FUEL IN THE APPLICABLE WING TANKS. THIS WILL PREVENT DRY RUNNING AND SUBSEQUENT DAMAGE TO THE FUEL PUMPS.
A. Pressure Refuel with Manual Control
NOTE: If it becomes necessary, defuel (Ref. AMM TASK 28-25-00-650-001) or transfer fuel (Ref. AMM TASK 28-25-00-869-001).
   (1) To prevent a fuel spill, on panel 40VU, make sure that:
  • The X FEED P/BSW 4QE is released out (OFF)
  • The MODE SEL P/BSW 4QL is in the AUTO position
  • The CTR TK L and R XFR P/BSW are released out (OFF).
   (2) On refuel/defuel control panel 800VU:
     (a) Put the MODE SELECT switch to the REFUEL position.
     (b) Put the REFUEL VALVES switch(s) for the applicable fuel tank(s) to the OPEN position.
     (c) Put the REFUEL VALVES switch(s) for the tank(s) which will not be refueled to the SHUT position.
   (3) Before refuel, record actual fuel quantity indicated on preselector 5QT and fuel tanker. When refuel is complete do a discrepancy check.
   (4) Start the pump on the fuel tanker/pump unit.
CAUTION: DO NOT LET THE REFUEL PRESSURE BE MORE THAN THE MAXIMUM PRESSURE OF 50 PSI (3.45 BARS). IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE AIRCRAFT OR EQUIPMENT CAN OCCUR.
   (5) On refuel/defuel control panel 800VU:
     (a) Make sure that the numbers on the ACTUAL and the FUEL QTY displays increase.
     (b) Monitor the FUEL QTY displays.
NOTE: Refer to the fuel tables for the maximum capacity of each fuel tank and for the total fuel capacity.
     (c) When each tank has the correct fuel quantity put its REFUEL VALVE switch to the SHUT position.
   (6) When the fuel tank quantities are correct stop the pump on the fuel tanker/pump unit.
   (7) On refuel/defuel control panel 800VU:
     (a) Put the MODE SELECT switch to the OFF position and put the guard on the switch.
     (b) Put the applicable REFUEL VALVES switch(s) to the NORM position and put the guard(s) on the switch(s).
   (8) If you have ground power available, make sure that the ECAM lower DU shows the correct fuel quantities.
Subtask 12-11-28-650-086-A ** ON A/C NOT FOR ALL
CAUTION: BEFORE YOU DO THIS REFUEL PROCEDURE, MAKE SURE THAT:
  • ALL THE FUEL PUMPS ARE OFF, OR
  • THE FUEL PUMPS ARE ON WITH THE MODE SEL PUSHBUTTON SWITCH 4QL IN THE AUTO POSITION.
IF THE FUEL PUMPS ARE ON AND THE MODE SEL PUSHBUTTON SWITCH 4QL IS NOT IN THE AUTO POSITION, THERE IS A RISK THAT FUEL WILL SPILL.
CAUTION: BEFORE YOU CLOSE THE CROSSFEED VALVE, MAKE SURE THAT THE FUEL PUMP(S) IS(ARE) OFF. THIS WILL PREVENT DAMAGE TO THE CROSSFEED VALVE.
CAUTION: BEFORE YOU START THE WING TANK PUMPS, MAKE SURE THAT THERE IS A MINIMUM OF 750 KG (1653 LB) OF FUEL IN THE APPLICABLE WING TANKS. THIS WILL PREVENT DRY RUNNING AND SUBSEQUENT DAMAGE TO THE FUEL PUMPS.
B. Pressure Refuel with Manual Control (with ACT installed)
NOTE: If it becomes necessary, defuel (Ref. AMM TASK 28-25-00-650-001) or transfer fuel (Ref. AMM TASK 28-25-00-869-001).
   (1) On the panel 40VU, make sure that:
  • the X FEED P/BSW 4QE is not pushed (in) (the ON and OPEN legends of the P/BSW are off).
   (2) On the refuel/defuel control panel 800VU:
     (a) Put the MODE SELECT switch to the REFUEL position.
   (3) On the refuel/defuel control panel 800VU and 801VU:
     (a) Put the REFUEL VALVES switch(es) for the applicable fuel tank(s) to the OPEN position.
     (b) Put the REFUEL VALVES switch(es) for the tank(s) which will not be refueled to the SHUT position.
   (4) Before refuel, record actual fuel quantity indicated on preselector 5QT and fuel tanker. When refuel is complete do a discrepancy check.
   (5) Start the pump on the fuel tanker/pump unit.
CAUTION: DO NOT LET THE REFUEL PRESSURE BE MORE THAN THE MAXIMUM PRESSURE OF 50 PSI (3.45 BARS). IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE AIRCRAFT OR EQUIPMENT CAN OCCUR.
   (6) On the refuel/defuel control panel 800VU:
     (a) Make sure that the numbers on the ACTUAL and the FUEL QTY displays increase.
     (b) Monitor the FUEL QTY displays.
NOTE: Refer to the fuel tables for the maximum capacity of each fuel tank and for the total fuel capacity.
     (c) To monitor the fuel quantity of the center tank, set the FQI SELECT CTR/ACT switch on panel 801VU to the CTR position:
  • on panel 800VU, read the fuel quantity on the CTR FUEL QTY display.
     (d) To monitor the total fuel quantity of the center tank and the ACT:
  • set the FQI SELECT CTR/ACT switch on panel 801VU to the CTR + ACT position
  • on panel 800VU, read the fuel quantity on the CTR FUEL QTY display.
     (e) To monitor the fuel quantity of the ACT, set the FQI SELECT CTR/ACT switch on panel 801VU to the ACT position:
  • on panel 800VU, read the fuel quantity on the CTR FUEL QTY display.
     (f) When each tank has the correct fuel quantity put its REFUEL VALVE switch to the SHUT position.
   (7) When the fuel tank quantities are correct stop the pump on the fuel tanker/pump unit.
   (8) On the refuel/defuel control panel 800VU:
     (a) Put the MODE SELECT switch to the OFF position and put the guard on the switch.
   (9) On the refuel/defuel control panel 800VU and 801VU:
     (a) Put the applicable REFUEL VALVES switch(es) to the NORM position and put the guard(s) on the switch(es).
   (10) If you have ground power available, make sure that the ECAM lower DU shows the correct fuel quantities.
Subtask 12-11-28-650-088-A ** ON A/C NOT FOR ALL
CAUTION: BEFORE YOU DO THIS REFUEL PROCEDURE, MAKE SURE THAT:
  • ALL THE FUEL PUMPS ARE OFF, OR
  • THE FUEL PUMPS ARE ON WITH THE MODE SEL PUSHBUTTON SWITCH 4QL IN THE AUTO POSITION.
IF THE FUEL PUMPS ARE ON AND THE MODE SEL PUSHBUTTON SWITCH 4QL IS NOT IN THE AUTO POSITION, THERE IS A RISK THAT FUEL WILL SPILL.
CAUTION: BEFORE YOU CLOSE THE CROSSFEED VALVE, MAKE SURE THAT THE FUEL PUMP(S) IS(ARE) OFF. THIS WILL PREVENT DAMAGE TO THE CROSSFEED VALVE.
CAUTION: BEFORE YOU START THE WING TANK PUMPS, MAKE SURE THAT THERE IS A MINIMUM OF 750 KG (1653 LB) OF FUEL IN THE APPLICABLE WING TANKS. THIS WILL PREVENT DRY RUNNING AND SUBSEQUENT DAMAGE TO THE FUEL PUMPS.
C. Pressure Refuel with Manual Control (with ACT(s) installed)
NOTE: If it becomes necessary, defuel (Ref. AMM TASK 28-25-00-650-001) or transfer fuel (Ref. AMM TASK 28-25-00-869-001).
   (1) On the panel 40VU, make sure that:
  • the X FEED P/BSW 4QE is not pushed (in) (the ON and OPEN legends of the P/BSW are off).
   (2) On the refuel/defuel control panel 800VU:
     (a) Put the MODE SELECT switch to the REFUEL position.
   (3) On the refuel/defuel control panel 800VU and 801VU:
     (a) Put the REFUEL VALVES switch(es) for the applicable fuel tank(s) to the OPEN position.
     (b) Put the REFUEL VALVES switch(es) for the tank(s) which will not be refueled to the SHUT position.
   (4) Before refuel, record actual fuel quantity indicated on preselector 5QT and fuel tanker. When refuel is complete do a discrepancy check.
   (5) Start the pump on the fuel tanker/pump unit.
CAUTION: DO NOT LET THE REFUEL PRESSURE BE MORE THAN THE MAXIMUM PRESSURE OF 50 PSI (3.45 BARS). IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE AIRCRAFT OR EQUIPMENT CAN OCCUR.
   (6) On the refuel/defuel control panel 800VU:
     (a) Make sure that the numbers on the ACTUAL and the FUEL QTY displays increase.
     (b) Monitor the FUEL QTY displays.
NOTE: Refer to the fuel tables for the maximum capacity of each fuel tank and for the total fuel capacity.
     (c) To monitor the fuel quantity of the center tank, put the FQI SELECT CTR/ACT switch on panel 801VU to the CTR position:
  • on panel 800VU, read the fuel quantity on the CTR FUEL QTY display.
     (d) To monitor the total fuel quantity of the center tank and the ACT(s), put the FQI SELECT CTR/ACT switch on panel 801VU to the CTR + ACT position:
  • on panel 800VU, read the fuel quantity on the CTR FUEL QTY display.
     (e) To monitor the fuel quantity of the ACT(s), put the FQI SELECT CTR/ACT switch on panel 801VU to each ACT position in turn.
  • on panel 800VU, read the fuel quantity of the applicable ACT on the CTR FUEL QTY display.
     (f) When each tank has the correct fuel quantity put its REFUEL VALVE switch to the SHUT position.
   (7) When the fuel tank quantities are correct stop the pump on the fuel tanker/pump unit.
   (8) On the refuel/defuel control panel 800VU:
     (a) Put the MODE SELECT switch to the OFF and guarded position.
   (9) On the refuel/defuel control panel 800VU and 801VU:
     (a) Put the applicable REFUEL VALVES switch(es) to the NORM and guarded position.
   (10) If you have ground power available, make sure that the ECAM lower DU shows the correct fuel quantities.
Subtask 12-11-28-650-080-B ** ON A/C NOT FOR ALL
CAUTION: BEFORE YOU DO THIS REFUEL PROCEDURE, MAKE SURE THAT:
  • ALL THE FUEL PUMPS ARE OFF, OR
  • THE FUEL PUMPS ARE ON WITH THE MODE SEL PUSHBUTTON SWITCH 4QL IN THE AUTO POSITION.
IF THE FUEL PUMPS ARE ON AND THE MODE SEL PUSHBUTTON SWITCH 4QL IS NOT IN THE AUTO POSITION, THERE IS A RISK THAT FUEL WILL SPILL.
CAUTION: BEFORE YOU CLOSE THE CROSSFEED VALVE, MAKE SURE THAT THE FUEL PUMP(S) IS(ARE) OFF. THIS WILL PREVENT DAMAGE TO THE CROSSFEED VALVE.
CAUTION: BEFORE YOU START THE WING TANK PUMPS, MAKE SURE THAT THERE IS A MINIMUM OF 750 KG (1653 LB) OF FUEL IN THE APPLICABLE WING TANKS. THIS WILL PREVENT DRY RUNNING AND SUBSEQUENT DAMAGE TO THE FUEL PUMPS.
D. Pressure Refuel with Manual Control (with ACT provision)
NOTE: If it becomes necessary, defuel (Ref. AMM TASK 28-25-00-650-001) or transfer fuel (Ref. AMM TASK 28-25-00-869-001).
   (1) To prevent a fuel spill, on the panel 40VU, make sure that:
  • the X FEED P/BSW 4QE is released out (OFF)
  • the MODE SEL P/BSW 4QL is in the AUTO position
  • the CTR TK L and R XFR P/BSW are released out (OFF).
   (2) On the refuel/defuel control panel 800VU:
     (a) Put the MODE SELECT switch to the REFUEL position.
   (3) On the refuel/defuel control panel 800VU and 801VU:
     (a) Put the REFUEL VALVES switch(es) for the applicable fuel tank(s) to the OPEN position.
     (b) Put the REFUEL VALVES switch(es) for the tank(s) which will not be refueled to the SHUT position.
   (4) Before refuel, record actual fuel quantity indicated on preselector 5QT and fuel tanker. When refuel is complete do a discrepancy check.
   (5) Start the pump on the fuel tanker/pump unit.
CAUTION: DO NOT LET THE REFUEL PRESSURE BE MORE THAN THE MAXIMUM PRESSURE OF 50 PSI (3.45 BARS). IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE AIRCRAFT OR EQUIPMENT CAN OCCUR.
   (6) On the refuel/defuel control panel 800VU:
     (a) Make sure that the numbers on the ACTUAL and the FUEL QTY displays increase.
     (b) Monitor the FUEL QTY displays.
NOTE: Refer to the fuel tables for the maximum capacity of each fuel tank and for the total fuel capacity.
     (c) When each tank has the correct fuel quantity put its REFUEL VALVE switch to the SHUT position.
   (7) When the fuel tank quantities are correct stop the pump on the fuel tanker/pump unit.
   (8) On the refuel/defuel control panel 800VU:
     (a) Put the MODE SELECT switch to the OFF position and put the guard on the switch.
   (9) On the refuel/defuel control panel 800VU and 801VU:
     (a) Put the applicable REFUEL VALVES switch(es) to the NORM position and put the guard(s) on the switch(es).
   (10) If you have ground power available, make sure that the ECAM lower Display Unit (DU) shows the correct fuel quantities.
Subtask 12-11-28-650-083-C ** ON A/C NOT FOR ALL
CAUTION: BEFORE YOU DO THIS REFUEL PROCEDURE, MAKE SURE THAT:
  • ALL THE FUEL PUMPS ARE OFF, OR
  • THE FUEL PUMPS ARE ON WITH THE MODE SEL PUSHBUTTON SWITCH 4QL IN THE AUTO POSITION.
IF THE FUEL PUMPS ARE ON AND THE MODE SEL PUSHBUTTON SWITCH 4QL IS NOT IN THE AUTO POSITION, THERE IS A RISK THAT FUEL WILL SPILL.
CAUTION: BEFORE YOU CLOSE THE CROSSFEED VALVE, MAKE SURE THAT THE FUEL PUMP(S) IS(ARE) OFF. THIS WILL PREVENT DAMAGE TO THE CROSSFEED VALVE.
CAUTION: BEFORE YOU START THE WING TANK PUMPS, MAKE SURE THAT THERE IS A MINIMUM OF 750 KG (1653 LB) OF FUEL IN THE APPLICABLE WING TANKS. THIS WILL PREVENT DRY RUNNING AND SUBSEQUENT DAMAGE TO THE FUEL PUMPS.
E. Pressure Refuel with Manual Control (with ACT(s) provision)
NOTE: If it becomes necessary, defuel (Ref. AMM TASK 28-25-00-650-001) or transfer fuel (Ref. AMM TASK 28-25-00-869-001).
   (1) To prevent a fuel spill, on the panel 40VU, make sure that:
  • the X FEED P/BSW 4QE is released out (OFF)
  • the MODE SEL P/BSW 4QL is in the AUTO position
  • the CTR TK L and R XFR P/BSW are released out (OFF).
   (2) On the refuel/defuel control panel 800VU/801VU:
  • put the MODE SELECT switch to the REFUEL position
  • put the REFUEL VALVES switch(es) for the applicable fuel tank(s) to the OPEN position
  • put the REFUEL VALVES switches for the tanks which will not be refueled to the SHUT position.
     (a) Before refuel, record actual fuel quantity indicated on preselector 5QT and fuel tanker. When refuel is complete do a discrepancy check.
     (b) Start the pump on the fuel tanker/pump unit.
CAUTION: DO NOT LET THE REFUEL PRESSURE BE MORE THAN THE MAXIMUM PRESSURE OF 50 PSI (3.45 BARS). IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE AIRCRAFT OR EQUIPMENT CAN OCCUR.
     (c) On the refuel/defuel control panel 800VU:
  • make sure that the numbers on the ACTUAL and the FUEL QTY displays increase
  • monitor the FUEL QTY displays.
     (d) On the refuel/defuel control panel 801VU:
  • set the ACT rotary selector to each applicable ACT in turn
  • make sure that the numbers on the ACT FUEL QTY display increases for each applicable ACT
  • monitor the ACT FUEL QTY display.
NOTE: Refer to the fuel tables for the maximum capacity of each fuel tank and for the total fuel capacity.
     (e) When each tank has the correct fuel quantity, put its REFUEL VALVE switch to the SHUT position.
     (f) When the fuel tank quantities are correct, stop the pump on the fuel tanker/pump unit.
     (g) On the refuel/defuel control panel 800VU/801VU:
  • put the MODE SELECT switch to the OFF and guarded position
  • put all the REFUEL VALVES switches to the NORM and guarded position.
     (h) If you have ground power available:
  • make sure that the ECAM lower DU shows the correct total fuel quantities
  • make sure that the fuel indicators on the panel 28VU show the correct quantity for each ACT.
Subtask 12-11-28-650-083-D ** ON A/C NOT FOR ALL
CAUTION: BEFORE YOU CLOSE THE CROSSFEED VALVE, MAKE SURE THAT THE FUEL PUMP(S) IS(ARE) OFF. THIS WILL PREVENT DAMAGE TO THE CROSSFEED VALVE.
CAUTION: BEFORE YOU DO THIS REFUEL PROCEDURE, MAKE SURE THAT:
  • ALL THE FUEL PUMPS ARE OFF, OR
  • THE FUEL PUMPS ARE ON WITH THE MODE SEL PUSHBUTTON SWITCH 4QL IN THE AUTO POSITION.
IF THE FUEL PUMPS ARE ON AND THE MODE SEL PUSHBUTTON SWITCH 4QL IS NOT IN THE AUTO POSITION, THERE IS A RISK THAT FUEL WILL SPILL.
CAUTION: BEFORE YOU START THE WING TANK PUMPS, MAKE SURE THAT THERE IS A MINIMUM OF 750 KG (1653 LB) OF FUEL IN THE APPLICABLE WING TANKS. THIS WILL PREVENT DRY RUNNING AND SUBSEQUENT DAMAGE TO THE FUEL PUMPS.
E. Pressure Refuel with Manual Control (with ACT(s) provision)
NOTE: If it necessary, defuel (Ref. AMM TASK 28-25-00-650-001) or transfer fuel (Ref. AMM TASK 28-25-00-869-001).
   (1) To prevent a fuel spill, on panel 40VU, make sure that:
  • X FEED P/BSW 4QE is released out (OFF)
  • MODE SEL P/BSW 4QL is in the AUTO position
  • The CTR TK L and R XFR P/BSW are released out (OFF).
   (2) On refuel/defuel control panel 800VU/801VU:
  • Set the MODE SELECT switch to the REFUEL position
  • Set the REFUEL VALVES switch(s) for the applicable fuel tank(s) to the OPEN position
  • Set the REFUEL VALVES switches for the tanks which will not be refueled to the SHUT position.
     (a) Before refuel, record actual fuel quantity indicated on preselector 5QT and fuel tanker. When refuel is complete do a fuel quantity check.
     (b) Start the pump on the fuel tanker/pump unit.
CAUTION: DO NOT LET THE REFUEL PRESSURE BE MORE THAN THE MAXIMUM PRESSURE OF 50 PSI (3.45 BARS). IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE AIRCRAFT OR EQUIPMENT CAN OCCUR.
     (c) On refuel/defuel control panel 800VU:
  • Make sure that the numbers on the ACTUAL and the FUEL QTY displays increase
  • Monitor the FUEL QTY displays.
     (d) On refuel/defuel control panel 801VU:
  • Set the ACT rotary selector to each applicable ACT in turn
  • Make sure that the numbers on the ACT FUEL QTY display increases for each applicable ACT
  • Monitor the ACT FUEL QTY display.
     (e) Refer to the fuel tables for the maximum capacity of each fuel tank and for the total fuel capacity (Ref. AMM TASK 12-11-28-650-007).
     (f) When each tank has the correct fuel quantity, set its REFUEL VALVE switch to the SHUT position.
     (g) When the fuel tank quantities are correct, stop the pump on the fuel tanker/pump unit.
     (h) On refuel/defuel control panel 800VU/801VU:
  • Set the MODE SELECT switch to the OFF and guarded position
  • Set all the REFUEL VALVES switches to the NORM and guarded position.
     (i) If you have ground power available:
  • Make sure that the ECAM lower DU shows the correct total fuel quantities
  • Make sure that the fuel indicators on panel 28VU show the correct quantity for each ACT.
5. Close-up
Subtask 12-11-28-860-058-A ** ON A/C NOT FOR ALL
A. Aircraft Configuration
   (1) Make an entry in the aircraft technical log, to check the fuel configuration before the subsequent flight.
   (2) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
   (3) Disconnect the coupling of the fuel supply-hose from the aircraft refuel/defuel coupling.
   (4) Install the coupling cap.
CAUTION: MAKE SURE THAT THE HANDLE OF THE REFUEL COUPLING CAP POINTS AFT WHEN THE CAP IS CLOSED AND LOCKED.
   (5) Install the refuel coupling cap 41QM.
Subtask 12-11-28-860-058-B ** ON A/C NOT FOR ALL
A. Aircraft Configuration
   (1) If you have external power available, do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002) then de-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
   (2) Disconnect the coupling of the fuel supply-hose from the aircraft refuel/defuel coupling.
   (3) Install the coupling cap.
CAUTION: MAKE SURE THAT THE HANDLE OF THE REFUEL COUPLING CAP POINTS AFT WHEN THE CAP IS CLOSED AND LOCKED.
   (4) Install the applicable refuel coupling cap 101QM(41QM).
Subtask 12-11-28-410-052-A ** ON A/C NOT FOR ALL
B. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close access door 192MB.
Subtask 12-11-28-942-053-A ** ON A/C NOT FOR ALL
C. Removal of Equipment
   (1) Disconnect the bonding and grounding (earthing) 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 ground support and maintenance equipment, the special and standard tools and all other items.
Subtask 12-11-28-410-052-B ** ON A/C NOT FOR ALL
D. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the doorstay from the doorstay bracket and close the access door 622KB.
Subtask 12-11-28-942-053-B ** ON A/C NOT FOR ALL
E. Removal of Equipment
   (1) Disconnect the bonding and grounding (earthing) 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).
   (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.03.31 22:54:34 UTC