Fuel Quantity Panel System (Refueling)
TASK 28-25-00-040-007-A
Fuel Quantity Panel System (Refueling)
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 28-25-00-941-083-A
Subtask 28-25-00-710-063-A ** ON A/C NOT FOR ALL
Subtask 28-25-00-860-068-A
[Rev.10 from 2021]
2026.04.02 06:17:37 UTC
Fuel Quantity Panel System (Refueling)
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.
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:
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 JobNOTE: This deactivation task is not related to an AFM-CDL/MMEL item
2. Job Set-up InformationA. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 190 | BELLY FAIR, AIR CONDITIONING & HYD COMPT |
| 500 | LEFT WING |
| 600 | RIGHT WING |
| 622KB | |
| 192MB, 622HB |
| 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 28-00-00-910-001-A | Fuel Safety Procedures |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
| TASK 28-11-00-00 | TANKS - DESCRIPTION AND OPERATION |
Subtask 28-25-00-941-083-A
A. Safety Precautions
(1) Obey the fuel safety procedures (Ref. AMM TASK 28-00-00-910-001).
(2) Obey refuel/defuel safety procedures (Ref. AMM TASK 12-11-28-650-001) and (Ref. AMM TASK 12-11-28-650-002).
(3) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(4) Put a WARNING NOTICE(S) in position to tell persons not to operate the MLG doors.
Subtask 28-25-00-010-081-A ** ON A/C NOT FOR ALL (1) Obey the fuel safety procedures (Ref. AMM TASK 28-00-00-910-001).
(2) Obey refuel/defuel safety procedures (Ref. AMM TASK 12-11-28-650-001) and (Ref. AMM TASK 12-11-28-650-002).
(3) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(4) Put a WARNING NOTICE(S) in position to tell persons not to operate the MLG doors.
B. Get Access
(1) Open access door 192MB:
(a) If operating in battery power, do not keep the door open longer than necessary because the battery can discharge.
(2) Put an ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below refuel/defuel coupling 40QM.
(3) Remove access panel 622HB.
Subtask 28-25-00-010-081-B ** ON A/C NOT FOR ALL (1) Open access door 192MB:
(a) If operating in battery power, do not keep the door open longer than necessary because the battery can discharge.
(2) Put an ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below refuel/defuel coupling 40QM.
(3) Remove access panel 622HB.
B. Get Access
(1) Put an ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below applicable access panel 622KB.
(2) Open access door 622KB:
(a) If operating in battery power, do not keep the door open longer than necessary because the battery can discharge.
Subtask 28-25-00-860-067-A ** ON A/C NOT FOR ALL (1) Put an ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below applicable access panel 622KB.
(2) Open access door 622KB:
(a) If operating in battery power, do not keep the door open longer than necessary because the battery can discharge.
C. Aircraft Maintenance Configuration
(a) Ground (earth) the fuel tanker/pump unit and the aircraft correctly (Ref. AMM TASK 12-34-24-869-001).
(2) Bond the fuel tanker/pump unit to the aircraft (Ref. AMM TASK 12-34-24-869-001).
(3) Make sure that the chocks do not touch the tires. The weight of the fuel can lower the aircraft and cause the chocks to catch.
(4) Remove refuel/defuel coupling cap 41QM.
(5) Make sure that the hose coupling of the fuel tanker/pump unit is clean.
(7) Set the fuel tanker/pump unit to the refuel mode.
(8) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(9) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
(10) On the ECAM Control Panel (CP), push the FUEL system page Pushbutton Switch (P/BSW).
(a) Make sure that the FUEL page is shown on the ECAM lower Display Unit (DU).
Subtask 28-25-00-860-067-B ** ON A/C NOT FOR ALL 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: (a) Ground (earth) the fuel tanker/pump unit and the aircraft correctly (Ref. AMM TASK 12-34-24-869-001).
(2) Bond the fuel tanker/pump unit to the aircraft (Ref. AMM TASK 12-34-24-869-001).
(3) Make sure that the chocks do not touch the tires. The weight of the fuel can lower the aircraft and cause the chocks to catch.
(4) Remove refuel/defuel coupling cap 41QM.
(5) Make sure that the hose coupling of the fuel tanker/pump unit is clean.
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.
(6) Connect the hose coupling of the fuel tanker/pump unit to aircraft refuel/defuel coupling 40QM. (7) Set the fuel tanker/pump unit to the refuel mode.
(8) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(9) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
(10) On the ECAM Control Panel (CP), push the FUEL system page Pushbutton Switch (P/BSW).
(a) Make sure that the FUEL page is shown on the ECAM lower Display Unit (DU).
C. Aircraft Maintenance Configuration
(1) Make sure that the aircraft and the fuel tanker/pump unit are grounded correctly (Ref. AMM TASK 12-34-24-869-001).
(3) Remove the refuel/defuel coupling-cap 101QM(41QM).
(4) Make sure that the hose-coupling of the fuel tanker/pump unit is clean.
(5) Connect the hose-coupling of the fuel tanker/pump unit to the aircraft refuel/defuel coupling.
(6) Set the fuel tanker/pump unit to the refuel mode.
(7) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(8) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
(9) On the ECAM CP, push (in) the FUEL system page pushbutton switch. Make sure that the FUEL page is shown on the ECAM lower DU.
4. Procedure(1) Make sure that the aircraft and the fuel tanker/pump unit are grounded correctly (Ref. AMM TASK 12-34-24-869-001).
NOTE: Bonding is mandatory. For grounding you must obey the local area regulations.
(2) Make sure that the chocks do not touch the tires. The weight of the fuel can lower the aircraft and cause the chocks to catch. (3) Remove the refuel/defuel coupling-cap 101QM(41QM).
(4) Make sure that the hose-coupling of the fuel tanker/pump unit is clean.
(5) Connect the hose-coupling of the fuel tanker/pump unit to the aircraft refuel/defuel coupling.
(6) Set the fuel tanker/pump unit to the refuel mode.
(7) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(8) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
(9) On the ECAM CP, push (in) the FUEL system page pushbutton switch. Make sure that the FUEL page is shown on the ECAM lower DU.
Subtask 28-25-00-710-063-A ** ON A/C NOT FOR ALL
A. Preparation for Refuel
(1) Do this test:
Subtask 28-25-00-710-083-B ** ON A/C NOT FOR ALL (1) Do this test:
| ACTION | RESULT |
|---|---|
On the panel 800VU:
| On the panel 800VU:
|
| | On the indicator 6QT:
|
| | On the preselector 5QT:
|
| On the panel 800VU:
|
| | On the indicator 6QT:
|
| | On the preselector 5QT:
|
| On the panel 800VU:
|
|
|
B. Test of the Refuel Panel 800VU and 801VU
Subtask 28-25-00-710-069-B ** ON A/C NOT FOR ALL NOTE: The HI LVL lights of the ACT(s) that are not installed will not come on during this test.
(1) Do this test: | ACTION | RESULT |
|---|---|
| 1.On the panel 800VU: | On the panel 800VU and 801VU: |
|
|
| | On the indicator 6QT:
|
| | On the preselector 5QT:
|
| On the panel 800VU and 801VU:
|
| | On the indicator 6QT:
|
| | On the preselector 5QT:
|
| On the panel 800VU and 801VU:
|
|
|
C. Preparation for Test
Subtask 28-25-00-650-069-A ** ON A/C NOT FOR ALL 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: | On panels 800VU and 801VU: |
|
|
| | On preselector 5QT:
|
| | On indicator 6QT:
|
| On panels 800VU and 801VU:
|
| | On preselector 5QT:
|
| | On indicator 6QT:
|
| On panels 800VU and 801VU:
|
|
|
D. Pressure Refuel with Automatic Control
(1) On the refuel/defuel control panel 800VU:
(5) On the ECAM lower DU:
(a) On the preselector 5QT:
(8) On the refuel/defuel control panel 800VU:
Subtask 28-25-00-650-075-A ** ON A/C NOT FOR ALL (1) On the refuel/defuel control panel 800VU:
- make sure that the REFUEL VALVES switches are in the NORM position.
- put the PRESELECTED rocker switch to the INC position and hold it there
- make sure that the number on the PRESELECTED display increases
- when the PRESELECTED display shows the necessary fuel load, release the PRESELECTED rocker switch.
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.
(4) Start the pump on the fuel tanker/pump unit. (5) On the ECAM lower DU:
- make sure that the fuel quantities increase.
(a) On the preselector 5QT:
- the END light comes on
- the numbers on the ACTUAL and the PRESELECTED displays are stable and the same +/- 100 kg (220.4622 lb).
NOTE: When the wing tanks are not full, the difference in tank quantities must be no more than 100 kg (220.4622 lb).
(b) On the ECAM lower DU: - make sure that the fuel quantities are correct.
- if the tanks are full, the HI LVL lights come on.
NOTE: Refer to the fuel tables for the maximum capacity of each tank and for the total fuel capacity (Ref. AMM TASK 12-11-28-650-007).
(7) Stop the pump on the fuel tanker/pump-unit. (8) On the refuel/defuel control panel 800VU:
- put the MODE SELECT switch to the OFF and guarded position.
E. Pressure Refuel with Automatic Control
(1) On the refuel/defuel control panel 800VU and 801VU:
(5) On the ECAM lower DU:
(a) On the preselector 5QT:
(8) On the refuel/defuel control panel 800VU:
Subtask 28-25-00-650-076-B ** ON A/C NOT FOR ALL (1) On the refuel/defuel control panel 800VU and 801VU:
- make sure that the REFUEL VALVES switches are in the NORM position.
- put the PRESELECTED rocker switch to the INC position and hold it there
- make sure that the number on the PRESELECTED display increases
- when the PRESELECTED display shows the necessary fuel load, release the PRESELECTED rocker switch.
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.
(4) Start the pump on the fuel tanker/pump unit. (5) On the ECAM lower DU:
- make sure that the fuel quantities increase.
(a) On the preselector 5QT:
- the END light comes on
- the numbers on the ACTUAL and the PRESELECTED displays are stable and the same +/- 100 kg (220.4622 lb).
- make sure that the fuel quantities are correct.
- if the tanks are full, the HI LVL lights come on.
NOTE: Refer to the fuel tables for the maximum capacity of each tank and for the total fuel capacity (Ref. AMM TASK 12-11-28-650-007).
(7) Stop the pump on the fuel tanker/pump-unit. (8) On the refuel/defuel control panel 800VU:
- put the MODE SELECT switch to the OFF and guarded position.
F. Pressure Refuel with Automatic Control
(1) For the maximum capacity of each tank and for the total fuel capacity, refer to the fuel tables in Para. Description (Ref. AMM D/O 28-11-00-00).
(2) On refuel/defuel control panels 800VU and 801VU:
(6) On the ECAM lower DU:
(a) On preselector 5QT:
(10) On refuel/defuel control panel 800VU:
Subtask 28-25-00-650-081-A ** ON A/C NOT FOR ALL (1) For the maximum capacity of each tank and for the total fuel capacity, refer to the fuel tables in Para. Description (Ref. AMM D/O 28-11-00-00).
(2) On refuel/defuel control panels 800VU and 801VU:
- Make sure that the REFUEL VALVE(S) switches are in the NORM position.
- Put the PRESELECTED switch to the INC position and hold it there.
- Make sure that the number on the PRESELECTED display increases.
- When the PRESELECTED display shows the necessary fuel load, release the PRESELECTED switch.
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) Start the pump on the fuel tanker/pump unit. (6) On the ECAM lower DU:
- Make sure that the fuel quantities for the main fuel tanks and ACT(s) increase.
(a) On preselector 5QT:
- The END light comes on.
- The numbers on the ACTUAL and the PRESELECTED displays are stable and the same +/- 100 kg (220.4622 lb).
- Make sure that the fuel quantities are correct.
- If the tanks are full, the HI LVL lights come on.
(10) On refuel/defuel control panel 800VU:
- Put the MODE SELECT switch to the OFF and guarded position.
G. Pressure Refuel with Manual Control
(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.
(c) Put the MODE SELECT switch to the REFUEL position.
(3) On the ECAM lower DU:
(a) Make sure that the fuel quantities increase.
(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:
Subtask 28-25-00-650-082-A ** ON A/C NOT FOR ALL NOTE: Two persons are necessary for this procedure. One at the refuel panel to control the refueling and one in the cockpit to monitor the fuel quantities. They must be able to speak to each other.
(1) On the refuel/defuel control panel 800VU: (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.
(c) Put the MODE SELECT switch to the REFUEL position.
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.
(2) Start the pump on the fuel tanker/pump unit. (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. AMM 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.
H. Pressure Refuel with Manual Control
(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.
(c) Put the MODE SELECT switch to the REFUEL position.
(3) On the ECAM lower DU:
(a) Make sure that the fuel quantities increase.
(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 and 801VU:
(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:
Subtask 28-25-00-650-083-B ** ON A/C NOT FOR ALL NOTE: Two persons are necessary for this procedure. One at the refuel panel to control the refueling and one in the cockpit to monitor the fuel quantities. They must be able to speak to each other.
(1) 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.
(c) Put the MODE SELECT switch to the REFUEL position.
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.
(2) Start the pump on the fuel tanker/pump unit. (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. AMM 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 and 801VU:
(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.
I. Pressure Refuel with Manual Control
(2) On refuel/defuel control panels 800VU and 801VU:
(a) Put the REFUEL VALVE(S) switch(es) of the applicable fuel tank(s) to the OPEN position.
(b) Put the REFUEL VALVE(S) switch(es) of the tank(s) which will not be refueled to the SHUT position.
(c) Put the MODE SELECT switch to the REFUEL position.
(4) On the ECAM lower DU:
(6) When the fuel tank quantities are correct stop the pump on the fuel tanker/pump unit.
(7) On refuel/defuel control panels 800VU and 801VU:
(a) Put the MODE SELECT switch to the OFF and guarded position.
(b) Put the applicable REFUEL VALVE(S) switch(es) to the NORM and guarded position.
(8) On the ECAM lower DU:
5. Close-upNOTE: Two persons are necessary for this procedure. One at the refuel panel to control the refuel procedure and one in the cockpit to monitor the fuel quantities.
(1) For the maximum capacity of each tank and for the total fuel capacity, refer to the fuel tables in Para. Description (Ref. AMM D/O 28-11-00-00). (2) On refuel/defuel control panels 800VU and 801VU:
(a) Put the REFUEL VALVE(S) switch(es) of the applicable fuel tank(s) to the OPEN position.
(b) Put the REFUEL VALVE(S) switch(es) of the tank(s) which will not be refueled to the SHUT position.
(c) Put the MODE SELECT switch to the REFUEL position.
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.
(3) Start the pump on the fuel tanker/pump unit. (4) On the ECAM lower DU:
- Make sure that the fuel quantities for the main fuel tanks and/or ACT(s) increase.
(6) When the fuel tank quantities are correct stop the pump on the fuel tanker/pump unit.
(7) On refuel/defuel control panels 800VU and 801VU:
(a) Put the MODE SELECT switch to the OFF and guarded position.
(b) Put the applicable REFUEL VALVE(S) switch(es) to the NORM and guarded position.
(8) On the ECAM lower DU:
- Make sure that the fuel quantities for the main fuel tanks and ACT(s) are correct.
Subtask 28-25-00-860-068-A
A. Aircraft Maintenance Configuration
(1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(3) Make an applicable entry in the aircraft technical log.
Subtask 28-25-00-410-073-A ** ON A/C NOT FOR ALL (1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(3) Make an applicable entry in the aircraft technical log.
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Disconnect the hose coupling of the fuel tanker/pump unit at aircraft refuel/defuel coupling 40QM.
(4) Disconnect these bonding/ground cables:
(6) Close access door 192MB.
Subtask 28-25-00-410-073-B ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Disconnect the hose coupling of the fuel tanker/pump unit at aircraft refuel/defuel coupling 40QM.
CAUTION:
MAKE SURE THAT THE HANDLE OF THE REFUEL COUPLING CAP POINTS AFT WHEN THE CAP IS CLOSED AND LOCKED.
(3) Install refuel/defuel coupling cap 41QM on applicable refuel/defuel coupling 40QM. (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.
(6) Close access door 192MB.
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Disconnect the hose coupling of the fuel tanker at the aircraft refuel/defuel coupling.
(3) Install the refuel/defuel coupling-cap on the applicable refuel/defuel coupling.
(4) Disconnect these bonding/ground cables:
Subtask 28-25-00-942-080-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) Disconnect the hose coupling of the fuel tanker at the aircraft refuel/defuel coupling.
(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.
C. Removal of Equipment
(1) If installed, remove the safety barriers.
(2) Remove the access platform(s).
(3) Remove the WARNING NOTICE(S).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) If installed, remove the safety barriers.
(2) Remove the access platform(s).
(3) Remove the WARNING NOTICE(S).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
Refuel/Defuel Control Panel