Operational Test of the Refuel System
TASK 28-25-00-710-003-A
Operational Test of the Refuel System
Self Explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 28-25-00-941-074-A
Subtask 28-25-00-710-054-C ** ON A/C NOT FOR ALL
Subtask 28-25-00-860-058-A
[Rev.10 from 2021]
2026.04.01 07:16:30 UTC
Operational Test of the Refuel System
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:
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.
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 WHEEL CHOCKS ARE IN POSITION. MOVEMENT OF THE AIRCRAFT CAN BE DANGEROUS.
1. Reason for the JobSelf Explanatory
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) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 190 | BELLY FAIR, AIR CONDITIONING & HYD COMPT |
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| 500 | LEFT WING |
| 600 | RIGHT WING |
| 622KB | |
| 192MB |
| 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 12-34-24-869-001-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 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 |
Subtask 28-25-00-941-074-A
A. Safety Precautions
(2) You must obey the refuel/defuel safety procedures (Ref. AMM TASK 12-11-28-650-001) (Ref. AMM TASK 12-11-28-650-002) when you do work on the refuel/defuel system.
(3) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
Subtask 28-25-00-010-059-A ** ON A/C NOT FOR ALL WARNING:
OBEY THE FUEL SAFETY PROCEDURES.
(1) You must obey the fuel safety procedures when you do work on the fuel system (Ref. AMM TASK 28-00-00-910-001). (2) You must obey the refuel/defuel safety procedures (Ref. AMM TASK 12-11-28-650-001) (Ref. AMM TASK 12-11-28-650-002) when you do work on the refuel/defuel system.
(3) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
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.
Subtask 28-25-00-010-059-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.
B. Get Access
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position below the applicable access panel 622KB.
(2) Open the access door 622KB.
Subtask 28-25-00-860-057-A ** ON A/C NOT FOR ALL (1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position below the applicable access panel 622KB.
(2) Open the access door 622KB.
NOTE: If operating in battery power, do not keep the door open longer than necessary because the battery can discharge.
C. Aircraft Maintenance Configuration
(1) Make sure that the fuel tanker is in the correct position.
(a) Ground (earth) the fuel tanker/pump unit and the aircraft correctly (Ref. AMM TASK 12-34-24-869-001).
(3) Bond the fuel tanker/pump unit to the aircraft (Ref. AMM TASK 12-34-24-869-001).
(4) Remove refuel coupling cap 41QM.
(5) Make sure that the hose coupling of the fuel tanker/pump unit is clean.
(6) Connect the hose coupling of the fuel tanker/pump unit to the aircraft refuel/defuel coupling.
(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) Energize the Electronic Centralized Aircraft Monitoring (ECAM) system (Ref. AMM TASK 31-60-00-860-001).
(10) On the ECAM CP, push (in) the FUEL system page pushbutton switch.
Subtask 28-25-00-860-057-B ** ON A/C NOT FOR ALL (1) Make sure that the fuel tanker is in the correct position.
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.
(2) 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).
(3) Bond the fuel tanker/pump unit to the aircraft (Ref. AMM TASK 12-34-24-869-001).
(4) Remove refuel coupling cap 41QM.
(5) Make sure that the hose coupling of the fuel tanker/pump unit is clean.
(6) Connect the hose coupling of the fuel tanker/pump unit to the aircraft refuel/defuel coupling.
(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) Energize the Electronic Centralized Aircraft Monitoring (ECAM) system (Ref. AMM TASK 31-60-00-860-001).
(10) On the ECAM CP, push (in) the FUEL system page pushbutton switch.
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 applicable refuel 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) Energize the Electronic Centralized Aircraft Monitoring (ECAM) system (Ref. AMM TASK 31-60-00-860-001).
(9) On the ECAM CP, push the FUEL system page pushbutton switch.
Subtask 28-25-00-710-053-A ** ON A/C NOT FOR ALL (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 applicable refuel 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) Energize the Electronic Centralized Aircraft Monitoring (ECAM) system (Ref. AMM TASK 31-60-00-860-001).
(9) On the ECAM CP, push the FUEL system page pushbutton switch.
D. Preparation for Test
(1) Do this test:
Subtask 28-25-00-710-053-C ** ON A/C NOT FOR ALL (1) Do this test:
| ACTION | RESULT |
|---|---|
1.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:
|
|
|
2.On the ECAM control panel (CP):
| On the ECAM lower display-unit:
|
| On the STATUS page:
|
D. Preparation for Test (If an ACT is Installed)
(1) Do this test:
Subtask 28-25-00-710-053-D ** ON A/C NOT FOR ALL (1) Do this test:
NOTE: The ACT HI LVL light on panel 801VU will not come on during this test when the ACT is not installed.
| ACTION | RESULT |
|---|---|
1.On panel 800VU:
| On panel 800VU and 801VU:
|
| | On indicator 6QT:
|
| | On preselector 5QT:
|
| On panel 800VU and 801VU:
|
| | On indicator 6QT:
|
| | On preselector 5QT:
|
| On panel 800VU and 801VU:
|
|
|
2.On the ECAM control panel (CP):
| On the ECAM lower display-unit:
|
| On the STATUS page:
|
D. Preparation for Test (If ACT's are Installed)
(1) Do this test:
Subtask 28-25-00-710-076-B ** ON A/C NOT FOR ALL (1) Do this test:
NOTE: The HI LVL lights of the 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:
|
| | 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:
|
|
|
2.On the ECAM control panel (CP):
| On the ECAM lower display-unit:
|
| On the STATUS page:
|
E. Preparation for Test (If ACT's are Installed)
4. ProcedureNOTE: The HI LVL lights of the ACTs that are not installed will not come on during this test.
(1) Do this test: | ACTION | RESULT |
|---|---|
1.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:
|
2.On the ECAM control panel (CP):
| On the ECAM lower display-unit:
|
| On the STATUS page:
|
Subtask 28-25-00-710-054-C ** ON A/C NOT FOR ALL
A. Operational Test of the Refuel System, to the Wing Tank Capacity
(2) Do the test that follows:
Subtask 28-25-00-710-054-D ** ON A/C NOT FOR ALL 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.
(1) Defuel the aircraft so that there is room in all of the tanks (Ref. AMM TASK 28-25-00-650-001). (2) Do the test that follows:
| ACTION | RESULT |
|---|---|
1.On the panel 800VU and 801VU:
| |
| |
2.On the preselector 5QT:
| On the preselector 5QT:
|
|
|
3.On the panel 800VU:
| |
| 4.Start the pump on the fuel tanker/pump unit. | On the indicator 6QT:
|
| | On the preselector 5QT:
|
| | When the fuel is at the set quantity: |
| | On the preselector 5QT:
NOTE: When the wing tanks are not full, the difference in tank quantities will be no more than 200 kg (441 lb). |
5.On the ECAM lower DU:
| |
6.On the panel 800VU:
| On the indicator 6QT:
|
| | On the preselector 5QT:
|
| On the panel 800VU:
|
| | On the preselector 5QT:
NOTE: Each fuel tank will fill to maximum capacity only if the aircraft is level. |
7.On the panel 800VU:
| |
| |
| 8.Stop the pump on the fuel tanker/pump unit. | |
9.On the ECAM lower DU:
| |
A. Operational Test of the Refuel System, to the Wing Tank Capacity
(2) Do the test that follows:
Subtask 28-25-00-710-054-E ** ON A/C NOT FOR ALL 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.
(1) Defuel the aircraft so that there is room in all of the tanks (Ref. AMM TASK 28-25-00-650-001). (2) Do the test that follows:
| ACTION | RESULT |
|---|---|
1.On the panel 800VU and 801VU:
| |
| |
2.On the preselector 5QT:
| On the preselector 5QT:
|
|
|
3.On the panel 800VU:
| |
| 4.Start the pump on the fuel tanker/pump unit. | On the indicator 6QT:
|
| | On the preselector 5QT:
|
| | When the fuel is at the set quantity: |
| | On the preselector 5QT:
NOTE: When the wing tanks are not full, the difference in tank quantities will be no more than 200 kg (441 lb). |
5.On the ECAM lower DU:
| |
| 6.Stop the pump on the fuel tanker/pump unit. | On the indicator 6QT:
|
| | On the preselector 5QT:
|
7.On the panel 51VU:
| On the panel 51VU:
|
| | On the preselector 10QT:
|
| | On the preselector 5QT:
|
| 8.Wait for 30 seconds. | On the panel 51VU:
NOTE: A HI LVL test is done automatically. |
9.On the preselector 10QT:
| On the preselector 10QT:
|
|
|
| | On the preselector 5QT:
|
10.On the panel 51VU:
| On the panel 51VU:
|
| | Adjacent to the refuel/defuel coupling in the wing:
|
| 11.Start the pump on the fuel tanker/pump unit. | On the preselector 10QT:
|
| | When the fuel is at the set quantity: |
| | On the preselector 10QT:
|
| | On the preselector 5QT:
NOTE: When the wing tanks are not full, the difference in the tank quantities will be no more than 200 kg (441 lb). |
| | Adjacent to the refuel/defuel coupling in the wing:
|
12.On the ECAM lower DU:
| |
13.On the panel 51VU:
| On the panel 51VU:
|
| | On the indicator 10QT:
|
| | On the preselector 5QT:
|
14.On the panel 800VU:
| On the indicator 6QT:
|
| | On the preselector 5QT:
|
| On the panel 800VU:
|
| | On the preselector 5QT:
NOTE: Each fuel tank will fill to maximum capacity only if the aircraft is level. |
15.On the panel 800VU:
| |
| |
| 16.Stop the pump on the fuel tanker/pump unit. | |
17.On the ECAM lower DU:
| |
A. Operational Test of the Refuel System, to the Wing Tank Capacity
(2) Do the test that follows:
Subtask 28-25-00-710-055-B ** ON A/C NOT FOR ALL 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.
(1) Defuel the aircraft so that there is room in all of the tanks (Ref. AMM TASK 28-25-00-650-001). (2) Do the test that follows:
| ACTION | RESULT |
|---|---|
1.On the panel 800VU:
| |
| |
2.On the preselector 5QT:
| On the preselector 5QT:
|
|
|
3.On the panel 800VU:
| |
| 4.Start the pump on the fuel tanker/pump unit. | On the indicator 6QT:
|
| | On the preselector 5QT:
|
| | When the fuel is at the set quantity: |
| | On the preselector 5QT:
NOTE: When the wing tanks are not full, the difference in tank quantities will be no more than 200 kg (441 lb). |
5.On the ECAM lower DU:
| |
6.On the panel 800VU:
| On the indicator 6QT:
|
| | On the preselector 5QT:
|
| On the panel 800VU:
|
| | On the preselector 5QT:
NOTE: Each fuel tank will fill to maximum capacity only if the aircraft is level. |
7.On the panel 800VU:
| |
| |
| 8.Stop the pump on the fuel tanker/pump unit. | |
9.On the ECAM lower DU:
| |
B. Operational Test of the Refuel System, to the Wing Tanks and Center Tank Capacity
(1) Defuel the aircraft so that there is room in all of the tanks (Ref. AMM TASK 28-25-00-650-001).
Subtask 28-25-00-710-055-C ** ON A/C NOT FOR ALL (1) Defuel the aircraft so that there is room in all of the tanks (Ref. AMM TASK 28-25-00-650-001).
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.
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) Do the test that follows: | ACTION | RESULT |
|---|---|
1.On REFUEL/DEFUEL Control panel 800VU:
| |
| |
2.On preselector 5QT:
| On preselector 5QT:
|
|
|
3.On REFUEL/DEFUEL control panel 800VU:
| |
| 4.Start the pump on the fuel tanker/pump unit. | On indicator 6QT:
|
| | On preselector 5QT:
|
| | NOTE: Before the wing tanks are full, the CTR FUEL QTY numbers will stop. They will not increase again until the HI LVL LEFT and RIGHT lights come on. |
| | When the fuel is at the set quantity |
| | On preselector 5QT:
|
| | On REFUEL/DEFUEL Control panel 800VU:
|
5.On the ECAM lower DU:
| |
6.On REFUEL/DEFUEL Control panel 800VU:
| On indicator 6QT:
|
| | On preselector 5QT:
|
| On REFUEL/DEFUEL Control panel 800VU:
|
| | On preselector 5QT:
NOTE: Each fuel tank will fill to maximum capacity only if the aircraft is level. |
7.On REFUEL/DEFUEL Control panel 800VU:
| |
| |
| 8.Stop the pump on the fuel tanker/pump unit. | |
9.On the ECAM lower DU:
| |
B. Operational Test of the Refuel System, to the Wing Tank and Center Tank Capacity
(1) Defuel the aircraft so that there is space in all of the tanks (Ref. AMM TASK 28-25-00-650-001).
Subtask 28-25-00-710-068-B ** ON A/C NOT FOR ALL (1) Defuel the aircraft so that there is space in all of the tanks (Ref. AMM TASK 28-25-00-650-001).
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.
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) Do the test that follows: | ACTION | RESULT |
|---|---|
1.On the panel 800VU and 801VU:
| |
| |
2.On preselector 5QT:
| On preselector 5QT:
|
|
|
3.On panel 800VU:
| |
| 4.Start the pump on the fuel tanker/pump unit. | On indicator 6QT:
|
| | On preselector 5QT:
|
| | NOTE: Before the wing tanks are full, the CTR FUEL QTY numbers will stop. They will not increase again until the HI LVL LEFT and RIGHT lights come on. |
| | When the fuel is at the set quantity: |
| | On preselector 5QT:
|
| | On panel 800VU:
|
5.On the ECAM lower DU:
| |
6.On panel 800VU:
| On the indicator 6QT:
|
| | On preselector 5QT:
|
| On panel 800VU:
|
| | On preselector 5QT:
NOTE: Each fuel tank will fill to maximum capacity only if the aircraft is level. |
7.On the panel 800VU:
| |
| |
| 8.Stop the pump on the fuel tanker/pump unit. | |
9.On the ECAM lower DU:
| |
C. Operational Test of the Refuel System, to the Wing Tanks, Center Tank and ACT(s) Capacity.
(1) Make sure that paragraphs 4.A. and 4.B. are done.
(4) Stop the pump on the fuel tanker/pump unit.
(5) On control panel 800VU, put the MODE SELECT switch to the OFF and quarded position.
Subtask 28-25-00-710-073-A ** ON A/C NOT FOR ALL (1) Make sure that paragraphs 4.A. and 4.B. are done.
NOTE: On preselector 5QT, ACTUAL indicator shows value about 18900 kg (41667.3558 lb). On control panel 800VU, LEFT, CTR and RIGHT HI LVL indications are on.
(2) Defuel/transfer the aircrafts fuel so that there is room in the ACT(s) (Ref. AMM TASK 28-25-00-869-001) (Ref. AMM TASK 28-25-00-650-001). 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) Do the test that follows for each installed ACT, according to ACT automatic refuel sequence: NOTE: ACT automatic refuel sequence is ACT1, ACT2 and ACT4.1.
| ACTION | RESULT |
|---|---|
1.On control panel 800VU:
| |
2.On control panels 800VU and 801VU:
| |
On control panel 801VU:
| On indicator 6QT:
NOTE: If the ACT rotary switch is not installed, ACT indicator shows fuel quantity in ACT1. |
3.On preselector 5QT:
| On preselector 5QT:
|
|
|
4.On control panel 800VU:
| |
| 5.Start the pump on the fuel tanker/pump unit. | On indicator 6QT:
|
| | On preselector 5QT:
|
| | When the fuel is at the set quantity: |
| | On preselector 5QT:
|
| | On control panel 800VU:
|
6.On the ECAM lower DU:
| |
7.On control panel 801VU:
| |
| 8.Continue to refuel until the HI LVL light of the tested ACT comes on. | On control panel 801VU:
|
| | On preselector 5QT:
NOTE: Each fuel tank will fill to maximum capacity only if the aircraft is level. |
9.On control panel 801VU:
| |
10.On the ECAM lower DU:
| |
(5) On control panel 800VU, put the MODE SELECT switch to the OFF and quarded position.
D. Operational Test of the Refuel System, to the Wing Tanks, Center Tank and ACT Capacity
(1) Defuel the aircraft so that there is room in all of the tanks (Ref. AMM TASK 28-25-00-650-001).
Subtask 28-25-00-710-073-B ** ON A/C NOT FOR ALL (1) Defuel the aircraft so that there is room in all of the tanks (Ref. AMM TASK 28-25-00-650-001).
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.
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) Do the test that follows: | ACTION | RESULT |
|---|---|
1.On the panel 800VU:
| |
2.On the panels 800VU and 801VU:
| |
| 3.On the preselector 5QT: | On the preselector 5QT: |
|
|
|
|
4.On the panel 800VU:
| |
| 5.Start the pump on the fuel tanker/pump unit. | On the indicator 6QT:
|
| | On the preselector 5QT:
|
| 6.On the panel 801VU: | On the indicator 6QT: |
|
|
| NOTE: Before the wing tanks are full, the CTR FUEL QTY numbers will stop. They will not increase again until the HI LVL LEFT and RIGHT lights come on. |
| | When the fuel is at the set quantity: |
| | On the preselector 5QT:
|
| | On the panel 800VU:
|
7.On the ECAM lower DU:
| |
8.On the panel 801VU:
| |
| 9.Continue to refuel until the HI LVL ACT light comes on. | On the panel 801VU:
|
| | On the preselector 5QT:
NOTE: Each fuel tank will fill to maximum capacity only if the aircraft is level. |
| 10.Stop the pump on the fuel tanker/pump unit. | |
11.On the panel 800VU:
| |
12.On the panel 801VU:
| |
13.On the ECAM lower DU:
| |
D. Operational Test of the Refuel System, to the Wing Tanks, Center Tank, ACT1 and ACT2 Capacity
(1) Defuel the aircraft so that there is room in all of the tanks (Ref. AMM TASK 28-25-00-650-001).
5. Close-up(1) Defuel the aircraft so that there is room in all of the tanks (Ref. AMM TASK 28-25-00-650-001).
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.
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) Do the test that follows: | ACTION | RESULT |
|---|---|
1.On the panel 800VU:
| |
2.On the panels 800VU and 801VU:
| |
| 3.For the ACT1, on the preselector 5QT: | On the preselector 5QT: |
|
|
|
|
4.On the panel 800VU:
| |
| 5.Start the pump on the fuel tanker/pump unit. | On the indicator 6QT:
|
| | On the preselector 5QT:
|
| 6.On the panel 801VU: | On the indicator 6QT: |
|
|
| NOTE: Before the wing tanks are full, the CTR FUEL QTY numbers will stop. They will not increase again until the HI LVL LEFT and RIGHT lights come on. |
| | When the fuel is at the set quantity: |
| | On the preselector 5QT:
|
| | On the panel 800VU:
|
7.On the ECAM lower DU:
| |
8.On the panel 801VU:
| |
| 9.Continue to refuel until the HI LVL ACT1 light comes on. | On the panel 801VU:
|
| | On the preselector 5QT:
NOTE: Each fuel tank will fill to maximum capacity only if the aircraft is level. |
10.On the panel 801VU:
| |
11.On the ECAM lower DU:
| |
| 12.For the ACT2, on the preselector 5QT: | On the preselector 5QT: |
|
|
|
|
| | On the indicator 6QT:
|
| | On the preselector 5QT:
|
| 13.On the panel 801VU: | On the indicator 6QT: |
|
|
| NOTE: Before the wing tanks are full, the CTR FUEL QTY numbers will stop. They will not increase again until the HI LVL LEFT and RIGHT lights come on. |
| | When the fuel is at the set quantity: |
| | On the preselector 5QT:
|
| | On the panel 800VU:
|
| | On the panel 801VU:
|
14.On the ECAM lower DU:
| |
15.On the panel 801VU:
| |
| 16.Continue to refuel until the HI LVL ACT2 light comes on. | On the panel 801VU:
|
| | On the preselector 5QT:
NOTE: Each fuel tank will fill to maximum capacity only if the aircraft is level. |
| 17.Stop the pump on the fuel tanker/pump unit. | |
18.On the panel 800VU:
| |
19.On the panel 801VU:
| |
20.On the ECAM lower DU:
| |
Subtask 28-25-00-860-058-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).
Subtask 28-25-00-410-061-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).
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 aircraft refuel/defuel coupling 40QM.
(3) Install refuel/defuel coupling cap 41QM on refuel/defuel coupling 40QM.
(4) Disconnect these bonding/ground cables:
Subtask 28-25-00-410-061-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 at aircraft refuel/defuel coupling 40QM.
(3) Install refuel/defuel coupling cap 41QM on 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.
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 coupling cap on the applicable refuel/defuel coupling.
(4) Disconnect these bonding/ground cables:
Subtask 28-25-00-942-061-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 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