Operational Test of the Main Fuel-Pump System with Fuel Flow by Transfer
TASK 28-21-00-710-007-A
Operational Test of the Main Fuel-Pump System with Fuel Flow by Transfer
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 28-21-00-941-068-A
Subtask 28-21-00-860-063-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:46:28 UTC
Operational Test of the Main Fuel-Pump System with Fuel Flow by Transfer
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.
ZONE: 211
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 4M (13 FT)-ADJUSTABLE |
| No specific | AR | SAFETY BARRIER(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 211 | COCKPIT |
| 622KB | |
| 192MB |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 12-11-28-650-003-A | Pressure Refuel with Automatic Control |
| 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 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
Subtask 28-21-00-941-068-A
A. Safety Precautions
(1) Put the SAFETY BARRIER(S) in position.
Subtask 28-21-00-860-064-A (1) Put the SAFETY BARRIER(S) in position.
B. Aircraft Maintenance Configuration
(2) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001), then:
Subtask 28-21-00-010-054-A ** ON A/C NOT FOR ALL WARNING:
MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS.
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002). (2) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001), then:
- on the ECAM control panel (CP), push (in) the FUEL pushbutton switch (P/BSW)
- make sure that the FUEL page shows on the ECAM lower Display Unit (DU).
C. Get Access
(1) Open the access door 192MB.
Subtask 28-21-00-010-054-B ** ON A/C NOT FOR ALL (1) Open the access door 192MB.
NOTE: If operating in battery power, do not keep the door open longer than necessary because the battery can discharge.
C. Get Access
(1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below zone 622.
(2) Open the access door 622KB.
Subtask 28-21-00-860-065-A (1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position below zone 622.
(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.
D. Preparation For Test
(1) On the panel 800VU:
4. Procedure(1) On the panel 800VU:
- put the MODE SELECT switch to the DEFUEL/XFR position.
- push (in) the X-FEED pushbutton switch (P/BSW).
WARNING:
WHEN YOU OPERATE THE FUEL PUMPS DURING A MAINTENANCE PROCEDURE, A MAINTENANCE PERSON MUST BE IN THE COCKPIT. THIS PERSON MUST STOP THE PUMPS WHEN THE LOW PRESSURE FAULT LIGHT(S) (ON PANEL 40VU) COME ON, TO PREVENT OPERATION OF THE PUMPS(S) WITHOUT FUEL ('DRY RUNNING'). OPERATION OF THE PUMPS WITHOUT FUEL CAN CAUSE A FIRE.
Subtask 28-21-00-710-058-A A. Operational Test of the Main Fuel-Pump System with Fuel Flow by Transfer (Wing Tank Pumps)
Subtask 28-21-00-710-059-A ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
| 1.On the panel 40VU: | On the panel 40VU: |
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| 2.On the panel 800VU: | |
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| 3.On the panel 40VU: | |
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| | On the ECAM lower DU: |
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| 4.On the panel 40VU: | On the panel 40VU: |
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| | On the ECAM lower DU: |
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| 5.On the panel 800VU: | |
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| 6.On the panel 40VU: | On the panel 40VU: |
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| | On the ECAM lower DU: |
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| On the panel 40VU: |
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| | On the ECAM lower DU: |
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B. Operational Test of the Main Fuel-Pump System with Fuel Flow by Transfer (Center Tank Pumps)
5. Close-up| ACTION | RESULT |
|---|---|
| 1.On the panel 800VU: | |
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| 2.On the panel 40VU: | On the panel 40VU: |
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| | On the ECAM lower DU: |
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| On the panel 40VU: |
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| | On the ECAM lower DU: |
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| 3.On the panel 800VU: | |
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| 4.On the panel 40VU: | On the panel 40VU: |
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| | On the ECAM lower DU: |
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| On the panel 40VU: |
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| | On the ECAM lower DU: |
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| 5.On the panel 40VU: | On the panel 40VU: |
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| | On the ECAM lower DU: |
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| On the panel 40VU: |
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| | On the ECAM lower DU: |
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Subtask 28-21-00-860-063-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(2) On refuel/defuel control-panel 800VU:
(4) Close access door 192MB.
(5) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(6) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
Subtask 28-21-00-860-063-B ** 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.
(1) In the cockpit, on fuel panel 40VU, release the X-FEED pushbutton switch.(2) On refuel/defuel control-panel 800VU:
- Put the REFUEL VALVE switches to the NORM position
- Put the MODE SELECT switch to the OFF position.
(4) Close access door 192MB.
(5) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(6) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
A. Aircraft Maintenance Configuration
(2) On refuel/defuel control-panel 800VU:
(4) Close access door 622KB.
(5) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(6) In the cockpit, on the ECAM CP, put the BRT switches to the OFF position.
(7) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
Subtask 28-21-00-942-070-A 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.
(1) In the cockpit, on fuel panel 40VU, release the X-FEED pushbutton switch.(2) On refuel/defuel control-panel 800VU:
- Put the REFUEL VALVE switches to the NORM position
- Put the MODE SELECT switch to the OFF position.
(4) Close access door 622KB.
(5) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(6) In the cockpit, on the ECAM CP, put the BRT switches to the OFF position.
(7) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
B. Removal of Equipment
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the safety barriers.
(3) Remove the access platform(s).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the safety barriers.
(3) Remove the access platform(s).
(4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.