Operational Test of the Center-Tank Pump Control
TASK 28-21-00-710-010-A
Operational Test of the Center-Tank Pump Control
To test the Center Tank Pump Control by the Full/Under-full Level Sensors and the FLSCUs Logic 2.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 28-21-00-941-077-A ** ON A/C NOT FOR ALL
Subtask 28-21-00-860-072-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 00:04:20 UTC
Operational Test of the Center-Tank Pump Control
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
1. Reason for the Job- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
To test the Center Tank Pump Control by the Full/Under-full Level Sensors and the FLSCUs Logic 2.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | SAFETY BARRIER(S) |
| 98D27803500001 | 1 | LOCKING TOOL ZERO POS |
| 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 27-80-00-866-005-A | Retracting the Slats on the Ground |
| 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 28-21-00-941-077-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(1) Put the SAFETY BARRIER(S) in position.
Subtask 28-21-00-860-071-A ** ON A/C NOT FOR ALL (1) Put the SAFETY BARRIER(S) in position.
B. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the slats are fully retracted (Ref. AMM TASK 27-80-00-866-005).
(3) Make sure that the 98D27803500001 LOCKING TOOL ZERO POS is on the slat/flap control lever.
(4) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001), then:
Subtask 28-21-00-865-061-A ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the slats are fully retracted (Ref. AMM TASK 27-80-00-866-005).
(3) Make sure that the 98D27803500001 LOCKING TOOL ZERO POS is on the slat/flap control lever.
(4) 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 push icon switch
- make sure that the FUEL page shows on the ECAM lower Display Unit (DU).
- the center tank contains more than 500 kg (1102 lb)
- the applicable wing-tank outer-cell full
- the applicable wing-tank inner-cell contains between 5000 kg (11023 lb) and 5500 kg (12125 lb).
NOTE: Make sure that the fuel in the center tank is kept above 500 kg (1102 lb) during the test procedure.
C. Make sure that this(these) circuit breaker(s) is(are) closed:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FUEL/FQI/CHAN/1 | 1QT | A13 |
| 121VU | FUEL/FQI/CHAN/2 | 2QT | M27 |
| 121VU | FUEL/CTR TK/PUMP2 SPLY | 30QA | P26 |
| 121VU | FUEL/CTR TK/PUMP1 SPLY | 29QA | P23 |
| 121VU | FUEL/CTR TK/AUTO/CTL | 47QA | R27 |
| 121VU | FUEL/CTR TK/PUMPS1 AND 2/CTL AND IND | 32QA | R26 |
| 121VU | FUEL/CTR TK/PUMPS1 AND 2/CTL AND IND | 31QA | R25 |
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 28-21-00-710-069-A ** ON A/C NOT FOR ALL A. Operational Test of the Center-Tank Pump Control by the Full/Under-full Level Sensors and FLSCUs Logic 2
5. Close-up| ACTION | RESULT |
|---|---|
| For the left side pump control test, do the procedure that follows: | |
1.On fuel control-panel 40VU:
| On fuel control-panel 40VU:
|
2.On refuel/defuel control-panel 800VU:
| On refuel/defuel control-panel 800VU:
|
| 3.Monitor fuel quantity-indicator 6QT. |
|
4.On refuel/defuel control-panel 800VU:
|
|
5.Monitor fuel quantity-indicator 6QT:
|
|
| On the ECAM lower DU:
NOTE: If the center tank pump operates for more than 45 seconds, you can stop the test and troubleshoot the system (Ref. TSM Chapter 28). (This is to prevent a possible fuel spill from the left wing NACA vent). |
|
|
6.On refuel/defuel control-panel 800VU:
| |
7.On fuel control-panel 40VU:
|
|
| 8.Monitor fuel quantity-indicator 6QT. |
|
| 9.Monitor fuel quantity-indicator 6QT, until approximately 400 kg (882 lb) of fuel used. | On the ECAM lower DU:
|
10.On fuel control-panel 40VU:
|
|
11.On refuel/defuel control-panel 800VU:
| |
| For the right side pump control test, do the procedure that follows: | |
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. 12.On fuel control-panel 40VU:
|
|
13.On refuel/defuel control-panel 800VU:
|
|
| 14.Monitor fuel quantity-indicator 6QT. |
|
| 15.On refuel/defuel control-panel 800VU. |
|
16.On refuel/defuel control-Panel 800VU:
|
|
17.Monitor fuel quantity-indicator 6QT:
|
|
| On the ECAM lower DU:
NOTE: If the center tank pump operates for more than 45 seconds, you can stop the test and troubleshoot the system (Ref. TSM Chapter 28). (This is to prevent a possible fuel spill from the left wing NACA vent). |
|
|
18.On refuel/defuel control-panel 800VU:
| |
19.On fuel control-panel 40VU:
|
|
| 20.Monitor fuel quantity-indicator 6QT. |
|
| 21.Monitor fuel quantity-indicator 6QT, until approximately 400 kg (882 lb) of fuel used. | On the ECAM lower DU:
|
22.On fuel control-panel 40VU:
| On fuel control-panel 40VU:
|
23.On refuel/defuel control-panel 800VU:
| On refuel/defuel control-panel 800VU:
|
24.On fuel control-panel 40VU:
| On fuel control-panel 40VU:
|
Subtask 28-21-00-860-072-A ** ON A/C NOT FOR ALL
A. Aircraft Configuration
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Refuel, defuel or transfer fuel as necessary (Ref. AMM TASK 12-11-28-650-003), (Ref. AMM TASK 28-25-00-650-001) or (Ref. AMM TASK 28-25-00-869-001).
(3) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(4) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Subtask 28-21-00-942-081-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Refuel, defuel or transfer fuel as necessary (Ref. AMM TASK 12-11-28-650-003), (Ref. AMM TASK 28-25-00-650-001) or (Ref. AMM TASK 28-25-00-869-001).
(3) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(4) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
B. Removal of Equipment
(1) Remove the safety barriers.
(2) Remove the 98D27803500001 LOCKING TOOL ZERO POS from the flap/slat control lever.
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Remove the safety barriers.
(2) Remove the 98D27803500001 LOCKING TOOL ZERO POS from the flap/slat control lever.
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.