Operational Test of the Suction and the Air Release Valves
TASK 28-21-00-710-004-A
Operational Test of the Suction and the Air Release Valves
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 28-21-00-941-073-A
Subtask 28-21-00-710-057-A
Subtask 28-21-00-860-058-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:17:23 UTC
Operational Test of the Suction and the Air Release Valves
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.
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | SAFETY BARRIER(S) |
| 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 28-21-00-710-006-A | Operational Test of the Fuel Flow through the Fuel Pumps with Gravity Feed |
| 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 71-00-00-710-003-A | Engine Automatic Start |
| TASK 71-00-00-710-003-B | Engine Automatic Start |
| TASK 71-00-00-710-018-A | Discontinued Start, Restart and Shutdown Procedures |
| TASK 71-00-00-710-028-A | Engine Shutdown |
| TASK 71-00-00-710-028-B | Engine Shutdown |
| TASK 71-00-00-710-043-A | Normal Engine Automatic-Start Procedure |
Subtask 28-21-00-941-073-A
A. Safety Precautions
(1) Put the SAFETY BARRIER(S) in position.
Subtask 28-21-00-860-057-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) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
(3) On the ECAM control panel (CP), push (in) the FUEL P/BSW:
Subtask 28-21-00-860-057-B ** ON A/C NOT FOR ALL (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).
(3) On the ECAM control panel (CP), push (in) the FUEL P/BSW:
- make sure that the FUEL page shows on the ECAM lower Display Unit (DU).
- a minimum of 2000 kg (4409 lb) and maximum 3000 kg (6614 lb) of fuel in each wing tank.
B. Aircraft Maintenance Configuration
(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).
(3) On the ECAM control panel (CP), push (in) the FUEL P/BSW:
Subtask 28-21-00-860-057-C ** ON A/C NOT FOR ALL (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).
(3) On the ECAM control panel (CP), push (in) the FUEL P/BSW:
- make sure that the FUEL page shows on the ECAM lower Display Unit (DU).
- a minimum of 2000 kg (4409 lb) and maximum 3000 kg (6614 lb) of fuel in each wing tank.
B. Aircraft Maintenance Configuration
(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).
(3) On the ECAM control panel (CP), push (in) the FUEL P/BSW:
4. Procedure(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).
(3) On the ECAM control panel (CP), push (in) the FUEL P/BSW:
- make sure that the FUEL page shows on the ECAM lower Display Unit (DU).
- a minimum of 2000 kg (4409 lb) and maximum 3000 kg (6614 lb) of fuel in each wing tank.
Subtask 28-21-00-710-057-A
A. Operational Test of the Suction and the Air Release Valves
(1) Do the Operational Test of the Fuel Flow through the Fuel Pumps with Gravity Feed (Ref. AMM TASK 28-21-00-710-006).
5. Close-up(1) Do the Operational Test of the Fuel Flow through the Fuel Pumps with Gravity Feed (Ref. AMM TASK 28-21-00-710-006).
Subtask 28-21-00-860-058-A ** ON A/C NOT FOR ALL
A. Aircraft Configuration
(1) Shutdown the engines (Ref. AMM TASK 71-00-00-710-028).
(2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Subtask 28-21-00-860-058-B ** ON A/C NOT FOR ALL (1) Shutdown the engines (Ref. AMM TASK 71-00-00-710-028).
(2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
A. Aircraft Configuration
(1) Shutdown the engines (Ref. AMM TASK 71-00-00-710-018).
(2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Subtask 28-21-00-860-058-C ** ON A/C NOT FOR ALL (1) Shutdown the engines (Ref. AMM TASK 71-00-00-710-018).
(2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
A. Aircraft Configuration
(1) Shutdown the engines (Ref. AMM TASK 71-00-00-710-028).
(2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Subtask 28-21-00-942-078-A (1) Shutdown the engines (Ref. AMM TASK 71-00-00-710-028).
(2) 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 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 ground support and maintenance equipment, the special and standard tools and all other items.