Functional Check of Blue Electrical Pump Pressure by Reading ECAM Indication
TASK 29-12-00-710-001-A
Functional Check of Blue Electrical Pump Pressure by Reading ECAM Indication
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Work Zones and Access Panels
B. Referenced Information
3. Job Set-up
Subtask 29-12-00-865-050-A
Subtask 29-12-00-710-050-A
5. Close-up
Subtask 29-12-00-860-051-A
[Rev.10 from 2021]
2026.04.01 05:46:39 UTC
Functional Check of Blue Electrical Pump Pressure by Reading ECAM Indication
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Work Zones and Access Panels
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 210 | CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 12-12-29-611-001-A | Fill the Hydraulic Fluid Reservoir with a Hand Pump |
| 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 29-14-00-614-002-A | Pressurization of the Hydraulic Reservoirs through the Ground Connector |
| TASK 29-14-00-614-002-A-01 | Pressurization of the Hydraulic Reservoirs with the Auxiliary Power Unit (APU) |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
Subtask 29-12-00-865-050-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 29-12-00-860-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| 49VU | HYD/HYD PWR/B WARN/& CTL | 2702GJ | C12 |
| 123VU | B HYD/ELEC PUMP | 2701GJ | AB09 |
B. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(3) On the ECAM control panel on the center pedestal, push the HYD pushbutton. Make sure that the ECAM lower Display Unit (DU) shows the HYD page.
(4) On the panel 24VU, make sure that the ELAC 2 pushbutton switch (P/BSW) is set to ON (OFF and FAULT lights off).
(5) On the panel 23VU, make sure that the ELAC 1 and SEC 1 P/BSW are set to ON (OFF and FAULT lights off).
(6) Make sure that the ECAM does not show any of these conditions:
(8) If necessary. add fluid to the reservoir (Ref. AMM TASK 12-12-29-611-001).
(9) On the panel 40VU, make sure that the BLUE ELEC PUMP P/BSW is set to AUTO (OFF and FAULT lights off).
4. Procedure(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(3) On the ECAM control panel on the center pedestal, push the HYD pushbutton. Make sure that the ECAM lower Display Unit (DU) shows the HYD page.
(4) On the panel 24VU, make sure that the ELAC 2 pushbutton switch (P/BSW) is set to ON (OFF and FAULT lights off).
(5) On the panel 23VU, make sure that the ELAC 1 and SEC 1 P/BSW are set to ON (OFF and FAULT lights off).
(6) Make sure that the ECAM does not show any of these conditions:
- Low air pressure in the Blue reservoir,
- Low fluid level in the Blue reservoir.
(8) If necessary. add fluid to the reservoir (Ref. AMM TASK 12-12-29-611-001).
(9) On the panel 40VU, make sure that the BLUE ELEC PUMP P/BSW is set to AUTO (OFF and FAULT lights off).
Subtask 29-12-00-710-050-A
WARNING:
MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
WARNING:
MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
A. Do this test: | ACTION | RESULT |
|---|---|
1.On the panel 50VU:
| On the panel 50VU:
|
| | The electric pump of the Blue hydraulic system starts. |
| | On the ECAM lower DU:
|
| 2.Operate the ailerons, the elevators and the rudder. | On the ECAM lower DU:
|
| 3.Stop the operation of the control surfaces. | On the ECAM lower DU:
|
| 4.On the panel 40VU: | |
| On the panel 40VU:
|
| | The electric pump of the Blue hydraulic system stops. |
Subtask 29-12-00-860-051-A
A. Put the aircraft back to its initial configuration.
(1) On the panel 40VU, push and release the BLUE ELEC PUMP P/BSW. Make sure that the OFF and FAULT lights are not on.
(2) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(3) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(1) On the panel 40VU, push and release the BLUE ELEC PUMP P/BSW. Make sure that the OFF and FAULT lights are not on.
(2) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(3) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).