Operational Test of the Aileron and Hydraulic Actuation
TASK 27-14-00-710-001-A
Operational Test of the Aileron and Hydraulic Actuation
Self explanatory
2. Job Set-up Information
A. Work Zones and Access Panels
B. Referenced Information
3. Job Set-up
Subtask 27-14-00-861-051-A Subtask 27-14-00-865-051-A
Subtask 27-14-00-710-050-A
Subtask 27-14-00-860-061-A
[Rev.10 from 2021]
2026.03.31 23:47:21 UTC
Operational Test of the Aileron and Hydraulic Actuation
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 TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
ZONE: 210
1. Reason for the JobSelf 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 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 29-10-00-863-003-A | Pressurize the Blue Hydraulic System with a Hydraulic Ground Power-Cart |
| TASK 29-10-00-863-003-A-01 | Pressurize the Blue Hydraulic System with the Blue Electric Pump |
| TASK 29-10-00-864-003-A | Depressurize the Blue Hydraulic System |
| TASK 29-23-00-863-001-A | Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump |
| TASK 29-23-00-864-001-A | Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU |
| TASK 31-60-00-860-001-A | EIS Start Procedure |
| TASK 31-60-00-860-002-A | EIS Stop Procedure |
Subtask 27-14-00-861-051-A Subtask 27-14-00-865-051-A
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 27-14-00-860-062-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B11 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B06 |
| ** ON A/C ALL | |||
| 121VU | FLIGHT CONTROLS/ELAC2/NORM/SPLY | 15CE2 | R20 |
C. Aircraft Maintenance Configuration
(1) On the center pedestal, make sure that the flap and slat control lever is in the 0 position.
(2) On the center pedestal, make sure that the speedbrake control lever is in the RET position.
(3) Make sure that the two side sticks are in the neutral position and that there is no priority on the side stick used.
(4) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001).
(5) Pressurize the Green hydraulic system (Ref. AMM TASK 29-23-00-863-001).
(6) On the FLT CTL section of the overhead panel 23VU, make sure that:
4. Procedure(1) On the center pedestal, make sure that the flap and slat control lever is in the 0 position.
(2) On the center pedestal, make sure that the speedbrake control lever is in the RET position.
(3) Make sure that the two side sticks are in the neutral position and that there is no priority on the side stick used.
(4) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001).
(5) Pressurize the Green hydraulic system (Ref. AMM TASK 29-23-00-863-001).
(6) On the FLT CTL section of the overhead panel 23VU, make sure that:
- The ELAC 1 pushbutton switch is pushed (on this pushbutton switch, the FAULT and OFF legends are off).
- The ELAC 2 pushbutton switch is pushed (on this pushbutton switch, the FAULT and OFF legends are off).
- The HYD/LEAK MEASUREMENT VALVES/B and G pushbutton switches are pushed (on these pushbutton switches the OFF legends are OFF).
Subtask 27-14-00-710-050-A
A. Do this test:
5. Close-up| ACTION | RESULT |
|---|---|
1.On the center pedestal, on the ECAM control panel:
| On the center instrument panel, on the lower ECAM DU:
|
| 2.Move one of the two side sticks to the left until it touches the stop. | On the L/AIL position indicator:
|
| | On the R/AIL position indicator:
|
| 3.Move the side stick to the right until it touches the stop. | On the L/AIL position indicator:
|
| | On the R/AIL position indicator:
|
| 4.Put the side stick in the neutral position. | On the L/AIL and R/AIL position indicators:
|
| 5.Depressurize the Green hydraulic system (Ref. AMM TASK 29-23-00-864-001). | |
| 6.Pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003). | |
| 7.Move one of the two side sticks to the left until it touches the stop. | On the L/AIL position indicator:
|
| | On the R/AIL position indicator:
|
| 8.Move the side stick to the right until it touches the stop. | On the L/AIL position indicator:
|
| | On the R/AIL position indicator:
|
| 9.Put the side stick in the neutral position. | On the L/AIL and R/AIL position indicators:
|
Subtask 27-14-00-860-061-A
A. Aircraft Maintenance Configuration
(1) Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
(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) Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
(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).