Integrity Test of the Hydraulic Power

TASK 29-00-00-710-001-A
Integrity Test of the Hydraulic Power

WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.

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.

MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE 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.

WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES.

WARNING: MAKE SURE THAT THE RAT TRAVEL RANGE IS CLEAR BEFORE YOU EXTEND/RETRACT THE RAT.

1. Reason for the Job
To make sure that the hydraulic system is safe after maintenance work on the electrical system.
2. Job Set-up Information
A. Referenced Information

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 29-00-00-870-001-A	Bleeding Procedure of the Green Hydraulic System Upstream of the Engine Pump
TASK 29-00-00-870-002-A	Bleeding Procedure of the Green Hydraulic System Upstream of the PTU
TASK 29-00-00-870-003-A	Bleeding Procedure of the Green Hydraulic System Downstream of the Engine Pump
TASK 29-00-00-870-004-A	Bleeding Procedure of the Yellow Hydraulic System Upstream of the Engine Pump
TASK 29-00-00-870-005-A	Bleeding Procedure of the Yellow Hydraulic System Upstream of the PTU
TASK 29-00-00-870-006-A	Bleeding Procedure of the Yellow Hydraulic System Upstream of the Yellow E-Pump
TASK 29-00-00-870-007-A	Bleeding Procedure of the Yellow Hydraulic System Downstream of the Engine Pump
TASK 29-00-00-870-008-A	Bleeding Procedure of the Blue Hydraulic System Upstream of the Blue E-Pump
TASK 29-00-00-870-009-A	Bleeding Procedure of the Blue Hydraulic System Downstream of the Blue E-Pump
TASK 29-10-00-710-001-A	Operational Check of Hydraulic Fire Shut Off Valves and Associated Indicating System
TASK 29-11-00-710-001-A	Operational Test of the Green Hydraulic System
TASK 29-12-00-710-001-A	Functional Check of Blue Electrical Pump Pressure by Reading ECAM Indication
TASK 29-13-00-710-002-A	Operational Test of the Yellow Hydraulic System
TASK 29-22-00-710-006-A	Operational Check of Ram Air Turbine (RAT) Automatic Deployment
TASK 29-22-00-710-007-A	Operational Test of the Manual Deployment and the Retraction of the Ram Air Turbine
TASK 29-23-00-710-002-A	Functional Check of the Power Transfer Unit (PTU) Green to Yellow
TASK 29-23-00-710-003-A	Functional Check of the Power Transfer Unit (PTU) Yellow to Green
TASK 29-24-00-710-001-A	Operational Test of the Yellow Auxiliary Power
TASK 29-31-00-710-001-A	Functional Check of Reservoir Low Level Warning
TASK 31-50-00-710-003-A	Operational Test of the System Data Acquisition Concentrator (SDAC)
TASK 31-60-00-860-001-A	EIS Start Procedure
TASK 31-60-00-860-002-A	EIS Stop Procedure

3. Job Set-up
Subtask 29-00-00-860-082-A

A. 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, push the HYD key. Make sure that the HYD page comes into view on the ECAM lower DU.

4. Procedure
Subtask 29-00-00-870-067-A

A. Bleeding

NOTE: The subsequent bleeding procedures are only necessary after the replacement of hydraulic components, or opening of the hydraulic system(s).

(1) Do the applicable bleeding procedure for the related hydraulic system:
(a) For the Green hydraulic system:

(b) For the Yellow hydraulic system:

Subtask 29-00-00-710-051-A

B. Do the operational test of the System Data Acquisition Concentrator (SDAC) (Ref. AMM TASK 31-50-00-710-003).

Subtask 29-00-00-710-052-A

C. Operational Tests
(1) Do the operational test of the applicable hydraulic system:

For the Green hydraulic system (Ref. AMM TASK 29-11-00-710-001),
For the Yellow hydraulic system (Ref. AMM TASK 29-13-00-710-002),
For the Blue hydraulic system (Ref. AMM TASK 29-12-00-710-001),

(2) Do the operational test of the hydraulic fire shut-off valve of the applicable hydraulic system (Ref. AMM TASK 29-10-00-710-001).
(3) Do the operational tests of the Power Transfer Unit (PTU):

(4) Do the operational test of the leak-measurement valve of the applicable hydraulic system:

ACTION	RESULT
1.On the ECAM control panel on the center pedestal: push the HYD pushbutton.	On the ECAM lower DU: the HYD page is shown.
2.On the overhead panel 50VU: lift the guard and set the applicable HYD/LEAK MEASUREMENT VALVE pushbutton switch (P/BSW) to OFF (the OFF light comes on).	In less than 15 s on the ECAM lower DU: the color of the system name and system arrow change to amber.
3.On the overhead panel 50VU: lift the guard and set the applicable HYD/LEAK MEASUREMENT VALVE/ P/BSW to on (the OFF light goes off).	On the ECAM lower DU: the color of the system name changes to white, the color of the system arrow changes to green. NOTE: When you set the P/BSW to on, the ECAM lower DU can change to the ELEC page. Also the single chime audio warning and MASTER CAUT light operate. You can ignore these indications. Cancel the MASTER CAUT light and set the HYD page on the ECAM lower DU to find the hydraulic indications.

Subtask 29-00-00-710-053-A

D. Do the operational test of the Yellow auxiliary power (Ref. AMM TASK 29-24-00-710-001).

Subtask 29-00-00-710-054-B

E. Operational Tests of the Ram Air Turbine (RAT)
(1) Do the operational test of the manual deployment and the retraction of the RAT (Ref. AMM TASK 29-22-00-710-007).
(2) Do the operational test of the automatic deployment of the RAT (Ref. AMM TASK 29-22-00-710-006).

Subtask 29-00-00-710-055-A

F. Do the operational test of the Fluid Low-Level Warning-System (Ref. AMM TASK 29-31-00-710-001).

5. Close-up
Subtask 29-00-00-860-083-A

A. Put the aircraft back to the serviceable condition.
(1) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002)
(2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).

[Rev.10 from 2021] 2026.04.01 04:13:18 UTC