Installation of the Self Sealing Half-Coupling of the Green Pump Suction

TASK 29-11-39-400-803-A
Installation of the Self Sealing Half-Coupling of the Green Pump Suction

WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES.

WARNING: DO NOT TOUCH THE HYDRAULIC SYSTEM COMPONENTS FOR A SHORT TIME AFTER THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS STAY HOT FOR SOME TIME AND CAN CAUSE INJURY.

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.

CAUTION: DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS.

FIN: 1700GM ** ON A/C NOT FOR ALL

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	1	ACCESS PLATFORM 2M (6 FT)
No specific	1	CONTAINER 10 L(2 1/2 USGAL)
No specific	AR	WARNING NOTICE(S)
No specific	Torque wrench: range to between 10.17 and 9.04 m.daN (75.00 and 66.67 lbf.ft )

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.02ABA1)	Phosphate Ester Hydraulic Fluid-General Power - -

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
195BB, 197CB, 437AL

D. Expendable Parts

FIG.ITEM	DESIGNATION	IPC-CSN
2	TEFLON RETAINER RING	AIPC 29-11-06-01-031
3	O-RING	AIPC 29-11-06-01-032
5	O-RING	AIPC 29-11-06-01-040

E. Referenced Information

REFERENCE	DESIGNATION
TASK 12-12-29-611-001-A	Fill the Hydraulic Fluid Reservoir with a Hand Pump
TASK 20-29-00-911-002-A	Removal/Installation of an O-ring (Hydraulic Systems)
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 29-10-00-864-001-A	Depressurize the Green Hydraulic System
TASK 29-11-00-710-001-A	Operational Test of the Green Hydraulic System
TASK 29-14-00-614-001-A	Depressurization of the Hydraulic Reservoirs
TASK 31-60-00-860-001-A	EIS Start Procedure
TASK 31-60-00-860-002-A	EIS Stop Procedure
TASK 70-23-00-911-001-A	Tightening Torques
TASK 71-13-00-010-040-A	Opening of the Fan Cowl Doors
TASK 71-13-00-410-040-A	Closing of the Fan Cowl Doors
Self Sealing Half-Coupling of the Green Pump Suction

3. Job Set-up
Subtask 29-11-39-860-057-A ** ON A/C NOT FOR ALL

A. Aircraft Maintenance Configuration
(1) Make sure that the aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that the Green hydraulic system is depressurized
(Ref. AMM TASK 29-10-00-864-001).
(3) Make sure that the reservoir of the Green hydraulic system is depressurized
(Ref. AMM TASK 29-14-00-614-001).
(4) Make sure that the WARNING NOTICE(S) is (are) in position to tell persons not to pressurize the Green hydraulic system:

On the ground service panel of the Green hydraulic-system access-door 197CB.

(5) Make sure that the WARNING NOTICE(S) is (are) in position on the hydraulic-reservoir pressurization access-door 195BB to tell persons not to pressurize the Green hydraulic reservoir.
(6) Make sure that the ACCESS PLATFORM 2M (6 FT) is in position at the engine 1.
(7) Make sure that the left fan-cowl door 437AL is open (Ref. AMM TASK 71-13-00-010-040).

Subtask 29-11-39-941-055-A ** ON A/C NOT FOR ALL

B. Safety Precautions
(1) On the center pedestal, on the ENG panel 115VU:

Make sure that the WARNING NOTICE(S) is (are) in position to tell persons not to start the engine.

(2) Make sure that the engine 1(2) shut down occured not less than five minutesbefore you do this procedure.
(3) Make sure that the WARNING NOTICE(S) is (are) in position to tell persons not to pressurize the Green hydraulic system:

In the cockpit, on the HYD section of the HYD/FUEL panel 40VU.

(4) On the maintenance panel 50VU:

Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
Make sure that the WARNING NOTICE(S) is (are) in position to tell persons not to energize the FADEC 1(2).

(5) Make sure that a CONTAINER 10 L(2 1/2 USGAL) is below the connection of the pressure hose (1) and the fluid disconnect panel (6) to collect the fluid.

4. Procedure
Subtask 29-11-39-420-053-A ** ON A/C NOT FOR ALL

A. Installation of the Self Sealing Half-Coupling of the Green Pump Suction

CAUTION: USE TWO WRENCHES TO REMOVE OR INSTALL THE TUBE COUPLING NUTS:

ONE WRENCH TO HOLD THE UNION, AND
ONE TO LOOSEN OR TIGHTEN THE COUPLING NUT.

THIS PREVENTS DAMAGE TO THE PARTS.

(1) Apply Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) to the new AIPC 29-11-06-01-032 O-RING (3) and AIPC 29-11-06-01-040 O-RING (5).
(2) Install the O-ring (5) on the self sealing half-coupling (4) (Ref. AMM TASK 20-29-00-911-002).
(3) Remove the PLUG - BLANKING from the fluid disconnect panel (6).
(4) Install the self sealing half-coupling (4) on the fluid disconnect panel (6). Tighten the self sealing half-coupling with your hand.
(5) Install the O-ring (3) and the new AIPC 29-11-06-01-031 TEFLON RETAINER RING (2) on the self sealing half-coupling (4).
(6) Remove the PLUG - BLANKING from the disconnected hose (1).
(7) Connect the hose (1) to the self sealing half-coupling (4).
(8) TORQUE the coupling nut of the hose (1) to between 10.17 and 9.04 m.daN (75.00 and 66.67 lbf.ft )

(Ref. AMM TASK 70-23-00-911-001) .

Subtask 29-11-39-710-053-A ** ON A/C NOT FOR ALL

B. Test
(1) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only)
(Ref. AMM TASK 31-60-00-860-001).
(2) Do an operational test of the Green hydraulic system (Ref. AMM TASK 29-11-00-710-001).
(3) During the dry motoring, make sure that there are no leaks from the self sealing half-coupling (4).
(4) Make sure that the level of the hydraulic fluid in the Green reservoir is correct. If necessary, fill the reservoir (Ref. AMM TASK 12-12-29-611-001).

5. Close-up
Subtask 29-11-39-942-053-A ** ON A/C NOT FOR ALL

A. Aircraft Maintenance Configuration
(1) Remove the access platform(s).
(2) remove the CONTAINER 10 L(2 1/2 USGAL).
(3) Make sure that the work area is clean and clear of tools and other items.
(4) Do the EIS stop procedure
(Ref. AMM TASK 31-60-00-860-002).
(5) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

Subtask 29-11-39-410-053-A ** ON A/C NOT FOR ALL

B. Close Access
(1) Close the left fan-cowl door 437AL (Ref. AMM TASK 71-13-00-410-040).

[Rev.10 from 2021] 2026.04.01 00:15:30 UTC