Functional Test of the HP Bleed Valve with the Test Set P/N 98D36109001000

TASK 36-11-51-720-805-A
Functional Test of the HP Bleed Valve with the Test Set P/N 98D36109001000

WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE ENGINE SHUTDOWN. USE APPLICABLE THERMAL GLOVES. THE ENGINE PARTS CAN STAY HOT FOR ONE HOUR AFTER SHUTDOWN AND CAN BURN YOU.

WARNING: YOU MUST NOT TOUCH HOT PARTS WITHOUT APPLICABLE GLOVES. HOT PARTS CAN CAUSE AN INJURY.

WARNING: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN POSITION BEFORE YOU START A TASK ON OR NEAR:

THE FLIGHT CONTROLS
THE FLIGHT CONTROL SURFACES
THE LANDING GEAR AND RELATED DOORS
COMPONENTS THAT MOVE.

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

WARNING: BEFORE YOU INSTALL/REMOVE THE GSE TOOL, READ THE MANUFACTURER'S INSTRUCTIONS, AND, WHILE YOU OPERATE THIS TOOL, CAREFULLY OBEY THEM. IF YOU DO NOT DO THIS, INJURY TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.

NOTE: Two persons are necessary to do this test.

FIN: 4000HA1
FIN: 4000HA2

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

REFERENCE	QTY	DESIGNATION
No specific	AR	ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE
No specific	1	AIR SOURCE 3 BAR (43.5 PSI) - REGULATED, FILTERED, DRY
No specific	AR	WARNING NOTICE(S)
No specific	Torque wrench: range to between 0.5 and 0.4 m.daN (44.25 and 35.40 lbf.in )
98D36109001000	1	TEST SET-EBAS,BLEED

B. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
438AR, 452AR
FOR [1000EM2] (ENGINE-2)
448AR, 462AR

C. 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 36-11-00-740-804-A	BITE Test of the Engine Bleed Air System (EBAS) (System Test)
TASK 71-13-00-010-803-A	Opening of the Fan Cowl Doors
TASK 71-13-00-410-803-A	Closing of the Fan Cowl Doors
TASK 78-36-00-010-806-A	Opening of the Thrust Reverser Cowl Doors
TASK 78-36-00-410-806-A	Closing of the Thrust Reverser Cowl Doors
Functional Test of the HP Bleed Valve with the Test Set P/N 98D36109001000

3. Job Set-up
Subtask 36-11-51-861-071-A

A. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).

Subtask 36-11-51-941-073-A

B. Safety Precautions
(1) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(2) On AIR COND panel 30VU:

Make sure that the APU BLEED pushbutton switch is released (the ON legend is off).
Put a WARNING NOTICE(S) in position to tell persons not to operate the pneumatic system.

(3) On ENG panel 115VU:

Put a WARNING NOTICE(S) in position to tell persons not to start the engine 1(2).

(4) On the HP ground connector:

Put a WARNING NOTICE(S) in position to tell persons not to pressurize the pneumatic system.

(5) On the ENG section of maintenance panel 50VU:

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

Subtask 36-11-51-865-073-A

C. Make sure that this(these) circuit breaker(s) is(are) closed:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C ALL
49VU	AIR BLEED/APU BLEED VLV CTL/BMC1 OVRD	11HV	D14
49VU	AIR BLEED/X FEED/VALVE/BAT	2HV	D13
49VU	AIR BLEED/ENG 2/MONG	3HA2	D12
49VU	AIR BLEED/ENG 1/CTL	2HA1	D11
122VU	AIR BLEED/ENG 1/MONG	3HA1	Z23
122VU	AIR BLEED/ENG 2/CTL	2HA2	Z22
122VU	AIR BLEED/X FEED VALVE/NORM	1HV	Z20
122VU	AIR BLEED/APU BLEED VLV CTL/BMC2 OVRD	12HV	Z19

Subtask 36-11-51-010-095-A

D. Get Access
(1) Open the right fan cowl doors (Ref. AMM TASK 71-13-00-010-803):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR.

Subtask 36-11-51-010-096-A

E. Get Access
(1) Open the right thrust reverser cowl doors (Ref. AMM TASK 78-36-00-010-806):
(a) FOR [1000EM1] (ENGINE-1)
452AR
(b) FOR [1000EM2] (ENGINE-2)
462AR.
(2) Put the ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in position below the applicable engine.

4. Procedure
Subtask 36-11-51-750-051-A

A. Manual Test of the HP Bleed Valve
(1) On the valve position indicator, record the position of the valve butterfly.
(2) Make sure that the valve butterfly moves freely:

On the position indicator, use a WRENCH - STANDARD to fully open and fully close the valve butterfly.
Put the valve butterfly in the initial position that you recorded.

Subtask 36-11-51-480-069-A

B. Preparation for the Functional Test

CAUTION: BE CAREFUL WHEN YOU CONNECT/DISCONNECT THE TEST SET TO/FROM THE EQUIPMENT. THE PRESSURE REGULATING VALVE AND THE PRESSURE GAGE ASSEMBLY OF THE TEST SET ARE HEAVY AND CAN CAUSE DAMAGE TO THE ENGINE.

(1) Remove the blanking plug from the test port of the HP bleed valve.
(2) Connect the adaptor assembly to the test port of the HP bleed valve.
(3) Connect the 98D36109001000 TEST SET-EBAS,BLEED with the short hose to the adaptor assembly.
(4) On the 98D36109001000 TEST SET-EBAS,BLEED, close the shutoff valve, the purge valve and the pressure regulator valve.

NOTE: If the air cylinder has a regulator valve, it is not necessary to install the primary regulator valve supplied with the test set.

(5) Connect the AIR SOURCE 3 BAR (43.5 PSI) - REGULATED, FILTERED, DRY to the 98D36109001000 TEST SET-EBAS,BLEED.
(6) Set the digital pressure gage back to zero.

Subtask 36-11-51-720-076-A

C. Functional Test of the HP Bleed Valve with the Engine-Bleed System Test-Set.
(1) Do this test:

ACTION	RESULT
1.On the AIR SOURCE 3 BAR (43.5 PSI) - REGULATED, FILTERED, DRY, open the shutoff valve.	On the AIR SOURCE 3 BAR (43.5 PSI) - REGULATED, FILTERED, DRY, the cylinder pressure gage shows the pressure.
2.On the AIR SOURCE 3 BAR (43.5 PSI) - REGULATED, FILTERED, DRY, use the primary regulator to pressurize the pressure source to 43.5 psi (3.00 bar).	On the AIR SOURCE 3 BAR (43.5 PSI) - REGULATED, FILTERED, DRY, the primary gage shows 43.5 psi (3.00 bar).
3.On the 98D36109001000 TEST SET-EBAS,BLEED: Slowly pressurize the system between 30 psi (2.07 bar) and 40 psi (2.76 bar).	On the HP bleed valve: Make sure that you hear the airflow through the vent of the valve.
4.In the cockpit: DO the BITE test of the EBAS (Ref. AMM TASK 36-11-00-740-804).	On the HP bleed valve: Make sure that the position indicator shows OPEN.
5.In the cockpit: Complete the BITE test. NOTE: The pressure must be applied during all the test.
6.On the 98D36109001000 TEST SET-EBAS,BLEED: Depressurize the system and close the shutoff valve. NOTE: The HPV stays open and will close automatically at the next engine start.

Subtask 36-11-51-080-069-A

D. Disconnection of the Test Set

(1) Disconnect the 98D36109001000 TEST SET-EBAS,BLEED from the adaptor assembly.
(2) Disconnect the adaptor assembly from the test port of the HP bleed valve.
(3) Install the blanking plug on the test port.
(4) TORQUE the blanking plug to between 0.5 and 0.4 m.daN (44.25 and 35.40 lbf.in )

.
(5) Disconnect the 98D36109001000 TEST SET-EBAS,BLEED from the AIR SOURCE 3 BAR (43.5 PSI) - REGULATED, FILTERED, DRY.

5. Close-up
Subtask 36-11-51-410-091-A

A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the access platform(s).
(3) Close the right thrust-reverser cowl doors (Ref. AMM TASK 78-36-00-410-806):
(a) FOR [1000EM1] (ENGINE-1)
452AR.
(b) FOR [1000EM2] (ENGINE-2)
462AR.

Subtask 36-11-51-410-092-A

B. Close Access
(1) Close the right fan cowl doors (Ref. AMM TASK 71-13-00-410-803):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR.
(2) Remove the WARNING NOTICE(S).

Subtask 36-11-51-862-068-A

C. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

[Rev.10 from 2021] 2026.04.01 01:12:33 UTC