Functional Test of the Bleed Transferred Pressure-Transducer with the Bleed Test Set P/N 98D36109001000

TASK 36-11-15-720-803-A
Functional Test of the Bleed Transferred Pressure-Transducer with the Bleed Test Set P/N 98D36109001000

WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AFTER SHUTDOWN. THE ENGINE CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.

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: 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.

WARNING: BEFORE YOU START WORK, YOU MUST PUT ON A SAFETY HARNESS AND ATTACH IT TO THE ACCESS PLATFORM. WITHOUT A SAFETY HARNESS, YOU CAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.

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.

FIN: 7HA1
FIN: 7HA2

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 5M (16 FT)- ADJUSTABLE
No specific	1	AIR SOURCE - REGULATED, FILTERED, DRY
No specific	AR	PLUG - BLANKING
No specific	AR	WARNING NOTICE(S)
No specific	Torque wrench: range to between 0.84 and 0.83 m.daN (74.34 and 73.45 lbf.in )
98D36109001000	1	TEST SET-EBAS,BLEED

B. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
FOR [7HA1] (XDCR-BLEED TRANSFER PRESS, ENG 1)
415BL
FOR [7HA2] (XDCR-BLEED TRANSFER PRESS, ENG 2)
425BL

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 31-32-00-860-011-A	Procedure to Get Access to the SYSTEM REPORT/TEST/PNEU Page
TASK 78-30-00-040-807-A	Deactivation of the Thrust Reverser System for Nacelle Maintenance (ICU)
TASK 78-30-00-440-807-A	Reactivation of the Thrust Reverser System after Nacelle Maintenance (ICU)
MCDU Valve Status Page
Functional Test of the Bleed Transferred Pressure-Transducer with the Bleed Test Set P/N 98D36109001000
FOR [7HA1] (XDCR-BLEED TRANSFER PRESS, ENG 1)
TASK 54-51-21-000-804-A	Removal of the Pylon Lateral Access-Doors
TASK 54-51-21-400-803-A	Installation of the Pylon Lateral Access-Doors
FOR [7HA2] (XDCR-BLEED TRANSFER PRESS, ENG 2)
TASK 54-51-21-000-804-A	Removal of the Pylon Lateral Access-Doors
TASK 54-51-21-400-803-A	Installation of the Pylon Lateral Access-Doors

3. Job Set-up
Subtask 36-11-15-861-059-A

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

Subtask 36-11-15-941-058-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 ENG 1(2) BLEED pushbutton switch is released (OFF legend is on).
Make sure that the APU BLEED pushbutton switch is released (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 the persons not to start 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 36-11-15-865-061-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 36-11-15-040-051-A

D. Deactivation of the Thrust Reverser System

WARNING: MAKE SURE THAT THE THRUST REVERSER HYDRAULIC CONTROL UNIT (HCU) IS DEACTIVATED BEFORE YOU DO WORK ON OR AROUND THE THRUST REVERSER. IF THE HCU IS NOT DEACTIVATED, THERE IS A RISK OF UNWANTED THRUST REVERSER OPERATION WHICH CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.

(1) Make the thrust reverser unserviceable for maintenance (Ref. AMM TASK 78-30-00-040-807).

Subtask 36-11-15-010-063-A

E. Get Access
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the pylon access.
(2) Remove the access panel:
(a) FOR [7HA1] (XDCR-BLEED TRANSFER PRESS, ENG 1)
415BL (Ref. AMM TASK 54-51-21-000-804)
(b) FOR [7HA2] (XDCR-BLEED TRANSFER PRESS, ENG 2)
425BL (Ref. AMM TASK 54-51-21-000-804).

Subtask 36-11-15-020-055-A

F. Disconnection of the Sense Line

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

CAUTION: USE A SECOND WRENCH TO APPLY COUNTERTORQUE TO THE UNION WHEN YOU DISCONNECT/CONNECT THE PNEUMATIC LINES ON UNIONS.

(1) Disconnect the sense line from the bleed transferred pressure-transducer.
(2) Put the PLUG-BLANKING in each disconnected line end.

Subtask 36-11-15-860-060-A

G. Aircraft Maintenance Configuration
(1) Adjust the brightness of the MCDU screen.
(2) On one MCDU, get the SYSTEM REPORT/TEST PNEU/SENSOR STATUS menu page (Ref. AMM TASK 31-32-00-860-011).

MCDU Valve Status Page

4. Procedure
Subtask 36-11-15-720-055-A

A. Functional Test of the Bleed Transferred Pressure-Transducer
(1) Close the shutoff valve, the purge valve and the pressure regulator valve on the 98D36109001000 TEST SET-EBAS,BLEED.
(2) Connect an AIR SOURCE - REGULATED, FILTERED, DRY to the 98D36109001000 TEST SET-EBAS,BLEED.
(3) Connection of the 98D36109001000 TEST SET-EBAS,BLEED:
(a) Connect the 98D36109001000 TEST SET-EBAS,BLEED with the short hose to the adaptor assembly.
(b) Connect the adaptor assembly to the test port of the bleed transferred pressure-transducer.
(c) Tighten the adaptor assembly.
(4) Do a reset of the digital pressure gage.
(5) Make sure that the regulator valve of the 98D36109001000 TEST SET-EBAS,BLEED is closed before pressurize the system.
(6) Do the test that follows:

ACTION	RESULT
1.On the MCDU control panel: Push the SENSOR STATUS key.	On the MCDU: The SENSOR STATUS page comes into view and shows the bleed pressure.
2.Pressurize the 98D36109001000 TEST SET-EBAS,BLEED: If there is a manometer on the AIR SOURCE - REGULATED, FILTERED, DRY, installation of the primary regulator valve is not necessary. Use the AIR SOURCE - REGULATED, FILTERED, DRY shutoff valve and the manometer to slowly pressurize the 98D36109001000 TEST SET-EBAS,BLEED to 200 psi (13.7895 bar). If there is no manometer in the AIR SOURCE - REGULATED, FILTERED, DRY, installation of primary regulator valve is mandatory. In this case the primary regulator valve will limit the pressure in the 98D36109001000 TEST SET-EBAS,BLEED to 217 psi (14.9616 bar).
3.On the 98D36109001000 TEST SET-EBAS,BLEED: Open the shutoff valve. Use the regulator valve on the 98D36109001000 TEST SET-EBAS,BLEED to slowly pressurize the system from 10 psi (0.6895 bar) to 170 psi (11.7211 bar)	On the 98D36109001000 TEST SET-EBAS,BLEED: The digital pressure gage shows the pressure. On the SD: The status page shows the supplied pressure, which must agree with the value of the digital pressure gage plus or minus 2 psi (0.14 bar).
4.On the 98D36109001000 TEST SET-EBAS,BLEED: Use the regulator valve on the 98D36109001000 TEST SET-EBAS,BLEED to depressurize the system.	On the 98D36109001000 TEST SET-EBAS,BLEED: The digital pressure gage shows 0 psi (0.0000 bar).

(7) Close the shutoff valve of the AIR SOURCE - REGULATED, FILTERED, DRY.
(8) Slowly open the purge valve to depressurize the 98D36109001000 TEST SET-EBAS,BLEED to 0 psi (0.0000 bar).
(9) Disconnection of the 98D36109001000 TEST SET-EBAS,BLEED:

WARNING: BEFORE YOU START TO REMOVE THE TOOLING, MAKE SURE THAT THERE IS NO PRESSURIZED GAS LEFT INSIDE THE DUCTS. IT CAN CAUSE AN INJURY TO PERSONNEL AND/OR DAMAGE TO EQUIPMENT.

(a) Disconnect the 98D36109001000 TEST SET-EBAS,BLEED from the test port of the bleed transferred pressure-transducer.
(b) Disconnect the short hose from the adaptor assembly.
(c) Disconnect the short hose from the 98D36109001000 TEST SET-EBAS,BLEED.

5. Close-up
Subtask 36-11-15-860-061-A

A. Aircraft Maintenance Configuration
(1) Close the MCDU session.
(2) Fully decrease the brightness of the MCDU screen (display off).

Subtask 36-11-15-420-057-A

B. Connection of the Sense Line

CAUTION: USE A SECOND WRENCH TO APPLY COUNTERTORQUE TO THE UNION WHEN YOU DISCONNECT/CONNECT THE PNEUMATIC LINES ON UNIONS.

(1) Remove the PLUG-BLANKING from each disconnected line end.
(2) Connect the sense line to the bleed transferred pressure-transducer.
(3) TORQUE the nut of the sense line to between 0.84 and 0.83 m.daN (74.34 and 73.45 lbf.in )

Subtask 36-11-15-410-061-A

C. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the access panel:
(a) FOR [7HA1] (XDCR-BLEED TRANSFER PRESS, ENG 1)
415BL (Ref. AMM TASK 54-51-21-400-803)
(b) FOR [7HA2] (XDCR-BLEED TRANSFER PRESS, ENG 2)
425BL (Ref. AMM TASK 54-51-21-400-803).
(3) Remove the access platform(s).
(4) Remove the WARNING NOTICE(S).

Subtask 36-11-15-440-050-A

D. Reactivation of the Thrust Reverser System
(1) Make the thrust reverser serviceable (Ref. AMM TASK 78-30-00-440-807).

Subtask 36-11-15-862-058-A

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

[Rev.10 from 2021] 2026.04.01 01:08:24 UTC