Leak Check of the RH Wing using Bleed Air from the opposite Engine 1

TASK 36-11-00-720-808-A
Leak Check of the RH Wing using Bleed Air from the opposite Engine 1

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.

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 2M (6 FT) - ADJUSTABLE
No specific	AR	ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific	AR	PLUG - BLANKING
No specific	AR	WARNING NOTICE(S)

B. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
191BB, 192FB
192BT, 192CT, 621AB, 621BT, 621CB, 621EB
FOR [1000EM2] (ENGINE-2)
423CL, 423DL, 423FL, 424CR, 447AL, 461AL

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 31-60-00-860-001-A	EIS Start Procedure
TASK 36-22-00-790-001-A	Leak Check on all the Bleed Air Ducts and the Packs Components
TASK 53-35-11-000-001-A	Removal of the Wing-to-Fuselage Fairings
TASK 53-35-11-400-001-A	Installation of the Wing-to-Fuselage Fairings
TASK 57-41-37-000-004-A	Removal of the Pressure Relief Panels
TASK 57-41-37-400-002-A	Installation of the Pressure Relief Panels
TASK 71-00-00-710-003-A	Engine Automatic Start
TASK 71-00-00-710-003-B	Engine Automatic Start
TASK 71-00-00-710-018-A	Discontinued Start, Restart and Shutdown Procedures
TASK 71-00-00-710-028-A	Engine Shutdown
TASK 71-00-00-710-028-B	Engine Shutdown
TASK 71-00-00-710-043-A	Normal Engine Automatic-Start Procedure
TASK 71-13-00-010-010-A	Opening of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 71-13-00-010-040-A	Opening of the Fan Cowl Doors
TASK 71-13-00-010-040-B	Opening of the Fan Cowl Doors
TASK 71-13-00-410-010-A	Closing of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 71-13-00-410-040-A	Closing of the Fan Cowl Doors
TASK 71-13-00-410-040-B	Closing of the Fan Cowl Doors
TASK 78-32-00-010-010-A	Opening of the Thrust Reverser Halves
TASK 78-32-00-410-010-A	Closing of the Thrust Reverser Halves
TASK 78-36-00-010-040-A	Opening of the Thrust Reverser Doors
TASK 78-36-00-010-040-B	Opening of the Thrust Reverser Doors
TASK 78-36-00-410-040-A	Closing of the Thrust Reverser Doors
TASK 78-36-00-410-040-B	Closing of the Thrust Reverser Doors

3. Job Set-up
Subtask 36-11-00-861-118-A ** ON A/C NOT FOR ALL

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

Subtask 36-11-00-941-121-A ** ON A/C NOT FOR ALL

B. Safety Precautions
(1) Make sure that the engine 2 shut down occurred not less than 5 minutes before you do this procedure.
(2) Put a WARNING NOTICE(S) on the panel 115VU to tell persons not to start the engine 2.
(3) In the cockpit:

put WARNING NOTICE(S) to tell persons not to operate the pneumatic system,
put WARNING NOTICE(S) to tell persons not to operate the slats.

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

make sure that the ON legend of the ENG/FADEC GND PWR 1 pushbutton switch is off,
put a WARNING NOTICE(S) to tell persons not to operate the FADEC 1.

Subtask 36-11-00-865-087-A ** ON A/C NOT FOR ALL

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

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	AIR BLEED/X FEED/VALVE/BAT	2HV	D13
49VU	AIR BLEED/ENG 1/CTL	3HA1	D12
49VU	AIR BLEED/ENG 1/MONG	2HA1	D11

Subtask 36-11-00-010-140-A ** ON A/C NOT FOR ALL

D. Get Access
(1) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position under the zone 191BB.
(2) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position under the zone 621.
(3) Open the access doors of the air conditioning units 191BB.
(4) Remove the access panels on the wings and belly fairings:
(a) For the right wing and belly fairing:

(5) Remove these access panels on the pylon:
(a) FOR [1000EM2] (ENGINE-2)
423CL 424CR 423DL 423FL.
(6) Open the right fan cowl door (Ref. AMM TASK 71-13-00-010-040).
(a) FOR [1000EM2] (ENGINE-2)
447AL.
(7) Open the right thrust-reverser cowl door (Ref. AMM TASK 78-36-00-010-040):
(a) FOR [1000EM2] (ENGINE-2)
461AL.

Subtask 36-11-00-010-140-C ** ON A/C NOT FOR ALL

Subtask 36-11-00-010-140-D ** ON A/C NOT FOR ALL

(5) Remove these access panels on the pylon:
(a) FOR [1000EM2] (ENGINE-2)
423CL 423DL 423FL 424CR.
(6) Open the right fan cowl door (Ref. AMM TASK 71-13-00-010-010).
(a) FOR [1000EM2] (ENGINE-2)
447AL.
(7) Open the right thrust-reverser cowl door (Ref. AMM TASK 78-32-00-010-010):
(a) FOR [1000EM2] (ENGINE-2)
461AL.

Subtask 36-11-00-860-081-A ** ON A/C NOT FOR ALL

E. Aircraft Maintenance Configuration
(1) Do the EIS start procedure (ECAM system only) (Ref. AMM TASK 31-60-00-860-001).
(2) In the air conditioning compartment:

disconnect the pressurization interconnection line of the water tank, hydraulic reservoir and trim air valve from the pressure service check valves (7272HM and 7270HM).

(3) Put PLUG - BLANKING on the disconnected line ends.
(4) On the ECAM control panel 11VU:

push the BLEED pushbutton switch (the BLEED page comes into view on the lower ECAM display unit).

(5) On the AIR COND panel 30VU, make sure that:

the PACK1 and PACK2 pushbutton switches are released (the OFF legends are on),
the X BLEED selector switch is set to AUTO (the BLEED page shows that the X BLEED valve is closed),
the ENG1 BLEED pushbutton switch is released (the ON legend is off) (the BLEED page shows that the ENG1 BLEED valve is closed).

(6) On the ANTI-ICE section of the panel 25VU:

make sure that the ANTI-ICE/WING pushbutton switch is released (the ON legend is off).

4. Procedure
Subtask 36-11-00-720-089-A ** ON A/C NOT FOR ALL

A. Functional Test of the Engine Bleed-Air-Supply System
(1) Start the ENG1 and let it become stable at ground idle (Ref. AMM TASK 71-00-00-710-003).
(2) On the AIR COND panel 30VU, push the ENG1 BLEED pushbutton switch (the ON legend is on) to pressurize the bleed duct system.
(3) Set the XBLEED selector switch to OPEN.
(a) The BLEED page shows that the XBLEED valve is open.
(4) Do the leak test of all the air ducts in the RH wing (Ref. AMM TASK 36-22-00-790-001).
(5) Stop the ENG1 (Ref. AMM TASK 71-00-00-710-028).

Subtask 36-11-00-720-089-C ** ON A/C NOT FOR ALL

Subtask 36-11-00-720-089-D ** ON A/C NOT FOR ALL

A. Functional Test of the Engine Bleed-Air-Supply System
(1) Start the ENG1 and let it become stable at ground idle (Ref. AMM TASK 71-00-00-710-043).
(2) On the AIR COND panel 30VU, push the ENG1 BLEED pushbutton switch (the ON legend is on) to pressurize the bleed duct system.
(3) Set the XBLEED selector switch to OPEN.
(a) The BLEED page shows that the XBLEED valve is open.
(4) Do the leak test of all the air ducts in the RH wing (Ref. AMM TASK 36-22-00-790-001).
(5) Stop the ENG1 (Ref. AMM TASK 71-00-00-710-018).

5. Close-up
Subtask 36-11-00-860-082-A ** ON A/C NOT FOR ALL

A. Put the aircraft back to its initial configuration.
(1) On the AIR COND panel 30VU, release the ENG1 BLEED pushbutton switch (the ON legend is off)
(2) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(3) In the air conditioning compartment:

remove the PLUG - BLANKING from the line ends.

(4) Connect the pressurization interconnection lines of the water tank, hydraulic reservoir and trim air valve to the pressure service check valves (7272HM and 7270HM).
(5) Make sure that the work area is clean and clear of tools and other items.
(6) Close the access doors of the air conditioning units 191BB 192FB.

Subtask 36-11-00-410-133-A ** ON A/C NOT FOR ALL

B. Close Access
(1) Close the right thrust-reverse cowl door (Ref. AMM TASK 78-36-00-410-040).
(a) FOR [1000EM2] (ENGINE-2)
461AL.
(2) Close the right fan cowl door (Ref. AMM TASK 71-13-00-410-040).
(a) FOR [1000EM2] (ENGINE-2)
447AL.
(3) Install these access panels on the pylon:
(a) FOR [1000EM2] (ENGINE-2)
423CL 424CR 423DL 423FL.
(4) Install the access panels under the leading edge of the wing and belly fairing:
(a) For the right wing and belly fairing:

(5) Remove the WARNING NOTICE(S).
(6) Remove the access platform(s).

Subtask 36-11-00-410-133-C ** ON A/C NOT FOR ALL

(5) Remove the WARNING NOTICE(S).
(6) Remove the access platform(s).

Subtask 36-11-00-410-133-D ** ON A/C NOT FOR ALL

B. Close Access
(1) Close the right thrust-reverse cowl door (Ref. AMM TASK 78-32-00-410-010).
(a) FOR [1000EM2] (ENGINE-2)
461AL.
(2) Close the right fan cowl door (Ref. AMM TASK 71-13-00-410-010).
(a) FOR [1000EM2] (ENGINE-2)
447AL.
(3) Install these access panels on the pylon:
(a) FOR [1000EM2] (ENGINE-2)
423CL 423DL 423FL 424CR.
(4) Install the access panels under the leading edge of the wing and belly fairing:
(a) For the right wing and belly fairing:

(5) Remove the WARNING NOTICE(S).
(6) Remove the access platform(s).

Subtask 36-11-00-862-103-A ** ON A/C NOT FOR ALL

C. De-energize the aircraft electrical circuits

[Rev.10 from 2021] 2026.04.01 01:07:20 UTC