Reactivation of the Pylon Overheat Sensing-Element

TASK 36-22-00-440-001-A
Reactivation of the Pylon Overheat Sensing-Element

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: MAKE SURE THAT THE PNEUMATIC SYSTEM IS DEPRESSURIZED BEFORE YOU START WORK. PRESSURIZED AIR CAN CAUSE INJURY TO PERSONNEL.

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

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

FIN: 1HF1 ** ON A/C NOT FOR ALL
FIN: 1HF2 ** ON A/C NOT FOR ALL

1. Reason for the Job
MMEL 36-22-01B
PYLON LEAK DETECTION SYSTEM
MMEL 36-22-01C
PYLON LEAK DETECTION SYSTEM
MMEL 36-22-01D
PYLON LEAK DETECTION SYSTEM
MMEL 36-22-01A
PYLON LEAK DETECTION SYSTEM
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	AR	CAP - BLANKING
No specific	AR	GUN - SPRAY
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER
No specific	AR	WARNING NOTICE(S)
98D27803000000	AR	LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
FOR [1HF1] (SNSG ELEM-OVHT, ENG 1 PYLON)
FOR [1HF2] (SNSG ELEM-OVHT, ENG 2 PYLON)
No specific	Torque wrench: range to between 0.68 and 0.57 m.daN (60.18 and 50.44 lbf.in )

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.08BGB1)	Non Aqueous Cleaner-Sensing element - Xylene based -
FOR [1HF1] (SNSG ELEM-OVHT, ENG 1 PYLON)
FOR [1HF2] (SNSG ELEM-OVHT, ENG 2 PYLON)
(Material No.14QDC1)	Wire-Locking Dia: 0.5 mm (0.020 inch) CRES -

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
191DB
FOR [1HF1] (SNSG ELEM-OVHT, ENG 1 PYLON)
413DT, 471AL, 471AR
413CL, 413DL, 414CR, 414FR
FOR [1HF2] (SNSG ELEM-OVHT, ENG 2 PYLON)
423DT, 481AL, 481AR
423CL, 423DL, 423FL, 424CR

D. 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 27-00-00-080-002-A	Removal of the Flap/Slat Control-Lever Locking Tool (98D27803000000)
TASK 27-00-00-480-002-A	Installation of the Flap/Slat Control-Lever Locking Tool (98D27803000000)
TASK 36-11-00-740-001-A	BITE Test of the BMC 1(2)
TASK 54-53-11-000-002-A	Removal of the Pylon-to-Wing Access Panels
TASK 54-53-11-000-002-B	Removal of the Pylon-to-Wing Access Panels
TASK 54-53-11-400-002-A	Installation of the Pylon-to-Wing Access Panels
TASK 54-53-11-400-002-B	Installation of the Pylon-to-Wing Access Panels
Pylon Overheat-Sensing-Element Electrical-Connectors

3. Job Set-up
Subtask 36-22-00-861-053-A ** ON A/C NOT FOR ALL

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

Subtask 36-22-00-941-053-A ** ON A/C NOT FOR ALL

B. Safety Precautions
(1) Make sure that engine 1(2) shutdown occurred for a minimum of 5 minutes before you do this procedure.
(2) In the cockpit, on AIR COND panel 30VU:
(a) Make sure that the ENG 1(2) BLEED pushbutton switch is released (the OFF legend is on).
(b) Make sure that the APU BLEED pushbutton switch is released (the ON legend is off).
(c) Put a WARNING NOTICE(S) in position to tell persons not to operate the pneumatic system.
(3) In the cockpit, on ENG panel 115VU:
(a) Make sure that the ENG/MODE selector switch is in the NORM position.
(b) Make sure that the ENG/MASTER 1(2) control switch was in the OFF position for a minimum of 5 minutes before you do this procedure.
(c) Put the WARNING NOTICE(S) in position to tell persons not to start engine 1(2).
(4) In the cockpit, on FLAPS panel 114VU:
(a) Put the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION in position on the flap/slat control lever (Ref. AMM TASK 27-00-00-480-002).
(b) Put the WARNING NOTICE(S) in position on the flap/slat control lever to tell persons not to operate the flap/slat controls.
(5) Open access door 191DB, on the HP ground connector:

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

(6) In the cockpit, on ENG section of the maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR 1(2) pushbutton switch is off.
(b) Put the WARNING NOTICE(S) in position to tell persons not to energize FADEC 1(2).

Subtask 36-22-00-865-055-A ** ON A/C NOT FOR ALL

C. Open, safety and tag this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
FOR FIN: 1HF1 (SNSG ELEMOVHT, ENG 1 PYLON)
49VU	AIR BLEED/ENG 1/CTL	3HA1	D12
49VU	AIR BLEED/ENG 1/MONG	2HA1	D11
FOR FIN: 1HF2 (SNSG ELEMOVHT, ENG 2 PYLON)
122VU	AIR BLEED/ENG 2/CTL	3HA2	Z23
122VU	AIR BLEED/ENG 2/MONG	2HA2	Z22

Subtask 36-22-00-410-051-A ** ON A/C NOT FOR ALL

D. Get Access
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the pylon access.
(2) Remove these access panels (Ref. AMM TASK 54-53-11-000-002):
(a) FOR [1HF1] (SNSG ELEM-OVHT, ENG 1 PYLON)
413CL 414CR 413DL 414FR
(b) FOR [1HF2] (SNSG ELEM-OVHT, ENG 2 PYLON)
423CL 424CR 423DL 423FL.

Subtask 36-22-00-410-051-C ** ON A/C NOT FOR ALL

D. Get Access
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the pylon access.
(2) Remove these access panels (Ref. AMM TASK 54-53-11-000-002):
(a) FOR [1HF1] (SNSG ELEM-OVHT, ENG 1 PYLON)
471AL 471AR 413DT
(b) FOR [1HF2] (SNSG ELEM-OVHT, ENG 2 PYLON)
481AL 481AR 423DT.

4. Procedure
Subtask 36-22-00-110-058-A ** ON A/C NOT FOR ALL

A. Cleaning of the Outer Side of the Electrical Connectors

Pylon Overheat-Sensing-Element Electrical-Connectors ** ON A/C NOT FOR ALL

(1) Do a visual inspection of the component interfaces and the adjacent area.
(2) Make sure that the parts removed after the deactivation procedure are clean and in correct condition.
(3) Cut, remove and discard the tie-wraps.
(4) Remove the electrical connectors from the adjacent structure or cables.
(5) Cut, remove and discard the tie-wraps.
(6) Remove the plastic bags or the shrinkable sleeves from the electrical connectors (1) and (2).
(7) Remove the CAP - BLANKING from each electrical connector and the sensing-element connector ends.
(8) Use a GUN - SPRAY to apply the Non Aqueous Cleaner-Sensing element - Xylene based - (Material No.08BGB1) to:

The end fittings of the sensing elements
The end fittings of the electrical connectors (1) and (2).

NOTE: Airbus recommends that you do not use probes, swabs or other instruments to examine the ends of the connectors when you clean them.

Subtask 36-22-00-440-050-A ** ON A/C NOT FOR ALL

B. Reactivation of the Pylon Overheat Sensing-Element

Pylon Overheat-Sensing-Element Electrical-Connectors ** ON A/C NOT FOR ALL

(1) FOR [1HF1] (SNSG ELEM-OVHT, ENG 1 PYLON), [1HF2] (SNSG ELEM-OVHT, ENG 2 PYLON)

CAUTION: MAKE SURE THAT THE ELECTRICAL CONNECTORS ARE CLEAN BEFORE YOU DISCONNECT OR CONNECT THEM. CONTAMINATION ON THE ELECTRICAL CONNECTORS CAN CAUSE DAMAGE TO EQUIPMENT.

(a) Install the electrical connectors (1) and (2) on the sensing element as follows:
1 Connect the electrical connectors (1) and (2) to the sensing element.
2 TORQUE the electrical connectors (1) and (2) to between 0.68 and 0.57 m.daN (60.18 and 50.44 lbf.in )

WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.

3 Safe tie the electrical connectors (1) and (2) with the 14QDC1Wire-Locking Dia: 0.5 mm (0.020 inch) CRES -.

Subtask 36-22-00-865-056-A ** ON A/C NOT FOR ALL

C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
FOR FIN: 1HF1 (SNSG ELEMOVHT, ENG 1 PYLON)
49VU	AIR BLEED/ENG 1/CTL	3HA1	D12
49VU	AIR BLEED/ENG 1/MONG	2HA1	D11
FOR FIN: 1HF2 (SNSG ELEMOVHT, ENG 2 PYLON)
122VU	AIR BLEED/ENG 2/CTL	3HA2	Z23
122VU	AIR BLEED/ENG 2/MONG	2HA2	Z22

Subtask 36-22-00-740-051-A ** ON A/C NOT FOR ALL

D. Do the BITE test of the BMC 1(2) (Ref. AMM TASK 36-11-00-740-001).
(1) Make sure that there are no messages related to the pylon loops.

5. Close-up
Subtask 36-22-00-410-052-A ** ON A/C NOT FOR ALL

A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install these access panels (Ref. AMM TASK 54-53-11-400-002):
(a) FOR [1HF1] (SNSG ELEM-OVHT, ENG 1 PYLON)
413CL 414CR 413DL 414FR
(b) FOR [1HF2] (SNSG ELEM-OVHT, ENG 2 PYLON)
423CL 424CR 423DL 423FL.
(3) In the cockpit, on FLAPS panel 114VU:
(a) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the flap/slat control lever (Ref. AMM TASK 27-00-00-080-002).
(4) Close access door 191DB.
(5) Remove the WARNING NOTICE(S).
(6) Remove the access platform(s).

Subtask 36-22-00-410-052-C ** ON A/C NOT FOR ALL

A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install these access panels (Ref. AMM TASK 54-53-11-400-002):
(a) FOR [1HF1] (SNSG ELEM-OVHT, ENG 1 PYLON)
471AL 471AR 413DT
(b) FOR [1HF2] (SNSG ELEM-OVHT, ENG 2 PYLON)
481AL 481AR 423DT.
(3) In the cockpit, on FLAPS panel 114VU:
(a) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the flap/slat control lever (Ref. AMM TASK 27-00-00-080-002).
(4) Close access door 191DB.
(5) Remove the WARNING NOTICE(S).
(6) Remove the access platform(s).

Subtask 36-22-00-862-053-A ** ON A/C NOT FOR ALL

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

[Rev.10 from 2021] 2026.04.01 01:16:28 UTC