Deactivation of the Pylon Overheat Sensing-Element
TASK 36-22-00-040-001-A
Deactivation of the Pylon Overheat Sensing-Element
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
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 36-22-00-861-052-A ** ON A/C NOT FOR ALL Subtask 36-22-00-941-052-A ** ON A/C NOT FOR ALL
Subtask 36-22-00-790-052-A ** ON A/C NOT FOR ALL
Subtask 36-22-00-865-054-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 01:16:26 UTC
Deactivation 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.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
1. Reason for the JobMMEL 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 | BRUSH - BRISTLED, SOFT |
| 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 | AR | CAP - BLANKING |
| No specific | AR | TIE WRAP |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.08BBB1) | Non Aqueous Cleaner-- Petroleum Based - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| 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 | |
| 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 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 36-22-00-790-001-A | Leak Check on all the Bleed Air Ducts and the Packs Components |
| 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 |
| FOR [1HF1] (SNSG ELEM-OVHT, ENG 1 PYLON) | |
| FOR [1HF2] (SNSG ELEM-OVHT, ENG 2 PYLON) | |
| ESPM 205451 | |
Subtask 36-22-00-861-052-A ** ON A/C NOT FOR ALL Subtask 36-22-00-941-052-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:
(a) Put the WARNING NOTICE(S) in position to tell persons not to pressurize the pneumatic system.
(6) In the cockpit, on the ENG section of 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 36-22-00-865-057-A ** ON A/C NOT FOR ALL (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:
(a) Put the WARNING NOTICE(S) in position to tell persons not to pressurize the pneumatic system.
(6) In the cockpit, on the ENG section of 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).
C. Open, safety and tag this(these) circuit breaker(s):
Subtask 36-22-00-010-050-A ** ON A/C NOT FOR ALL | 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 |
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 36-22-00-010-050-C ** ON A/C NOT FOR ALL (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.
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(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.
Subtask 36-22-00-790-052-A ** ON A/C NOT FOR ALL
A. Leak Check
(1) Do a leak check on the related pylon (Ref. AMM TASK 36-22-00-790-001) at the bleed air ducts. Make sure that there are no leaks, specially from the clamps and the connections.
Subtask 36-22-00-110-057-A ** ON A/C NOT FOR ALL (1) Do a leak check on the related pylon (Ref. AMM TASK 36-22-00-790-001) at the bleed air ducts. Make sure that there are no leaks, specially from the clamps and the connections.
- If there is a leak, it will be a NO GO. Repair the bleed air duct.
- If there is no leak, do the deactivation of the related sensing element (refer to Para. 4.B and 4.C).
B. Cleaning of the Outer Side of the Electrical Connectors
(1) Remove the collected oil, grease and dirt from the outer side of each connector.
(2) To do this, use a BRUSH - BRISTLED, SOFT with Non Aqueous Cleaner-- Petroleum Based - (Material No.08BBB1) . Dry them with a Textile-Lint free Cotton - (Material No.14SBA1) .
Subtask 36-22-00-040-050-A ** ON A/C NOT FOR ALL (1) Remove the collected oil, grease and dirt from the outer side of each connector.
(2) To do this, use a BRUSH - BRISTLED, SOFT with Non Aqueous Cleaner-- Petroleum Based - (Material No.08BBB1) . Dry them with a Textile-Lint free Cotton - (Material No.14SBA1) .
C. Deactivation of the Pylon Overheat Sensing-Element
(1) FOR [1HF1] (SNSG ELEM-OVHT, ENG 1 PYLON), [1HF2] (SNSG ELEM-OVHT, ENG 2 PYLON)
(c) Put the CAP - BLANKING on each disconnected electrical connector and sensing-element connector ends.
(d) Put a plastic bag or a shrinkable sleeve on the connectors and safety it with a TIE WRAP ESPM 205451.
5. Close-up(1) FOR [1HF1] (SNSG ELEM-OVHT, ENG 1 PYLON), [1HF2] (SNSG ELEM-OVHT, ENG 2 PYLON)
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.
(a) Cut, remove and discard the lockwires from the electrical connectors (1) and (2). 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.
(b) Disconnect the electrical connectors (1) and (2) from the sensing element. (c) Put the CAP - BLANKING on each disconnected electrical connector and sensing-element connector ends.
(d) Put a plastic bag or a shrinkable sleeve on the connectors and safety it with a TIE WRAP ESPM 205451.
NOTE: The plastic bag or the shrinkable sleeve gives protection from humidity.
(e) Safe tie the electrical connectors with a TIE WRAP to the adjacent structure or the nearest cable in the upright position ESPM 205451.Subtask 36-22-00-865-054-A ** ON A/C NOT FOR ALL
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 36-22-00-740-050-A ** ON A/C NOT FOR ALL | 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 |
B. Do the BITE test of the BMC 1(2) (Ref. AMM TASK 36-11-00-740-001).
(1) The pylon loop 1(2) message ENG 1(2) PYLON LOOP INOP must come into view.
(2) Make sure that the related ENG1(2) BLEED pushbutton switch stays released for the flight (the OFF legend is on).
(3) Make an entry in the logbook.
Subtask 36-22-00-410-050-A ** ON A/C NOT FOR ALL (1) The pylon loop 1(2) message ENG 1(2) PYLON LOOP INOP must come into view.
(2) Make sure that the related ENG1(2) BLEED pushbutton switch stays released for the flight (the OFF legend is on).
(3) Make an entry in the logbook.
C. 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 36-22-00-410-050-C ** ON A/C NOT FOR ALL (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).
C. 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).
(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).
Pylon Overheat-Sensing-Element Electrical-Connectors