Installation of the Pylon Bleed-Air Ducts

TASK 36-11-49-400-041-A
Installation of the Pylon Bleed-Air Ducts

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

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.

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	AR	WARNING NOTICE(S)

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.03QBB9)	Dry lubricant-General Assembly Molybdenum Disulfide -

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
413CL, 413DL, 414CR, 414FR, 423CL, 423DL, 423FL, 424CR

D. Expendable Parts

FIG.ITEM	DESIGNATION	IPC-CSN
4	SEALS	AIPC 36-11-06-01-140

E. Referenced Information

REFERENCE	DESIGNATION
TASK 20-26-00-910-002-A	Installation of Expansion Joints
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 24-41-00-862-002-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 36-11-42-000-001-A	Removal of the Bleed-Air Precooler Exchanger
TASK 36-11-42-400-001-A	Installation of the Bleed-Air Precooler Exchanger
TASK 36-11-43-000-001-A	Removal of the Fan-Air Valve Control-Thermostat
TASK 36-11-43-400-001-A	Installation of the Fan-Air Valve Control-Thermostat
TASK 36-11-55-000-001-A	Removal of the Bleed-Pressure-Regulator Valve Control-Solenoid
TASK 36-11-55-400-001-A	Installation of the Bleed-Pressure-Regulator Valve Control-Solenoid
TASK 36-12-00-860-001-A	Pressurization of the Bleed System with the APU
TASK 36-12-00-860-002-A	Pressurization of the Bleed System through the HP Ground Connector
TASK 49-00-00-860-009-A	APU Shutdown by External Power (131-9(A))
TASK 49-00-00-860-009-A-01	APU Shutdown by Batteries (131-9(A))
Pylon Bleed-Air Ducts
Installation of the Expansion Joints

3. Job Set-up
Subtask 36-11-49-860-051-A ** ON A/C NOT FOR ALL

A. Aircraft Maintenance Configuration
(1) Make sure that the aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002) or (Ref. AMM TASK 24-41-00-861-002).
(2) Make sure that engine 1(2) is shutdown for a minimum of 5 minutes before you do this procedure.
(3) In the cockpit, on AIR COND panel 30VU:

Make sure that the ENG 1(2) BLEED pushbutton-switch is released (the OFF legend is on)
Make sure that the APU BLEED pushbutton-switch is released (the ON legend is off)
Make sure that the WARNING NOTICE(S) is in position to tell persons not to operate the pneumatic system.

(4) In the cockpit, on ENG panel 115VU:

Make sure that the WARNING NOTICE(S) is in position to tell persons not to start engine 1(2).

(5) On the HP ground connector:

Make sure that the WARNING NOTICE(S) is in position to tell persons not to pressurize the pneumatic system.

(6) In the cockpit, 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.
Make sure that the WARNING NOTICE(S) is in position to tell persons not to energize FADEC 1(2).

(7) Make sure that the ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE is in position below the engine.

Subtask 36-11-49-010-072-A ** ON A/C NOT FOR ALL

B. Get Access
(1) Make sure that these access panels are removed:
(a) For the left pylon:

413CL 414CR 413DL 414FR.

(b) For the right pylon:

423CL 424CR 423DL 423FL.

(2) Make sure that the bleed-air precooler exchanger is removed (Ref. AMM TASK 36-11-42-000-001).
(3) Make sure that the bleed pressure-regulator valve control-solenoid is removed (Ref. AMM TASK 36-11-55-000-001).
(4) Make sure that the fan-air valve-control thermostat is removed (Ref. AMM TASK 36-11-43-000-001).

Subtask 36-11-49-865-077-A ** ON A/C NOT FOR ALL

C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	AIR BLEED/ENG 1/CTL	3HA1	D12
49VU	AIR BLEED/ENG 1/MONG	2HA1	D11
122VU	AIR BLEED/ENG 2/CTL	3HA2	Z23
122VU	AIR BLEED/ENG 2/MONG	2HA2	Z22

4. Procedure
Subtask 36-11-49-420-062-E ** ON A/C NOT FOR ALL

A. Installation of the Wing Connection Sleeve
(1) If you use the APU to energize the electrical circuits, stop the APU:

For GTCP 36-300 APU (Ref. AMM D/O 49-00-00-86)
For APS 3200 APU (Ref. AMM D/O 49-00-00-86)
For 131-9(A) APU (Ref. AMM TASK 49-00-00-860-009).

(2) In the cockpit, on the SD bleed page:
(a) Make sure that the pressure and the temperature of the bleed-air duct system are in ambient conditions.

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

WARNING: DO NOT TOUCH THE UNIT UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS WHEN YOU DO THE MAINTENANCE TASK(S).

(3) Remove the blanking plugs from the disconnected line ends.
(4) Install a new AIPC 36-11-06-01-140 SEALS (4) in one expansion joint (6) (Ref. AMM TASK 20-26-00-910-002).
(5) Install a new AIPC 36-11-06-01-140 SEALS (4) in the other expansion joint (6) (Ref. AMM TASK 20-26-00-910-002).
(6) Install the wing connection sleeve (3).

Subtask 36-11-49-420-064-A ** ON A/C NOT FOR ALL

B. Installation of the Expansion joints (Ref. AMM TASK 20-26-00-910-002)
(1) Install the clamp (2) but do not tighten it at this time.
(2) Install one expansion joint (6) on the wing connection sleeve (3), with Dry lubricant-General Assembly Molybdenum Disulfide - (Material No.03QBB9) .
(3) Install the other expansion joint (6) on the wing connection sleeve (3), with Dry lubricant-General Assembly Molybdenum Disulfide - (Material No.03QBB9) .
(4) Install the clamp (7) on the expansion joint (6). Install the other expansion joint (6). Do not tighten the clamp (7).
(5) Install the aft pipe of the exchanger (11). To do this, apply a layer of Dry lubricant-General Assembly Molybdenum Disulfide - (Material No.03QBB9) to the friction surface of the expansion joint.

Subtask 36-11-49-420-064-B ** ON A/C NOT FOR ALL

B. Installation of the Expansion Joints (Ref. AMM TASK 20-26-00-910-002)
(1) Install the clamp (2) but do not tighten it at this time.
(2) Install one expansion joint (6) on the wing connection sleeve (3).
(3) Install the other expansion joint (6) on the wing connection sleeve (3).
(4) Install the clamp (7) on the expansion joint (6). Do not tighten the clamp (7).
(5) Install the aft pipe of the exchanger (11).

Subtask 36-11-49-420-063-B ** ON A/C NOT FOR ALL

C. Installation of the Clamp
(1) Install the bolts (8), the washers (9) and the nuts (10). Tighten the nuts.
(2) Install the tab (13) and the nut (12). Tighten the nut.
(3) Tighten the clamps (2) and (7).

Subtask 36-11-49-820-051-A ** ON A/C NOT FOR ALL

D. Make sure that the expansion joints (6) are in the correct position in relation to the wing connection sleeve (3) and the pipe (11).

Installation of the Expansion Joints ** ON A/C NOT FOR ALL

Subtask 36-11-49-410-068-A ** ON A/C NOT FOR ALL

E. Installation of the Fan-Air Valve-Control Termostat
(1) Install the fan-air valve-control thermostat (Ref. AMM TASK 36-11-43-400-001).
(2) Install the bleed pressure-regulator valve control-solenoid (Ref. AMM TASK 36-11-55-400-001).
(3) Install the bleed-air precooler exchanger (Ref. AMM TASK 36-11-42-400-001).

Subtask 36-11-49-720-054-A ** ON A/C NOT FOR ALL

F. Do this test:
(1) Pressurize the bleed system through the HP ground connector (Ref. AMM TASK 36-12-00-860-002) or with the APU (Ref. AMM TASK 36-12-00-860-001).
(2) 0n the panel 30VU, put the X-BLEED selector switch in the OPEN position.
(3) If you pressurize the bleed system through the HP ground connector, the supplied pressure 30 psi (2.07 bar) must be stable.
(4) Make sure that there are no leaks at the junctions of the installed duct.

5. Close-up
Subtask 36-11-49-865-078-A ** ON A/C NOT FOR ALL

A. 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
49VU	AIR BLEED/ENG 1/CTL	3HA1	D12
49VU	AIR BLEED/ENG 1/MONG	2HA1	D11
122VU	AIR BLEED/ENG 2/CTL	3HA2	Z23
122VU	AIR BLEED/ENG 2/MONG	2HA2	Z22

Subtask 36-11-49-410-069-A ** ON A/C NOT FOR ALL

B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install these access panels:
(a) For the left pylon:

413CL 414CR 413DL 414FR.

(b) For the right pylon:

423CL 424CR 423DL 423FL.

(3) Remove the WARNING NOTICE(S).
(4) Remove the access platform(s).

Subtask 36-11-49-862-052-A ** ON A/C NOT FOR ALL

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

[Rev.10 from 2021] 2026.04.01 01:09:57 UTC