W DOC AIRBUS | AMM A320F

Installation of the Pylon Bleed-Air Ducts


TASK 36-11-49-400-009-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. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
413CL, 413CR, 413DL, 414CR, 414FR, 423CL, 423DL, 423FL, 424CR
413DT, 423DT, 471AL, 471AR, 481AL, 481AR
 C. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
4
SEALS
AIPC 36-11-06-01-140
 D. 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 49-00-00-860-006-A
APU Shutdown by External Power
TASK 49-00-00-860-006-A-01
APU Shutdown by Batteries
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))
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
F Pylon Bleed-Air Ducts ** ON A/C NOT FOR ALL
F Pylon Bleed-Air Ducts ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 36-11-49-860-097-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:
     (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) Make sure that the WARNING NOTICE(S) is(are) in position to tell persons not to operate the pneumatic system.
   (4) In the cockpit, on ENG panel 115VU:
     (a) Make sure that the WARNING NOTICE(S) is(are) in position to tell persons not to start engine 1(2).
   (5) On the HP ground connector:
     (a) Make sure that the WARNING NOTICE(S) is(are) in position to tell persons not to pressurize the pneumatic system.
   (6) 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) Make sure that the WARNING NOTICE(S) is(are) 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 36-11-49-010-164-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Make sure that these access panels are removed (Ref. AMM TASK 54-53-11-000-002):
     (a) For the left pylon:
     (b) For the right pylon:
   (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 36-11-49-010-164-B ** ON A/C NOT FOR ALL
B. Get Access
   (1) Make sure that these access panels are removed (Ref. AMM TASK 54-53-11-000-002):
     (a) For the left pylon:
     (b) For the right pylon:
   (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 36-11-49-865-146-A ** ON A/C NOT FOR ALL
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 1/CTL3HA1D12
49VUAIR BLEED/ENG 1/MONG2HA1D11
122VUAIR BLEED/ENG 2/CTL3HA2Z23
122VUAIR BLEED/ENG 2/MONG2HA2Z22
4. Procedure
Subtask 36-11-49-420-101-A ** 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:
   (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 two new AIPC 36-11-06-01-140 SEALS (4) in the two expansion joints (6) (Ref. AMM TASK 20-26-00-910-002).
   (5) Install the wing connection sleeve (3).
Subtask 36-11-49-420-102-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 step.
   (2) Install one expansion joint (6) on the wing connection sleeve (3).
   (3) Install the other expansion joint (6) on the aft pipe of the exchanger (11).
   (4) Install the clamp (7) on the expansion joints (6). Do not tighten the clamp (7).
   (5) Install the aft pipe (11) of the precooler exchanger.
Subtask 36-11-49-420-103-A ** ON A/C NOT FOR ALL
C. Installation of the Clamps
   (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 36-11-49-820-057-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) of the precooler exchanger.
Subtask 36-11-49-410-142-A ** ON A/C NOT FOR ALL
E. Installation of the Fan Air-Valve Control-Thermostat
   (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 36-11-49-720-076-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 AIR COND 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 36-11-49-865-147-A ** ON A/C NOT FOR ALL
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 1/CTL3HA1D12
49VUAIR BLEED/ENG 1/MONG2HA1D11
122VUAIR BLEED/ENG 2/CTL3HA2Z23
122VUAIR BLEED/ENG 2/MONG2HA2Z22
Subtask 36-11-49-410-143-A ** ON A/C NOT FOR ALL
B. Close Access
   (1) Make sure that the work area is clean and clear of tool and other items.
   (2) Install these access panels (Ref. AMM TASK 54-53-11-400-002):
     (a) For the left pylon:
     (b) For the right pylon:
   (3) Remove the warning notice.
   (4) Remove the access platform.
Subtask 36-11-49-410-143-B ** ON A/C NOT FOR ALL
B. Close Access
   (1) Make sure that the work area is clean and clear of tool and other items.
   (2) Install these access panels (Ref. AMM TASK 54-53-11-400-002):
     (a) For the left pylon:
     (b) For the right pylon:
   (3) Remove the warning notice.
   (4) Remove the access platform.
Subtask 36-11-49-862-091-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 01:10:26 UTC