W DOC AIRBUS | AMM A320F

Installation of the Bleed-Air Precooler-Exchanger Cold-Inlet


TASK 36-11-44-400-802-A
Installation of the Bleed-Air Precooler-Exchanger Cold-Inlet


WARNING: MAKE SURE THAT THE PNEUMATIC SYSTEM IS DEPRESSURIZED BEFORE YOU START WORK. PRESSURIZED AIR CAN CAUSE INJURY TO PERSONNEL.
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.
WARNING: ALWAYS USE APPLICABLE GLOVES TO TOUCH HOT PARTS. HOT PARTS CAN CAUSE INJURY TO PERSONS.
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.
CAUTION: BE VERY CAREFUL WHEN YOU DO WORK ON OR NEAR THE AIR-CONDITIONING DUCTS. THE DUCTS ARE MADE OF THIN MATERIAL AND YOU CAN EASILY BREAK THEM.
ZONE: 413
ZONE: 423
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE
No specific
AR
WARNING NOTICE(S)
98L12003001000
AR
HARNESS,SAFETY
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
413
UPPER FWD PYLON
423
UPPER FWD PYLON
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
413DT, 413ET
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
423DT, 423ET
 C. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
2
SEAL
AIPC 36-11-86-01-390
1
DIFFUSER
AIPC 36-11-86-01-400
2
SEAL
AIPC 36-11-86-02-390
1
DIFFUSER
AIPC 36-11-86-02-400
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 12-00-00-481-002-A
Installation of the Wingrip
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 36-11-42-400-802-A
Installation of the Bleed-Air Precooler Exchanger
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 71-00-00-860-833-A
Procedure to Prevent Engine Motoring
3. Job Set-up
Subtask 36-11-44-860-051-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (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) On the overhead panel, on the AIR section of panel 30VU:
  • Make sure that the APU BLEED pushbutton switch is released (ON legend off).
  • Make sure that the ENG BLEED pushbutton switch is released (OFF legend on).
  • Make sure that a WARNING NOTICE(S) is in position to tell persons not to operate the APU and the engine bleed-air systems.
   (3) Make sure that you did the procedure to prevent engine motoring
(Ref. AMM TASK 71-00-00-860-833).
   (4) On the HP ground connectors:
  • Make sure that a WARNING NOTICE(S) is in position to tell persons not to pressurize the pneumatic system.
   (5) Put on and attach a 98L12003001000 HARNESS,SAFETY before you start work in the work area (Ref. AMM TASK 12-00-00-481-002).
Subtask 36-11-44-865-056-A ** ON A/C NOT FOR ALL
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 2/MONG3HA2D12
49VUAIR BLEED/ENG 1/CTL2HA1D11
122VUAIR BLEED/ENG 1/MONG3HA1Z23
122VUAIR BLEED/ENG 2/CTL2HA2Z22
Subtask 36-11-44-010-061-A ** ON A/C NOT FOR ALL
C. Aircraft Maintenance Configuration
   (1) Make sure that an ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE is in position
   (2) Make sure that these access panels are removed:
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
413DT 413ET
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
423DT 423ET
4. Procedure
Subtask 36-11-44-420-051-A ** ON A/C NOT FOR ALL
A. Installation of the Bleed-Air Precooler-Exchanger Cold-Inlet
   (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) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (4) Do a visual inspection of the seals (2) and (4) of the bleed-air precooler-exchanger cold-inlet (1):
   (5) Install the seal (4) on the fan air valve (5).
   (6) Install the seal (2) on the structure (3).
   (7) Put the bleed-air precooler-exchanger cold-inlet (1) in position on the fan air valve (5) through the structure (3).
   (8) Make sure that there is no clearance between the bleed-air precooler-exchanger cold-inlet (1) and the seal (2).
   (9) Install the bleed-air precooler-exchanger (
Ref. AMM TASK 36-11-42-400-802).
5. Close-up
Subtask 36-11-44-865-057-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 2/MONG3HA2D12
49VUAIR BLEED/ENG 1/CTL2HA1D11
122VUAIR BLEED/ENG 1/MONG3HA1Z23
122VUAIR BLEED/ENG 2/CTL2HA2Z22
Subtask 36-11-44-410-055-A ** ON A/C NOT FOR ALL
B. Install these access panels:
   (1) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
413DT 413ET
   (2) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
423DT 423ET
Subtask 36-11-44-410-057-A ** ON A/C NOT FOR ALL
C. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove all the fixtures, tools, test and support equipment used during this procedure.
   (3) Remove the access platform(s).
   (4) Remove the WARNING NOTICE(S).
Subtask 36-11-44-862-052-A ** ON A/C NOT FOR ALL
D. 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 01:09:33 UTC