W DOC AIRBUS | AMM A320F

Installation of the Heat-Exchanger Outlet-Temperature Sensor

TASK 36-11-17-400-001-A
Installation of the Heat-Exchanger Outlet-Temperature Sensor

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.
ZONE: 471
ZONE: 481
FIN: 6HA1
FIN: 6HA2
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 3M (10 FT)- ADJUSTABLE
No specific
AR
CAP - BLANKING
No specific
AR
SAFETY BARRIER(S)
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 0.48 and 0.37 m.daN (42.48 and 32.74 lbf.in ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.14QFB1)
Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
471
PYLON LEADING EDGE
481
PYLON LEADING EDGE
471AL, 482AR
471BL, 481BR
FOR [6HA1] (SENSOR-EXCHANGER OUT TEMP, ENG 1)
471AL
471BL
FOR [6HA2] (SENSOR-EXCHANGER OUT TEMP, ENG 2)
482AR
481BR
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
3
O-RING
AIPC 36-11-05-07-140
5
O-RING
AIPC 36-11-05-07-140
5
O-RING
AIPC 36-11-85-01-500
 E. 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 24-41-00-862-002-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 31-60-00-860-001-A
EIS Start Procedure
TASK 36-11-00-720-004-A
Leak Check of Engine Bleed Air Supply System and Packs Components through HPGC
TASK 36-22-00-790-802-A
Leak Check on all the Bleed Air Ducts and the Packs Components
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))
F Heat-Exchanger Outlet-Temperature Sensor ** ON A/C NOT FOR ALL
F Heat-Exchanger Outlet-Temperature Sensor ** ON A/C NOT FOR ALL
F Heat-Exchanger Outlet-Temperature Sensor ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 36-11-17-941-052-A
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).
WARNING: MAKE SURE THAT THE PNEUMATIC SYSTEM IS DEPRESSURIZED BEFORE YOU START WORK. PRESSURIZED AIR CAN CAUSE INJURY TO PERSONNEL.
   (2) Make sure that the SAFETY BARRIER(S) are in position.
   (3) Make sure that on AIR COND panel 30VU, the ENG pushbutton switches are released (the OFF legends are on).
   (4) Make sure that the WARNING NOTICE(S) are in position in the cockpit to tell persons not to:
  • Operate the engines
  • Operate the slats
  • Operate the APU switch
  • Operate the pneumatic system.
Subtask 36-11-17-860-050-A ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is below the applicable access panel 471AL or 482AR.
   (2) Make sure that the applicable access panel is removed:
     (a) FOR [6HA1] (SENSOR-EXCHANGER OUT TEMP, ENG 1)
remove 471AL.
     (b) FOR [6HA2] (SENSOR-EXCHANGER OUT TEMP, ENG 2)
remove 482AR.
Subtask 36-11-17-860-050-B ** ON A/C NOT FOR ALL
B. Aircraft Maintenance Configuration
   (1) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is below the applicable access panel 471BL or 481BR.
   (2) Make sure that the applicable access panel is removed:
     (a) FOR [6HA1] (SENSOR-EXCHANGER OUT TEMP, ENG 1)
     (b) FOR [6HA2] (SENSOR-EXCHANGER OUT TEMP, ENG 2)
Subtask 36-11-17-865-051-A
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 6HA1 (SENSOREXCHANGER OUT TEMP, ENG 1)
49VUAIR BLEED/ENG 1/CTL3HA1D12
49VUAIR BLEED/ENG 1/MONG2HA1D11
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 1/CTL2HA1D11
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
** ON A/C NOT FOR ALL
122VUAIR BLEED/ENG 1/MONG3HA1Z23
** ON A/C NOT FOR ALL
FOR FIN: 6HA2 (SENSOREXCHANGER OUT TEMP, ENG 2)
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 2/MONG3HA2D12
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
** ON A/C NOT FOR ALL
122VUAIR BLEED/ENG 2/CTL3HA2Z23
122VUAIR BLEED/ENG 2/MONG2HA2Z22
** ON A/C NOT FOR ALL
122VUAIR BLEED/ENG 2/CTL2HA2Z22
4. Procedure
Subtask 36-11-17-420-051-A ** ON A/C NOT FOR ALL
A. Preparation for the Installation
   (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) Clean the component interface and/or the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
   (4) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (5) Do an inspection of the component interfaces and the adjacent area.
Subtask 36-11-17-420-050-A ** ON A/C NOT FOR ALL
B. Installation of the Heat-Exchanger Outlet-Temperature Sensor
   (1) Remove the CAP - BLANKING from the:
  • The temperature sensor (2)
  • The sensor location on the air-bleed duct
  • The electrical connector (1).
   (2) Install the temperature sensor (2) with the new AIPC 36-11-05-07-140 O-RING (3).
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) Safety the temperature sensor (2) with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
   (4) Connect the electrical connector (1) to the temperature sensor (2).
Subtask 36-11-17-420-051-B ** ON A/C NOT FOR ALL
C. Preparation for the Installation
   (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) Clean the component interface and/or the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
   (4) Remove the CAP - BLANKING from:
  • The temperature sensor (1)
  • The sensor location on the air-bleed duct
  • The electrical connectors (3) and (4).
   (5) Make sure that the socket grommets on the electrical connectors (3) and (4) are clean and serviceable.
   (6) Examine the condition of the temperature sensor (1) and make sure that:
  • There is no corrosion
  • There is no contamination
  • There are no bent pins
  • The sensor tubes are clean and serviceable.
Subtask 36-11-17-420-050-B ** ON A/C NOT FOR ALL
D. Installation of the Heat-Exchanger Outlet-Temperature Sensor
   (1) Install the new AIPC 36-11-05-07-140 O-RING (5) or the new AIPC 36-11-85-01-500 O-RING (5) on the temperature sensor (1).
   (2) Install the temperature sensor (1) with the screws (2).
   (3) TORQUE the screws (2) to between 0.48 and 0.37 m.daN (42.48 and 32.74 lbf.in ) T.
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.
   (4) Safety the screws (2) with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
   (5) Connect the electrical connectors (3) and (4) to the temperature sensor (1).
   (6) Tighten the electrical connectors (3) and (4) until you cannot see the witness line of the socket.
Subtask 36-11-17-865-052-A
E. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 6HA1 (SENSOREXCHANGER OUT TEMP, ENG 1)
49VUAIR BLEED/ENG 1/CTL3HA1D12
49VUAIR BLEED/ENG 1/MONG2HA1D11
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 1/CTL2HA1D11
122VUAIR BLEED/ENG 1/MONG3HA1Z23
FOR FIN: 6HA2 (SENSOREXCHANGER OUT TEMP, ENG 2)
49VUAIR BLEED/ENG 2/MONG3HA2D12
** ON A/C NOT FOR ALL
122VUAIR BLEED/ENG 2/CTL3HA2Z23
122VUAIR BLEED/ENG 2/MONG2HA2Z22
** ON A/C NOT FOR ALL
122VUAIR BLEED/ENG 2/CTL2HA2Z22
Subtask 36-11-17-750-050-A
F. Test
   (1) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
   (2) On panel 11VU, push the BLEED pushbutton switch.
   (3) On the lower ECAM display unit, make sure that you can see the BLEED air temperature (no amber XX).
   (4) On AIR COND panel 30VU, push the ENG pushbutton switches (the OFF legend is off).
Subtask 36-11-17-790-050-A ** ON A/C NOT FOR ALL
G. Functional Test
   (1) Do a functional test of the engine bleed air supply system:
Subtask 36-11-17-790-050-C ** ON A/C NOT FOR ALL
G. Functional Test
   (1) Do a check for the correct installation:
     (a) Make sure that the screws (2) are torqued and safetied with the 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
   (2) Do a functional test of the engine bleed air supply system:
     (a) Make sure that there are no leaks from the temperature sensor connections (Ref. AMM TASK 36-22-00-790-802).
5. Close-up
Subtask 36-11-17-865-053-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
Subtask 36-11-17-410-050-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 the applicable access panel:
     (a) FOR [6HA1] (SENSOR-EXCHANGER OUT TEMP, ENG 1)
install 471AL.
     (b) FOR [6HA2] (SENSOR-EXCHANGER OUT TEMP, ENG 2)
install 482AR.
Subtask 36-11-17-410-050-B ** 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 the applicable access panel:
     (a) FOR [6HA1] (SENSOR-EXCHANGER OUT TEMP, ENG 1)
     (b) FOR [6HA2] (SENSOR-EXCHANGER OUT TEMP, ENG 2)
Subtask 36-11-17-942-050-A
C. Removal of Equipment
   (1) Remove the safety barriers
   (2) Remove the WARNING NOTICE(S).
   (3) Remove the access platform(s).
   (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
Subtask 36-11-17-862-050-A
D. De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002) (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.01 01:08:45 UTC
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