W DOC AIRBUS | AMM A320F

Installation of the Compressor Overheat - Temperature Sensor


TASK 21-61-12-400-001-A
Installation of the Compressor Overheat - Temperature Sensor


WARNING: MAKE SURE THAT AIR IS NOT SUPPLIED TO THE AIR CONDITIONING SYSTEM FROM THE MAIN ENGINE, THE APU OR A GROUND SOURCE. HOT COMPRESSED AIR CAN CAUSE INJURY TO PERSONNEL.
NOTE: The procedure is the same for the compressor overheat temperature sensors 15HH and 35HH.
FIN: 15HH ** ON A/C NOT FOR ALL
FIN: 35HH ** ON A/C NOT FOR ALL
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
Torque wrench: range to between 1.0 and 0.8 m.daN (88.50 and 70.80 lbf.in ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.03FAB1)
Mineral Oil base Grease-- Vaseline or Petrolatum -
(Material No.14QDB1)
Wire-Locking Dia: 0.5 mm (0.020 inch) CRES Nickel Alloy -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [15HH] (SENSOR-COMPRESSOR OVHT)
191KB
FOR [35HH] (SENSOR-COMPRESSOR OVHT)
192KB
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
3
PACKING
AIPC 21-61-03-08-050
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 21-61-00-710-001-A
Operational Test of the Pack Temperature-Control System
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 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 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 53-35-13-000-002-A
Removal of the Quick-Release Access Panels from the Belly Fairing Structure
TASK 53-35-13-400-002-A
Installation of the Quick-Release Access Panels on the Belly Fairing Structure
3. Job Set-up
Subtask 21-61-12-860-050-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).
   (2) Make sure that the access panel/s is are removed (Ref. AMM TASK 53-35-13-000-002).
     (a) FOR [15HH] (SENSOR-COMPRESSOR OVHT)
     (b) FOR [35HH] (SENSOR-COMPRESSOR OVHT)
Subtask 21-61-12-865-055-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
FOR FIN: 15HH (SENSORCOMPRESSOR OVHT)
122VUAIR COND/PACK TEMP/CTL SYS1/1/115VAC1HHX22
122VUAIR COND/PACK TEMP/CTL SYS1/1/28VDC3HHX21
122VUAIR COND/PACK TEMP CTL SYS2/1/28VDC4HHY19
122VUAIR COND/PACK TEMP CTL SYS2/1/115VAC2HHY18
FOR FIN: 35HH (SENSORCOMPRESSOR OVHT)
122VUAIR COND/PACK TEMP/CTL SYS1/2/115VAC21HHW22
122VUAIR COND/PACK TEMP/CTL SYS1/2/28VDC23HHW21
122VUAIR COND/PACK TEMP CTL SYS2/2/28VDC24HHY21
122VUAIR COND/PACK TEMP CTL SYS2/2/115VAC22HHY20
4. Procedure
Subtask 21-61-12-420-050-A ** ON A/C NOT FOR ALL
A. Installation of the Compressor Overheat-Temperature Sensor
   (1) Make sure that the parts retained from the removed component are clean and in the correct condition.
   (2) Make sure that the removed packing (3) is in a good condition. If necessary replace the AIPC 21-61-03-08-050 PACKING (3).
   (3) Remove the blanking plugs from the disconnected line ends.
   (4) Clean the component interfaces and the adjacent area.
   (5) Apply a small quantity of Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.
03FAB1) to the contact faces of the compressor overheat- temperature sensor (1) and to the packing (3).
   (6) Put the packing (3) in position on the compressor overheat-temperature sensor (1).
   (7) Install the compressor overheat-temperature sensor (1) in the pipe assembly (4).
   (8) TORQUE the compressor overheat-temperature sensor (1) to between 1.0 and 0.8 m.daN (88.50 and 70.80 lbf.in ) T.
   (9) Wipe clean the excess Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.
03FAB1) from the compressor overheat-temperature sensor (1) and safety with 14QDB1Wire-Locking Dia: 0.5 mm (0.020 inch) CRES Nickel Alloy -.
   (10) Remove the blanking caps and connect the electrical connector (2).
   (11) Make sure that the work area is clean and clear of tools and other items.
Subtask 21-61-12-865-056-A ** ON A/C NOT FOR ALL
B. 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: 15HH (SENSORCOMPRESSOR OVHT)
122VUAIR COND/PACK TEMP/CTL SYS1/1/115VAC1HHX22
122VUAIR COND/PACK TEMP/CTL SYS1/1/28VDC3HHX21
122VUAIR COND/PACK TEMP CTL SYS2/1/28VDC4HHY19
122VUAIR COND/PACK TEMP CTL SYS2/1/115VAC2HHY18
FOR FIN: 35HH (SENSORCOMPRESSOR OVHT)
122VUAIR COND/PACK TEMP/CTL SYS1/2/115VAC21HHW22
122VUAIR COND/PACK TEMP/CTL SYS1/2/28VDC23HHW21
122VUAIR COND/PACK TEMP CTL SYS2/2/28VDC24HHY21
122VUAIR COND/PACK TEMP CTL SYS2/2/115VAC22HHY20
Subtask 21-61-12-710-050-A ** ON A/C NOT FOR ALL
C. Do the operational test of the pack temperature-control system (Ref. AMM TASK 21-61-00-710-001).
5. Close-up
Subtask 21-61-12-410-051-A ** ON A/C NOT FOR ALL
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the access panel/s (Ref. AMM TASK 53-35-13-400-002).
     (a) FOR [15HH] (SENSOR-COMPRESSOR OVHT)
     (b) FOR [35HH] (SENSOR-COMPRESSOR OVHT)
Subtask 21-61-12-862-050-A ** ON A/C NOT FOR ALL
B. De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:11:37 UTC