W DOC AIRBUS | AMM A320F

Installation of the Compressor Pneumatic Overheat-Sensor


TASK 21-61-18-400-001-A
Installation of the Compressor Pneumatic Overheat-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.
FIN: 10HM9 ** ON A/C NOT FOR ALL
FIN: 11HM9 ** 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 1.05 and 0.95 m.daN (92.92 and 84.07 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 [10HM9] (SENSOR-COMPRESSOR PNEUMATIC OVHT)
191KB
FOR [11HM9] (SENSOR-COMPRESSOR PNEUMATIC OVHT)
192KB
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
6
PACKING
AIPC 21-52-41-29-300
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 12-33-21-618-001-A-01
Pre-conditioning through the HP Ground Connection
TASK 12-33-21-618-001-A-02
Pre-conditioning with the APU
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 21-61-18-860-050-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Make sure that:
     (a) The aircraft electrical circuits are energized (Ref. AMM TASK 24-41-00-861-002).
     (b) The access panel is removed (Ref. AMM TASK 53-35-13-000-002):
       1 FOR [10HM9] (SENSOR-COMPRESSOR PNEUMATIC OVHT)
191KB.
       2 FOR [11HM9] (SENSOR-COMPRESSOR PNEUMATIC OVHT)
192KB.
Subtask 21-61-18-865-054-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: 10HM9 (SENSORCOMPRESSOR PNEUMATIC 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: 11HM9 (SENSORCOMPRESSOR PNEUMATIC 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 21-61-18-420-050-A ** ON A/C NOT FOR ALL
A. Installation of the Compressor Pneumatic Overheat-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 (6) is in a good condition. If necessary replace the AIPC 21-52-41-29-300 PACKING (6).
   (3) Remove the blanking plugs from the disconnected line ends.
   (4) Apply a small quantity of Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.
03FAB1) to the screws (3).
   (5) Clean the component interfaces and the adjacent area.
   (6) Put the packing (6) in position on the compressor pneumatic overheat-sensor (5).
   (7) Put the compressor pneumatic overheat-sensor (5) in position in the pipe assembly (1) and install the washers (4) and the screws (3).
   (8) Make sure that the compressor pneumatic overheat-sensor (5) is in the correct position and tighten the screws (3).
   (9) Wipe clean the excess Mineral Oil base Grease-- Vaseline or Petrolatum - (Material No.03FAB1) from the screws (3) and safety with 14QDB1Wire-Locking Dia: 0.5 mm (0.020 inch) CRES Nickel Alloy -.
   (10) Connect the sense line (2).
   (11) TORQUE the sense line (2) connector to between 1.05 and 0.95 m.daN (92.92 and 84.07 lbf.in ) T.
   (12) Make sure that the work area is clean and clear of tools and other items.
Subtask 21-61-18-865-055-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: 10HM9 (SENSORCOMPRESSOR PNEUMATIC 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: 11HM9 (SENSORCOMPRESSOR PNEUMATIC 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 21-61-18-710-050-A ** ON A/C NOT FOR ALL
C. Test
   (1) Do the pre-conditioning through the HP ground connector or with the APU (
Ref. AMM TASK 12-33-21-618-001) (Ref. AMM TASK 12-33-21-618-001).
   (2) Do a leak check of the compressor pneumatic overheat-sensor sense line connection.
NOTE: Leaks are not permitted.
   (3) After approx. 15 minutes stop the pre-conditioning (Ref. AMM TASK 12-33-21-618-001) (Ref. AMM TASK 12-33-21-618-001).
   (4) Do the operational test of the pack temperature control system (Ref. AMM TASK 21-61-00-710-001).
5. Close-up
Subtask 21-61-18-410-051-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 [10HM9] (SENSOR-COMPRESSOR PNEUMATIC OVHT)
     (b) FOR [11HM9] (SENSOR-COMPRESSOR PNEUMATIC OVHT)
Subtask 21-61-18-862-050-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 06:11:38 UTC