W DOC AIRBUS | TSM A320F

Pack 1/2 Inlet Pressure Sensor Fault


TASK 21-51-00-810-824-A
Pack 1/2 Inlet Pressure Sensor Fault


1. Possible Causes
  • SENSOR-PRESS, PACK 1 INLET [23HB1]
  • CONT-AIR COND SYSTEM 1 [47HH]
  • wiring
  • SENSOR-PRESS, PACK 2 INLET [24HB1]
  • CONT-AIR COND SYSTEM 2 [57HH]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 12-33-21-618-001
Pre-conditioning through the LP Ground Connection
AMM 21-51-13-000-001
Removal of the Pack-Inlet Pressure Sensor
AMM 21-51-13-400-001
Installation of the Pack-Inlet Pressure Sensor
ASM 216102
ASM 216104
AMM 21-61-34-000-002
Removal of the Air-Conditioning System Controller
AMM 21-61-34-400-002
Installation of the Air-Conditioning System Controller
AMM 31-32-00-860-002
Procedure to Get Access to the SYSTEM REPORT/TEST/AIR COND Page
3. Fault Confirmation
Subtask 21-51-00-710-085-C ** ON A/C NOT FOR ALL
A. Test
   (1) Do a read out of the POST FLIGHT REPORT.
   (2) Do the pre-conditioning of the air conditioning system with the APU AMM 12-33-21-618-001.
   (3) On one MCDU, get the SYSTEM REPORT/TEST/AIR COND menu page AMM 31-32-00-860-002.
   (4) On the MCDU push the line key adjacent to the TEMP CTL indication.
  • the CAB TEMP CONT menu page comes into view.
   (5) On the CAB TEMP CONT menu page:
  • push the line key adjacent to the SYSTEM DATA indication.
   (6) On the SYSTEM DATA menu page:
  • push the line key adjacent to the PRESS SENSORS indication.
  • the PRESS SENSORS SYSTEM DATA page comes into view.
   (7) On the PRESS SENSORS SYSTEM DATA page:
  • compare the PACK 1 & 2 Bleed Pressure.
NOTE: PACK 1 & 2 Bleed Pressure must be almost equal.
  • compare the pack 1 Pack Inlet Pressure with the pack 1 Bleed Pressure.
  • compare the pack 2 Pack Inlet Pressure with the pack 2 Bleed Pressure.
NOTE: Bleed Pressure and Pack Inlet Pressure must be almost equal for each pack.
   (8) After approximately 4 minutes, stop the pre-conditioning.
4. Fault Isolation
Subtask 21-51-00-810-098-D ** ON A/C NOT FOR ALL
A. If the POST FLIGHT REPORT gives the maintenance message,
P1 PR INL SENS(23HB1)/ P2 PRESS INL SENS(24HB1):
   (1) If the test shows for PACK 1, a large difference between Pack Inlet Pressure and Bleed Pressure:
     (a) If the fault continues:
     (b) If the fault continues:
  • do a check and repair the wiring ASM 216104 from:
  • the PRESSURE SENSOR (23HB1) to the ACSC1 (47HH).
   (2) If the test shows for PACK 2, a large difference between Pack Inlet Pressure and Bleed Pressure:
     (a) If the fault continues:
     (b) If the fault continues:
  • do a check and repair the wiring ASM 216102 from:
  • the PRESSURE SENSOR (24HB1) to the ACSC2 (57HH).
Subtask 21-51-00-720-059-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.
[Rev.8 from Aug 2018] 2026.04.04 04:24:49 UTC