W DOC AIRBUS | TSM A320F

Pack 1 Flow Sensor Fault


TASK 21-51-00-810-805-A
Pack 1 Flow Sensor Fault


1. Possible Causes
  • P1 FLOW SENSOR [10HB]
  • P1 CONTROLLER [7HH]
  • wiring
  • pressure sense line
  • P1 FLOW CTL VALVE [11HB]
  • SENSOR-DELTA P, PACK 1 [23HB2]
  • CONT-AIR COND SYSTEM 1 [47HH]
  • FLOW CTL UNIT - PACK 1 [23HB]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ASM 215101
ASM 215102
AMM 21-51-11-000-001
Removal of the Differential Pressure Sensor
AMM 21-51-11-400-001
Installation of the Differential Pressure Sensor
AMM 21-51-51-000-001
Removal of the Pack Flow-Control Valve/ Pack Flow-Control Unit
AMM 21-51-51-400-001
Installation of the Pack Flow-Control Valve/ Pack Flow-Control Unit
AMM 21-61-00-710-001
Operational Test of the Pack Temperature-Control System
AMM 21-61-34-000-001
Removal of the Pack Controller
AMM 21-61-34-000-002
Removal of the Air-Conditioning System Controller
AMM 21-61-34-400-001
Installation of the Pack Controller
AMM 21-61-34-400-002
Installation of the Air-Conditioning System Controller
3. Fault Confirmation
Subtask 21-51-00-710-058-A
A. Do the operational test of the pack temperature-control system AMM 21-61-00-710-001.
4. Fault Isolation
Subtask 21-51-00-810-058-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message P1 FLOW SENSOR:
   (1) If the fault continues:
   (2) If the fault continues:
  • do a check and repair the wiring if necessary between:
    CONNECTOR (7558VC) pin A/A and PC 1 (7HH) connector AB/9C,
    CONNECTOR (7558VC) pin A/D and PC 1 (7HH) connector AB/10C,
    CONNECTOR (7558VC) pin A/C and PC 1 (7HH) connector AB/10B,
    CONNECTOR (7558VC) pin A/B and PC 1 (7HH) connector AB/9D ASM 215101.
   (3) If the fault continues:
   (4) If the fault continues:
Subtask 21-51-00-810-058-C ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message,
P1 FLOW SENSOR(23HB2):
   (1) If the fault continues:
   (2) If the fault continues:
  • do a check and repair the wiring ASM 215102 from:
  • the SENSOR (23HB2) to the ACSC1 (47HH).
   (3) If the fault continues:
Subtask 21-51-00-710-059-A
B. Do the test as given in the Para. 3.A.
5. Close-up
Subtask 21-51-00-860-054-A
A. Put the aircraft back to its initial configuration.
[Rev.8 from Aug 2018] 2026.04.04 04:24:46 UTC