W DOC AIRBUS | TSM A320F

Failure of the HMU Torque Motor of the HPTCC Valve on Engine 1


TASK 75-21-00-810-805-A
Failure of the HMU Torque Motor of the HPTCC Valve on Engine 1


1. Possible Causes
  • High Pressure Turbine Clearance Control (HPTCC) valve
  • HMU-1 [4000KC1]
  • ECU [4000KS]
2. Job Set-up Information
 A. Consumable Materials
REFERENCE
DESIGNATION
(Material No.CP2011)
stoddard solvent
 B. Referenced Information
REFERENCE
DESIGNATION
AMM 73-21-10-000-001
Removal of the Hydromechanical Unit (HMU)
AMM 73-21-10-000-002
Removal of the Hydromechanical Unit (HMU)
AMM 73-21-10-400-001
Installation of the Hydromechanical Unit (HMU)
AMM 73-21-10-400-002
Installation of the Hydromechanical Unit (HMU)
AMM 73-21-50-210-001
Visual Inspection of the Wiring Harness
AMM 73-21-60-000-001
Removal of the Electronic Control Unit (ECU)
AMM 73-21-60-400-001
Installation of the Electronic Control Unit (ECU)
AMM 73-29-00-710-040
Operational Test of the FADEC on the ground (with Engine Motoring)
AMM 75-21-10-000-001
Removal of the High Pressure Turbine Active Clearance Control (HPTACC) Valve
AMM 75-21-10-000-002
Removal of the High Pressure Turbine Active Clearance Control (HPTACC) Valve
AMM 75-21-10-400-001
Installation of the High Pressure Turbine Active Clearance Control (HPTACC) Valve
AMM 75-21-10-400-002
Installation of the High Pressure Turbine Active Clearance Control (HPTACC) Valve
3. Fault Confirmation
Subtask 75-21-00-710-058-A ** ON A/C NOT FOR ALL
A. Do the operational test of the FADEC 1A on the ground (with engine motoring) AMM 73-29-00-710-040.
Subtask 75-21-00-710-058-B ** ON A/C NOT FOR ALL
A. Do the operational test of the FADEC 1A on the ground (with engine motoring) AMM 73-29-00-710-040.
4. Fault Isolation
Subtask 75-21-00-810-056-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message HPTC VLV (BLD), HMU:
   (1) If the fault continues:
   (2) If the fault continues:
Subtask 75-21-00-810-056-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message HPTC VLV (BLD), HMU:
  • disconnect the CJ13 connector (TCC-A) from the TCC sensor (9 O'Clock).
  • visually examine the harness connector and sensor receptacle for damaged pins or contamination/oxidation.
  • if damage is found, repair or replace as required.
  • do a cleaning of the connector and receptacle using a bristle brush with stoddard solvent (Material No.CP2011) AMM 73-21-50-210-001.
  • connect the harness connector to the sensor. Tighten the connector by hand plus one eighth of a turn. If necessary use soft nose pliers.
   (1) If the fault continues:
   (2) If the fault continues:
   (3) If the fault continues:
Subtask 75-21-00-710-059-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.
[Rev.8 from Aug 2018] 2026.04.04 04:37:01 UTC