W DOC AIRBUS | TSM A320F

Failure of the LPTC Valve on Engine 2


TASK 75-22-00-810-806-A
Failure of the LPTC Valve on Engine 2


1. Possible Causes
2. Job Set-up Information
 A. 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 73-21-60-000-001
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 75-22-10-000-001
Removal of the Low Pressure Turbine Active Clearance Control Valve (LPTACC).
AMM 75-22-10-000-002
Removal of the Low Pressure Turbine Active Clearance Control (LPTACC) Valve
AMM 75-22-10-400-001
Installation of the Low Pressure Turbine Active Clearance Control Valve (LPTACC).
AMM 75-22-10-400-002
Installation of the Low Pressure Turbine Active Clearance Control (LPTACC) Valve
3. Fault Confirmation
Subtask 75-22-00-710-060-A ** ON A/C NOT FOR ALL
A. Do the operational test of the FADEC 2A on the ground (with engine motoring) AMM 73-29-00-710-040.
4. Fault Isolation
Subtask 75-22-00-810-055-A ** ON A/C NOT FOR ALL
A. This fault is generated if the actual valve position disagrees with the demanded valve position for a set time interval.
   (1) If the failure message LPTC VLV, HMU is not confirmed:
     (a) No maintenance action is required.
   (2) If the failure message LPTC VLV, HMU is not confirmed but is repetitive:
NOTE: No maintenance action is required unless the fault becomes too repetitive.
- do the following steps until the fault is corrected.
     (a) Replace the LPTC valve AMM 75-22-10-000-001 and AMM 75-22-10-400-001.
     (b) If the fault continues during the subsequent flights:
     (c) If the fault continues during the subsequent flights:
   (3) If the failure message LPTC VLV, HMU is confirmed:
     (a) Replace the LPTC valve AMM 75-22-10-000-001 and AMM 75-22-10-400-001.
     (b) If the fault continues:
     (c) If the fault continues:
Subtask 75-22-00-810-055-B ** ON A/C NOT FOR ALL
A. This fault is generated if the actual valve position disagrees with the demanded valve position for a set time interval.
   (1) If the failure message LPTC VLV (POS), HMU is not confirmed:
     (a) No maintenance action is required.
   (2) If the failure message LPTC VLV (POS), HMU is not confirmed but is repetitive:
NOTE: No maintenance action is required unless the fault becomes too repetitive.
- do the following steps until the fault is corrected.
     (a) Replace the LPTC valve AMM 75-22-10-000-001 and AMM 75-22-10-400-001.
     (b) If the fault continues during the subsequent flights:
     (c) If the fault continues during the subsequent flights:
   (3) If the failure message LPTC VLV (POS), HMU is confirmed:
     (a) Replace the LPTC valve AMM 75-22-10-000-001 and AMM 75-22-10-400-001.
     (b) If the fault continues:
     (c) If the fault continues:
Subtask 75-22-00-810-055-C ** ON A/C NOT FOR ALL
A. This fault is generated if the actual valve position disagrees with the demanded valve position for a set time interval.
   (1) If the failure message LPTC VLV (POS), HMU is not confirmed:
     (a) No maintenance action is required.
   (2) If the failure message LPTC VLV (POS), HMU is not confirmed but is repetitive:
NOTE: No maintenance action is required unless the fault becomes too repetitive.
- do the following steps until the fault is corrected.
     (a) Replace the LPTC valve AMM 75-22-10-000-002 and AMM 75-22-10-400-002.
     (b) If the fault continues during the subsequent flights:
     (c) If the fault continues during the subsequent flights:
   (3) If the failure message LPTC VLV (POS), HMU is confirmed:
     (a) Replace the LPTC valve AMM 75-22-10-000-002 and AMM 75-22-10-400-002.
     (b) If the fault continues:
     (c) If the fault continues:
Subtask 75-22-00-710-061-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.
   (1) No additional maintenance action is required if the fault is not confirmed.
   (2) Repeat the fault isolation procedure if the fault continues.
[Rev.8 from Aug 2018] 2026.04.04 04:37:03 UTC