Failure of the LPTC Valve on Engine 1
TASK 75-22-00-810-805-A
Failure of the LPTC Valve on Engine 1
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 75-22-00-710-058-A ** ON A/C NOT FOR ALL
Subtask 75-22-00-810-054-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:37:03 UTC
Failure of the LPTC Valve on Engine 1
1. Possible Causes
- LPTC valve
- HMU
- ECU [4000KS]
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 |
Subtask 75-22-00-710-058-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.
4. Fault IsolationSubtask 75-22-00-810-054-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:
(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:
(a) Replace the LPTC valve AMM 75-22-10-000-001 and AMM 75-22-10-400-001.
(b) If the fault continues:
Subtask 75-22-00-810-054-B ** ON A/C NOT FOR ALL (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:
- replace the HMU AMM 73-21-10-000-001 and AMM 73-21-10-400-001.
- replace the ECU [4000KS] AMM 73-21-60-000-001 and AMM 73-21-60-400-001.
(a) Replace the LPTC valve AMM 75-22-10-000-001 and AMM 75-22-10-400-001.
(b) If the fault continues:
- replace the HMU AMM 73-21-10-000-001 and AMM 73-21-10-400-001.
- replace the ECU (4000KS) AMM 73-21-60-000-001 and AMM 73-21-60-400-001.
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:
(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:
(a) Replace the LPTC valve AMM 75-22-10-000-001 and AMM 75-22-10-400-001.
(b) If the fault continues:
Subtask 75-22-00-810-054-C ** ON A/C NOT FOR ALL (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:
- replace the HMU AMM 73-21-10-000-001 and AMM 73-21-10-400-001.
- replace the ECU [4000KS] AMM 73-21-60-000-001 and AMM 73-21-60-400-001.
(a) Replace the LPTC valve AMM 75-22-10-000-001 and AMM 75-22-10-400-001.
(b) If the fault continues:
- replace the HMU AMM 73-21-10-000-001 and AMM 73-21-10-400-001.
- replace the ECU (4000KS) AMM 73-21-60-000-001 and AMM 73-21-60-400-001.
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:
(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:
(a) Replace the LPTC valve AMM 75-22-10-000-002 and AMM 75-22-10-400-002.
(b) If the fault continues:
Subtask 75-22-00-710-059-A ** ON A/C NOT FOR ALL (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:
- replace the HMU AMM 73-21-10-000-002 and AMM 73-21-10-400-002.
- replace the ECU [4000KS] AMM 73-21-60-000-001 and AMM 73-21-60-400-001.
(a) Replace the LPTC valve AMM 75-22-10-000-002 and AMM 75-22-10-400-002.
(b) If the fault continues:
- replace the HMU AMM 73-21-10-000-002 and AMM 73-21-10-400-002.
- replace the ECU (4000KS) AMM 73-21-60-000-001 and AMM 73-21-60-400-001.
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.
(1) No additional maintenance action is required if the fault is not confirmed.
(2) Repeat the fault isolation procedure if the fault continues.