W DOC AIRBUS | TSM A320F

Loss of the Feedback Signal from the LPTC Valve - Engine 1 - Channel A

TASK 75-22-00-810-801-A
Loss of the Feedback Signal from the LPTC Valve - Engine 1 - Channel A

1. Possible Causes
  • LPTC valve
  • ECU [4000KS]
  • harness J11
  • harness CJ11R
  • harness HJ11
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 73-21-50-000-002
Removal of the CJ11R Harness
AMM 73-21-50-000-010
Removal of the J11 Harness
AMM 73-21-50-000-026
Removal of the CJ11R Harness for SAC Engines
AMM 73-21-50-000-044
Removal of the HJ11 Harness for SAC Engines
AMM 73-21-50-210-001
Visual Inspection of the Wiring Harness
AMM 73-21-50-210-002
Visual Inspection of the Wiring Harnesses
AMM 73-21-50-400-002
Installation of the CJ11R Harness
AMM 73-21-50-400-010
Installation of the J11 Harness
AMM 73-21-50-400-026
Installation of the CJ11R Harness for SAC Engines
AMM 73-21-50-400-044
Installation of the HJ11 Harness for SAC Engines
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 75-22-00-710-050-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 Isolation
Subtask 75-22-00-810-050-A ** ON A/C NOT FOR ALL
A. The fault message is generated if the channel A signal is invalid, out of range.
   (1) If the failure message LPTC VLV, J11, ECU is not confirmed:
     (a) no maintenance action is required.
   (2) If the failure message LPTC VLV, J11, ECU is not confirmed but is repetitive:
  • disconnect the CJ11R harness (LPT-A) connector (located in the right core compartment) from the LPTC valve and visually examine the receptacles and the connectors for damaged pins or contamination AMM 73-21-50-210-001.
     (a) If damage is found:
  • repair or replace as required.
     (b) If no dammage is found:
     (c) If the fault continues during the subsequent flights:
     (d) If the fault continues during the subsequent flights:
     (e) If the fault continues during the subsequent flights:
   (3) If the failure message LPTC VLV, J11, ECU is confirmed:
  • disconnect the CJ11R harness (LPT-A) connector (located in the right core compartment) from the LPTC valve and visually examine the CJ11R wire harness connector receptacles and the LPTC valve connectors for damaged pins or contamination AMM 73-21-50-210-001.
     (a) If damage is found:
  • repair or replace as required.
     (b) If no damage is found:
  • do an electrical resistance test through the LPTC valve between:
    . pins 2 and 3 (80 to 109.5 ohms)
    . pins 4 and 5 (85 to 115 ohms)
    . pins 6 and 7 (85 to 115 ohms)
    . pin 2 and the ground (> 10 megohms)
    . pin 4 and the ground (> 10 megohms)
    . pin 6 and the ground (> 10 megohms).
     (c) If the resistance values are out of the specified limits:
     (d) If the resistance values are in the specified limits:
  • reconnect the CJ11R harness (LPT-A) connector to the LPTC valve,
  • disconnect the J11 harness (channel A) from the ECU (4000KS) and visually examine the receptacle for damaged pins or contamination AMM 73-21-50-210-001.
       1 If damage is found:
  • repair or replace as required.
       2 If no damage is found:
  • do an electrical resistance test through the J11 harness between:
    . pins 4 and 5 (80 to 109.5 ohms)
    . pins 6 and 7 (85 to 115 ohms)
    . pins 2 and 3 (85 to 115 ohms)
    . pins 4 and 1 (> 10 megohms)
    . pins 6 and 1 (> 10 megohms)
    . pins 2 and 1 (> 10 megohms)
    . pin 4 and the ground (> 10 megohms)
    . pin 6 and the ground (> 10 megohms)
    . pin 2 and the ground (> 10 megohms).
       3 If the resistance values are in the specified limits:
       4 If the resistance values are out of the specified limits:
  • disconnect the J11 harness from the CJ11R harness located at the 6 o'clock junction box and do an electrical resistance test through the CJ11R harness between:
    . pins 20 and 21 (80 to 109.5 ohms)
    . pins 7 and 19 (85 to 115 ohms)
    . pins 2 and 9 (85 to 115 ohms)
    . pins 20 and 8 (> 10 megohms)
    . pins 7 and 8 (> 10 megohms)
    . pins 2 and 8 (> 10 megohms)
    . pin 20 and the ground (> 10 megohms)
    . pin 7 and the ground (> 10 megohms)
    . pin 2 and the ground (> 10 megohms).
       5 If the resistance values are in the specified limits:
       6 If the resistance values are out of the specified limits:
Subtask 75-22-00-810-050-B ** ON A/C NOT FOR ALL
A. The fault message is generated if the channel A signal is invalid, out of range.
   (1) If the failure message LPTC VLV, J11, ECU is not confirmed:
     (a) No maintenance action is required.
   (2) If the failure message LPTC VLV, J11, ECU is not confirmed but is repetitive:
  • disconnect the CJ11R harness (LPT-A) connector (located in the right core compartment) from the LPTC valve and visually examine the receptacles and the connectors for damaged pins or contamination AMM 73-21-50-210-002.
     (a) If damage is found:
  • repair or replace as required.
     (b) If no damage is found:
     (c) If the fault continues during the subsequent flights:
     (d) If the fault continues during the subsequent flights:
     (e) If the fault continues during the subsequent flights:
   (3) If the failure message LPTC VLV, J11, ECU is confirmed:
  • disconnect the CJ11R harness (LPT-A) connector (located in the right core compartment) from the LPTC valve and visually examine the CJ11R wire harness connector receptacles and the LPTC valve connectors for damaged pins or contamination AMM 73-21-50-210-002.
     (a) If damage is found:
  • repair or replace as required.
     (b) If no damage is found:
  • do an electrical resistance test through the LPTC valve between:
    . pins 2 and 3 (80 to 109.5 ohms)
    . pins 4 and 5 (85 to 115 ohms)
    . pins 6 and 7 (85 to 115 ohms)
    . pin 2 and the ground (> 10 megohms)
    . pin 4 and the ground (> 10 megohms)
    . pin 6 and the ground (> 10 megohms).
     (c) If the resistance values are out of the specified limits:
     (d) If the resistance values are in the specified limits:
  • reconnect the CJ11R harness (LPT-A) connector to the LPTC valve,
  • disconnect the HJ11 harness (channel A) from the ECU (4000KS) and visually examine the receptacle for damaged pins or contamination AMM 73-21-50-210-002.
       1 If damage is found:
  • repair or replace as required.
       2 If no damage is found:
  • do an electrical resistance test through the HJ11 harness between:
    . pins 4 and 5 (80 to 109.5 ohms)
    . pins 6 and 7 (85 to 115 ohms)
    . pins 2 and 3 (85 to 115 ohms)
    . pins 4 and 1 (> 10 megohms)
    . pins 6 and 1 (> 10 megohms)
    . pins 2 and 1 (> 10 megohms)
    . pin 4 and the ground (> 10 megohms)
    . pin 6 and the ground (> 10 megohms)
    . pin 2 and the ground (> 10 megohms).
       3 If the resistance values are in the specified limits:
       4 If the resistance values are out of the specified limits:
  • disconnect the HJ11 harness from the CJ11R harness located at the 6 o'clock junction box and do an electrical resistance test through the CJ11R harness between:
    . pins 20 and 21 (80 to 109.5 ohms)
    . pins 7 and 19 (85 to 115 ohms)
    . pins 2 and 9 (85 to 115 ohms)
    . pins 20 and 8 (> 10 megohms)
    . pins 7 and 8 (> 10 megohms)
    . pins 2 and 8 (> 10 megohms)
    . pin 20 and the ground (> 10 megohms)
    . pin 7 and the ground (> 10 megohms)
    . pin 2 and the ground (> 10 megohms).
       5 If the resistance values are in the specified limits:
       6 If the resistance values are out of the specified limits:
Subtask 75-22-00-710-051-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 04:37:02 UTC
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