W DOC AIRBUS | TSM A320F

Loss of the FMV Torque Motor Control through the Channel A on Engine 1


TASK 73-29-00-810-868-A
Loss of the FMV Torque Motor Control through the Channel A on Engine 1


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 73-21-50-000-006
Removal of J7 Harness
AMM 73-21-50-000-040
Removal of the HJ7 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 73-21-50-400-006
Installation of the J7 Harness
AMM 73-21-50-400-040
Installation of the HJ7 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)
3. Fault Confirmation
Subtask 73-29-00-710-152-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the operational test of the FADEC 1A on the ground (with engine non - motoring) AMM 73-29-00-710-040.
4. Fault Isolation
Subtask 73-29-00-810-160-A ** ON A/C NOT FOR ALL
A. Do this procedure:
NOTE: This fault is generated if there is an open or short to ground in the torque motor current loop on channel A.
   (1) If the test does not give the maintenance message J7, HMU(FMV TM), ECU:
  • No maintenance action is required.
   (2) If the test does not give the maintenance message J7, HMU(FMV TM), ECU, but is repetitive:
     (a) If the fault continues during the subsequent flights:
       1 If the fault continues during the subsequent flights:
   (3) If the test gives the maintenance message J7, HMU(FMV TM), ECU:
  • Disconnect the J7 harness from the ECU (4000KS) receptacle and visually examine it and the J7 harness connector for damaged pins, contamination AMM 73-21-50-210-001.
     (a) If damage on a connector is found:
  • Replace or repair as required.
     (b) If nothing is found:
  • Do an electrical resistance test through the J7 harness between:
    . pins 27 and 28 (17 to 23 Ohms)
    . pins 27 and 12 (> 10 Megohms)
    . pin 27 and the ground (> 10 Megohms).
       1 If the resistance values are in the specified limits:
       2 If the resistance values are out of the specified limits:
  • Reconnect the J7 harness to the ECU (4000KS) receptacle, and continue the troubleshooting.
     (c) Disconnect the J7 harness from the HMU receptacle (HMU-A) (located left hand core compartment), and visually examine the J7 harness connector and the HMU receptacle for damaged pins, contamination and fuel wetting AMM 73-21-50-210-001.
       1 If damage on a connector is found:
  • Replace or repair as required.
       2 If fuel wetting is found:
       3 If nothing is found:
  • Do an electrical resistance test on the HMU receptacle between:
    . pins 27 and 28 (17 to 23 Ohms)
    . pins 27 and 12 (> 10 Megohms)
    . pin 27 and the ground (> 10 Megohms).
         a If the resistance values are in the specified limits:
         b If the resistance values are out of the specified limits:
Subtask 73-29-00-810-160-B ** ON A/C NOT FOR ALL
A. Do this procedure:
NOTE: This fault is generated if there is an open or short to ground in the torque motor current loop on channel A.
   (1) If the test does not give the maintenance message J7, HMU(FMV TM), ECU:
  • No maintenance action is required.
   (2) If the test does not give the maintenance message J7, HMU(FMV TM), ECU, but is repetitive:
     (a) If the fault continues during the subsequent flights:
       1 If the fault continues during the subsequent flights:
   (3) If the test gives the maintenance message J7, HMU(FMV TM), ECU:
  • Disconnect the J7 harness from the ECU (4000KS) receptacle and visually examine it and the J7 harness connector for damaged pins, contamination AMM 73-21-50-210-002.
     (a) If damage on a connector is found:
  • Replace or repair as required.
     (b) If nothing is found:
  • Do an electrical resistance test through the J7 harness between:
    . pins 27 and 28 (17 to 23 Ohms)
    . pins 27 and 12 (> 10 Megohms)
    . pin 27 and the ground (> 10 Megohms).
       1 If the resistance values are in the specified limits:
       2 If the resistance values are out of the specified limits:
  • Reconnect the J7 harness to the ECU (4000KS) receptacle, and continue the troubleshooting.
     (c) Disconnect the J7 harness from the HMU receptacle (HMU-A) (located left hand core compartment), and visually examine the J7 harness connector and the HMU receptacle for damaged pins, contamination and fuel wetting AMM 73-21-50-210-002.
       1 If damage on a connector is found:
  • Replace or repair as required.
       2 If fuel wetting is found:
       3 If nothing is found:
  • Do an electrical resistance test on the HMU receptacle between:
    . pins 27 and 28 (17 to 23 Ohms)
    . pins 27 and 12 (> 10 Megohms)
    . pin 27 and the ground (> 10 Megohms).
         a If the resistance values are in the specified limits:
         b If the resistance values are out of the specified limits:
Subtask 73-29-00-710-153-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.(1).
   (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 04:35:59 UTC