W DOC AIRBUS | TSM A320F

Loss of the A/THR Control on Engine 1


TASK 71-50-00-810-822-A
Loss of the A/THR Control on Engine 1


1. Possible Causes
  • RELAY-A/THR1 INST DISC [5CA1]
  • harness J3
  • ECU [4000KS]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 71-51-43-000-044
Removal of the Thrust Reverser (Channel A and B) Harness
AMM 71-51-43-400-044
Installation of the Thrust Reverser (Channel A and B) Harness
AMM 71-51-44-000-004
Removal of the Electronic Control Unit (ECU) Channel A Harness 238W0904
AMM 71-51-44-400-004
Installation of the Electronic Control Unit (ECU) Channel A Harness 238W0904
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)
ASM 732512
AMM 73-29-00-710-040
Operational Test of the FADEC on the ground (with Engine Motoring)
3. Fault Confirmation
Subtask 71-50-00-710-086-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the operational test of the FADEC 1B on the ground (with engine non motoring) AMM 73-29-00-710-040.
4. Fault Isolation
Subtask 71-50-00-810-074-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message J3:
  • do a visual check of the connector J3 at the ECU (4000KS) for integrity ASM 732512.
   (1) If the fault continues:
  • do a check for open circuit at the harness J3 between pins 6 and 31.
   (2) If the fault continues:
   (3) If the fault continues:
   (4) If the fault continues:
Subtask 71-50-00-810-074-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message J3 (INSTINCT DISC):
  • do a visual check of the connector J3 at the ECU (4000KS) for integrity ASM 732512.
   (1) If the fault continues:
  • do a check for open circuit at the harness J3 between pins 6 and 31.
   (2) If the fault continues:
   (3) If the fault continues:
   (4) If the fault continues:
Subtask 71-50-00-810-074-C ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message J3 (INSTINCT DISC):
  • do a visual check of the connector J3 at the ECU (4000KS) for integrity ASM 732512.
   (1) If the fault continues:
  • do a check for open circuit at the harness J3 between pins 6 and 31.
   (2) If the fault continues:
   (3) If the fault continues:
   (4) If the fault continues:
Subtask 71-50-00-710-087-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.
[Rev.8 from Aug 2018] 2026.04.04 04:34:59 UTC