W DOC AIRBUS | TSM A320F

Loss of all Engine 2 Indication Plug Data

TASK 73-20-00-810-840-A
Loss of all Engine 2 Indication Plug Data

1. Possible Causes
  • wiring and the connector J14 at the ECU 2 (4000KS)
  • ECU [4000KS]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
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 73-20-00-710-102-A ** ON A/C NOT FOR ALL
A. Do the operational test of the FADEC 2A on the ground (with engine non motoring) AMM 73-29-00-710-040.
4. Fault Isolation
Subtask 73-20-00-810-091-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message J14, ECU:
  • reset the ECU 2 as follows:
   (1) On the panel 115VU, set the MASTER 2 switch from OFF to ON then back to OFF.
   (2) After 30 seconds do again one time the procedure given in step (1) above.
   (3) If the fault continues:
  • do a check of the wiring and the connector J14 at the ECU 2 (4000KS).
     (a) If there is no continuity:
  • repair the above wiring.
     (b) If there is continuity:
Subtask 73-20-00-810-091-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message J14, ECU (ENG IDENT):
  • reset the ECU 2 as follows:
   (1) On the panel 115VU, set the MASTER 2 switch from OFF to ON then back to OFF.
   (2) After 30 seconds do again one time the procedure given in step (1) above.
   (3) If the fault continues:
  • do a check of the wiring and the connector J14 at the ECU 2 (4000KS).
     (a) If there is no continuity:
  • repair the above wiring.
     (b) If there is continuity:
Subtask 73-20-00-710-103-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.
[Rev.8 from Aug 2018] 2026.04.04 04:35:18 UTC
"WTRUIB" 2025