W DOC AIRBUS | TSM A320F

Loss of Channel A Data from the ECU on Engine 2


TASK 73-25-00-810-844-A
Loss of Channel A Data from the ECU on Engine 2


1. Possible Causes
  • ECU [4000KS]
  • EIU-2 [1KS2]
  • wiring from the ECU 2 (4000KS) to the EIU 2 (1KS2)
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)
ASM 732510
AMM 73-25-34-000-040
Removal of the Engine Interface Unit (EIU)
AMM 73-25-34-400-040
Installation of the Engine Interface Unit (EIU)
AMM 73-25-34-710-040
Operational Test of the Engine Interface Unit
AMM 73-25-34-710-043
Operational Test of the Engine Interface Unit
3. Fault Confirmation
Subtask 73-25-00-710-136-A ** ON A/C NOT FOR ALL
A. Do the operational test of the Engine Interface Unit (EIU) through the Centralized Fault Display System (CFDS) AMM 73-25-34-710-040.
Subtask 73-25-00-710-136-B ** ON A/C NOT FOR ALL
A. Do the operational test of the Engine Interface Unit (EIU) through the Centralized Fault Display System (CFDS) AMM 73-25-34-710-043.
4. Fault Isolation
Subtask 73-25-00-810-093-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message EIU 2 : NO FADEC 2 A DATA:
   (1) If the fault continues:
   (2) If the fault continues:
  • do a check and repair the wiring from the ECU 2 (4000KS) to the EIU 2 (1KS2) pins J3/24, 11 to pins AA/15A, 15C ASM 732510.
Subtask 73-25-00-710-137-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.
[Rev.8 from Aug 2018] 2026.04.04 04:35:42 UTC