W DOC AIRBUS | TSM A320F

Loss of Data on EIU to FADEC Bus for Engine 1


TASK 73-25-00-810-885-A
Loss of Data on EIU to FADEC Bus for Engine 1


1. Possible Causes
  • EIU-1 [1KS1]
  • J3 harness from the EIU 1 (1KS1) to the ECU (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)
ASM 732505
ASM 732506
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 73-25-00-710-194-A ** ON A/C NOT FOR ALL
A. Do the operational test of the engine interface unit through the CFDS AMM 73-25-34-710-040.
Subtask 73-25-00-710-194-B ** ON A/C NOT FOR ALL
A. Do the operational test of the engine interface unit through the CFDS AMM 73-25-34-710-043.
4. Fault Isolation
Subtask 73-25-00-810-122-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message CHECK EIU 1 ARINC OUTPUT CIRCUIT TO FADEC OR EIU 1:
  • do a check for 28VDC at EIU 1 pins AC/9, 11.
   (1) If there is 28VDC:
   (2) If the fault continues:
  • do a check and repair the J3 harness from the EIU 1 (1KS1) to the ECU (4000KS) pins AB/5C, 5A to pins J3/22, 23 ASM 732506.
   (3) If the fault continues:
Subtask 73-25-00-710-195-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.
[Rev.8 from Aug 2018] 2026.04.04 04:35:46 UTC