W DOC AIRBUS | TSM A320F

Loss of the Data on ARINC Bus from the EIU to the FADEC on Engine 1


TASK 77-00-00-810-886-A
Loss of the Data on ARINC Bus from the EIU to the FADEC on Engine 1


1. Possible Causes
  • harness J3 between the EIU (1KS1) and the ECU (4000KS)
  • EIU-1 [1KS1]
  • CONT-AIR COND SYSTEM 1 [47HH]
  • CONT-AIR COND SYSTEM 2 [57HH]
  • ECU [4000KS]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 21-61-34-000-002
Removal of the Air-Conditioning System Controller
AMM 21-61-34-400-002
Installation of the Air-Conditioning System Controller
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 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 73-29-00-710-040
Operational Test of the FADEC on the ground (with Engine Motoring)
3. Fault Confirmation
Subtask 77-00-00-710-211-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the operational test of the Engine Interface Unit (EIU) through the Centralized Fault Display System (CFDS) AMM 73-25-34-710-040.
   (2) Do the operational test of the FADEC 1A and 1B on the ground (with engine non motoring) AMM 73-29-00-710-040.
4. Fault Isolation
Subtask 77-00-00-810-159-C ** ON A/C NOT FOR ALL
A. If the fault symptom is identified by the upper ECAM warning ENG1 BLEED STATUS FAULT and the tests of the EIU and FADEC give no maintenance messages:
  • do a check for open or short to ground of the harness J3 between the EIU (1KS1) and the ECU (4000KS) pins AB/5A, 5C to pins J3/22, 23 ASM 732506.
   (1) If the wiring is not correct:
  • repair the above wiring.
   (2) If the wiring is correct:
   (3) If the fault continues:
   (4) If the fault continues:
[Rev.8 from Aug 2018] 2026.04.04 04:37:35 UTC