W DOC AIRBUS | TSM A320F

Uncommanded Continuous Ignition on Engine 1 After Engine Start


TASK 74-00-00-810-820-A
Uncommanded Continuous Ignition on Engine 1 After Engine Start


1. Possible Causes
  • wiring from the ENG/MODE/CRANK/AUTO IGN/IGN selector switch (6KS) to the EIU-1 (1KS1)
  • EIU-1 [1KS1]
  • VALVE-ENG AIR INTAKE ANTI ICE [4000DN]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 30-21-51-000-040
Removal of the Engine Air-Intake Anti-Ice Valve
AMM 30-21-51-400-041
Installation of the Engine Air-Intake Anti-Ice Valve
ASM 732508
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)
3. Fault Confirmation
Subtask 74-00-00-710-100-A ** ON A/C NOT FOR ALL
A. Test
   (1) Not applicable, the fault is evident.
4. Fault Isolation
Subtask 74-00-00-810-076-C ** ON A/C NOT FOR ALL
A. If the fault symptom is identified by the crew observation ENG 1 - Uncommanded continuous IGNITION after engine start:
  • do a check of the wiring from the ENG/MODE/CRANK/AUTO IGN/IGN selector switch (6KS) to the EIU-1 (1KS1)
    . pin 3 to pin AA/1A
    . pin 4 to pin AA/1B ASM 732508.
   (1) If the fault continues:
   (2) If the fault continues:
Subtask 74-00-00-810-076-E ** ON A/C NOT FOR ALL
A. If the fault symptom is identified by the crew observation ENG 1 - Uncommanded continuous IGNITION after engine start:
  • do a check of the wiring from the ENG/MODE/CRANK/AUTO IGN/IGN selector switch (6KS) to the EIU-1 (1KS1)
    . pin 3 to pin AA/1A
    . pin 4 to pin AA/1B ASM 732508.
   (1) If the fault continues:
Subtask 74-00-00-710-101-A ** ON A/C NOT FOR ALL
B. After the subsequent flight, make sure that the fault does not continue.
[Rev.8 from Aug 2018] 2026.04.04 04:36:58 UTC