W DOC AIRBUS | TSM A320F

Failure of the Ignition 2 System - Engine 2 - Channel A or Channel B


TASK 74-00-00-810-804-A
Failure of the Ignition 2 System - Engine 2 - Channel A or Channel B


1. Possible Causes
  • SPARK-IGNITER, B [4001JH2]
  • left ignition lead
  • lower exciter box
  • ECU [4000KS]
  • J1 harness
  • J2 harness
  • EIU-2 [1KS2]
  • HJ1 harness
  • HJ2 harness
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 71-51-43-000-046
Removal of the ECU (Channel A) Harness
AMM 71-51-43-000-047
Removal of the ECU (Channel B) Harness
AMM 71-51-43-400-046
Installation of the ECU (Channel A) Harness
AMM 71-51-43-400-047
Installation of the ECU (Channel B) Harness
AMM 71-51-44-000-004
Removal of the Electronic Control Unit (ECU) Channel A Harness 238W0904
AMM 71-51-44-000-005
Removal of the Electronic Control Unit (ECU) Channel B Harness 238W0904
AMM 71-51-44-400-004
Installation of the Electronic Control Unit (ECU) Channel A Harness 238W0904
AMM 71-51-44-400-005
Installation of the Electronic Control Unit (ECU) Channel B Harness 238W0904
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 73-25-34-000-040
Removal of the Engine Interface Unit (EIU)
AMM 73-25-34-400-040
Installation of the Engine Interface Unit (EIU)
AMM 74-00-00-710-040
Operational Test of the Ignition System
AMM 74-00-00-710-043
Operational Test of the Ignition System
AMM 74-11-10-000-001
Removal of the Ignition Exciter
AMM 74-11-10-000-002
Removal of the Ignition Exciter
AMM 74-11-10-400-001
Installation of the Ignition Exciter
AMM 74-11-10-400-002
Installation of the Ignition Exciter
AMM 74-21-20-000-001
Removal of the Left Ignition Lead
AMM 74-21-20-000-002
Removal of the Left Ignition Lead
AMM 74-21-20-400-001
Installation of the Left Ignition Lead
AMM 74-21-20-400-002
Installation of the Left Ignition Lead
AMM 74-21-30-000-001
Removal of the Spark Igniter
AMM 74-21-30-000-002
Removal of the Spark Igniter
AMM 74-21-30-400-001
Installation of the Spark Igniter
AMM 74-21-30-400-002
Installation of the Spark Igniter
3. Fault Confirmation
Subtask 74-00-00-710-056-A ** ON A/C NOT FOR ALL
A. Do the operational test of the ignition system, by performing an aural check of the igniter plug operation AMM 74-00-00-710-040.
NOTE: The igniter test will spark the right igniter plug (A) for 10 seconds, wait 2 seconds then spark the left igniter plug (B) for 10 seconds. This test provides for an aural feedback of proper ignition operation . No CFDS test results are available.
Subtask 74-00-00-710-056-B ** ON A/C NOT FOR ALL
A. Do the operational test of the ignition system, by performing an aural check of the igniter plug operation AMM 74-00-00-710-043.
NOTE: The igniter test will spark the right igniter plug (A) for 10 seconds, wait 2 seconds then spark the left igniter plug (B) for 10 seconds. This test provides for an aural feedback of proper ignition operation . No CFDS test results are available.
4. Fault Isolation
Subtask 74-00-00-810-053-A ** ON A/C NOT FOR ALL
A. The failure message IGN2, ECU is generated if there is no light off detected 10 seconds after the fuel is turned on.
   (1) If an audible spark cannot be heard on the left igniter plug (B):
     (a) If an audible spark is not heard:
     (b) If an audible spark is not heard:
     (c) If an audible spark is not heard:
     (d) If an audible spark is not heard:
   (2) If an audible spark can be heard on the left igniter plug (B):
   (3) If an audible spark can be heard on the left igniter plug (B), but the failure message is repetitive:
     (a) If the fault continues during subsequent flights:
     (b) If the fault continues during subsequent flights:
     (c) If the fault continues during subsequent flights:
     (d) If the fault continues during subsequent flights:
Subtask 74-00-00-810-053-B ** ON A/C NOT FOR ALL
A. The failure message IGN2, ECU is generated if there is no light off detected 10 seconds after the fuel is turned on.
   (1) If an audible spark cannot be heard on the left igniter plug (B):
     (a) If an audible spark is not heard:
     (b) If an audible spark is not heard:
     (c) If an audible spark is not heard:
     (d) If an audible spark is not heard:
   (2) If an audible spark can be heard on the left igniter plug (B):
   (3) If an audible spark can be heard on the left igniter plug (B), but the failure message is repetitive:
     (a) If the fault continues during subsequent flights:
     (b) If the fault continues during subsequent flights:
     (c) If the fault continues during subsequent flights:
     (d) If the fault continues during subsequent flights:
Subtask 74-00-00-710-057-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.
   (1) No additional maintenance action is required if the fault is not confirmed.
   (2) Repeat the fault isolation procedure if the fault continues.
[Rev.8 from Aug 2018] 2026.04.04 04:36:57 UTC