DOC AIRBUS | TSM A320FEGT Significant Positive Step Change during Take-off and/or Cruise on Engine 2
1. Possible Causes
· LPC Bleed Duct for a partially detached seal
2 Job Set-up Information
A. Referenced Information
REFERENCE DESIGNATION
Ref. AMM 72-32-60-200-011 Inspection of the LPC Bleed Duct Seal
3. Fault Confirmation
Subtask 77-00-00-710-279-A
A. Test
· Not applicable.
4. Fault Isolation
Subtask 77-00-00-810-209-A
A. If the fault symptom significant step change in EGT occured:
· examine the LPC Bleed Duct for a partially detached seal Ref. AMM 72-32-60-200-011 . [Rev.6 from Feb 2017] 2026.04.04 04:37:50 UTC