W DOC AIRBUS | TSM A320F

Fuel Leak at the Engine 2 Turbine Rear Frame Water Drain


TASK 71-00-00-810-813-A
Fuel Leak at the Engine 2 Turbine Rear Frame Water Drain


1. Possible Causes
  • HMU
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 71-00-00-710-001
Dry Motoring Check
AMM 71-00-00-710-006
Minimum Idle Check
AMM 73-11-70-000-002
Removal of the Burner Selection Valve (BSV) for SAC Engines
AMM 73-11-70-400-002
Installation of the Burner Selection Valve (BSV) for SAC Engines
AMM 73-21-10-000-001
Removal of the Hydromechanical Unit (HMU)
AMM 73-21-10-000-002
Removal of the Hydromechanical Unit (HMU)
AMM 73-21-10-400-001
Installation of the Hydromechanical Unit (HMU)
AMM 73-21-10-400-002
Installation of the Hydromechanical Unit (HMU)
3. Fault Confirmation
Subtask 71-00-00-710-066-B ** ON A/C NOT FOR ALL
A. Not applicable.
4. Fault Isolation
Subtask 71-00-00-810-064-B ** ON A/C NOT FOR ALL
A. If the fault symptom is identified by the crew observation fuel leak at the Turbine Rear Frame water drain:
   (1) If fuel leak is present, replace the BSV AMM 73-11-70-000-002 and AMM 73-11-70-400-002.

END OF CFM SB 73-112

   (2) If fuel leak is present, replace the HMU AMM 73-21-10-000-001 AMM 73-21-10-400-001 AMM 73-21-10-000-002 AMM 73-21-10-400-002.
[Rev.8 from Aug 2018] 2026.04.04 04:34:56 UTC