# SDR ANCF20250330005

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 30, 2025
- Submitted: April 2, 2025
- Operation: Air carrier
- Aircraft: [N862AV](https://openairdocs.org/aircraft/N862AV), registered now
- Make and model: Airbus A320-214
- Registry model: [Airbus A320-214](https://openairdocs.org/model/airbus-a320-214) (OpenAirDocs)
- Aircraft serial: 4862
- Aircraft time: 31,277 hours, 28,636 cycles
- Engine: Cfmint CFM565B43
- Engine time: 30,562 hours, 27,891 cycles
- System (JASC): [3600 · Pneumatic System](https://openairdocs.org/jasc/3600)
- Part: Sense Line
- Condition: Leaking
- Stage of operation: CL
- How discovered: V
- Nature of condition: J
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/ANCF20250330005

## Discrepancy

ENGINE 2 BLEED FAULT IN FLIGHT DUE TO PNEUMATIC AIR LEAK WAS REMOVED AND REPLACED THE SENSE LINE BTW THE PRV AND THE PYLON INTERFACE ON ENGINE #2 I.A.W AMM 36-11-49-000/400-026-A REV 71 REV DATE 01-FEB-2025 AND PERFORMED LEAK CHECK I.W.A AMM 36-11-52-790-001-A REV 71 REV DATE 01-FEB-2025, NOT FOUND LEAKS ON THE SENSE LINE ENGINE 2 BLEED FAULT IN FLIGHT PERFORMED LEAK TEST OF THE BLEED PRESSURE REGULATOR VALVE WITH THE ENGINE IN OPERATION IAW AMM 36-11-52-790-001-A REV 71 REV DATE 01 FEB 2025 TEST PASS OK

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