# SDR ANCF2013030200149

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 2, 2013
- Submitted: March 5, 2013
- Operation: Air carrier
- Aircraft: [N451AV](https://openairdocs.org/aircraft/N451AV), registered now
- Make and model: Airbus A320-214
- Registry model: [Airbus A320-214](https://openairdocs.org/model/airbus-a320-214) (OpenAirDocs)
- Aircraft serial: 4051
- Aircraft time: 9,148,415 hours, 8,089 cycles
- Engine: Cfmint CFM565B43
- System (JASC): [7200 · Engine (Turbine/Turboprop)](https://openairdocs.org/jasc/7200)
- Part: Engine
- Condition: Bird Ingestion
- Location: Nr 2
- Stage of operation: CL
- How discovered: O
- Nature of condition: C, E
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/ANCF2013030200149

## Discrepancy

BIRD STRIKE ENGINE 2 AT TAKEOFF IN BGA HIGH VIBRATION DURING CLIMB N1 6.0.  IN ACCORDANCE WITH AMM TASK 72-00-00-200 006-A AND SUBTASKS 72-00-00-220-172-A (B1) 72-00-00-280-057-A BOROSCOPE INSPECTION OF THE STAGE 4 LP TURBINE BLADES, HPC STAGES 1, 3 AND 8 CONBUSTION CHAMBER DOME ASSEMBLY WAS PERFORMED, NO DAMAGES WERE FOUND.  IN ACCORDANCE WITH AMM 05-51-14-200-001-A, THE INSPECTION OF THE AIRFRAME AFTER A BIRD STRIKE ENGINE 2 WAS PERFORMED, AND AMM 72-00-00-200-006-A THE INSPECTION CHECK OF FOD WAS PERFORMED, AND NO ADDITIONAL DAMAGE FOUND.  IN ACCORDANCE WITH AMM 71-00-00-710-009- THE VIBRATION CHECK WAS PERFORMED.  THE VIBRATION VALVES ENGINE 2 MAX CLIMB 0.6% AND N2 0.3%.

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