# SDR BDEA2013F00114

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 15, 2013
- Submitted: July 15, 2013
- Operation: Air carrier
- Aircraft: [N513D](https://openairdocs.org/aircraft/N513D), registered now
- Make and model: Cessna 340A
- Registry model: [Cessna 340A](https://openairdocs.org/model/cessna-340a) (OpenAirDocs)
- Aircraft serial: 340A0048
- Aircraft time: 7,783 hours
- Engine: Cont TSIO520NB
- Engine time: 6,241 hours
- System (JASC): [8120 · Exhaust Turbocharger](https://openairdocs.org/jasc/8120)
- Part: Bearing
- Condition: Failed
- Location: Turbocharger
- Component: Turbocharger, Kelly
- Component part number: 20601
- Stage of operation: CR
- How discovered: O
- Nature of condition: K, F
- Precautionary procedure: E, A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/BDEA2013F00114

## Discrepancy

LOSS OF MANIFOLD PRESSURE DURING CRUISE FLIGHT (12,000 FT) IN THE LT ENGINE CAUSING A PRECAUTIONARY ENGINE SHUTDOWN.  POST FLIGHT INSPECTION FOUND THE BEARING IN THE TURBOCHARGER HAD FAILED AND ALLOWED SUBSTANTIAL OIL LOSS.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
