Aircraft Description
N47BC is a 1988 Piper PA-46-310P, a single-engine reciprocating (piston) aircraft registered to Brentech Leasing LLC in Cartersville, GA. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on August 23, 1988. The registration certificate was issued on March 17, 2025. The registration is set to expire on March 31, 2032. Powered by a Cont Motor TSIO-520 SER engine producing 300 horsepower, N47BC is. The aircraft's Mode S transponder code is A5BEDD (hex), used for ADS-B identification and flight tracking. N47BC was last tracked by AviatorDB at coordinates 31.4827, -82.8800 on April 2, 2026. The FAA registry record for N47BC was last updated on March 17, 2025. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Piper M600 represents the pinnacle of single-engine turboprop aviation, combining advanced safety technology with exceptional performance capabilities. First entering production in 2016, this low-wing single-engine aircraft seats six passengers and features the revolutionary Garmin Autoland system, making it the first certified aircraft with autonomous landing capability. Powered by a 600-shaft-horsepower Pratt & Whitney Canada PT6A-42A turboprop engine, the M600 achieves a maximum operating speed of 250 knots with a range exceeding 1,000 nautical miles. The aircraft is manufactured by Piper Aircraft Corporation at their Vero Beach, Florida facility. AviatorDB tracks 48,285 Piper aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is M600.
AviatorDB has found no NTSB accident or incident reports involving N47BC. AviatorDB cross-references all FAA registration data with NTSB accident and incident reports, providing a comprehensive safety overview for every registered aircraft in the United States.
Registered Owner
Powerplant & Avionics
NTSB Accident History (1)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Dec 26, 2007 | DEN08IA044 | MINR | None | The failure of the crankshaft due to fatigue. The fatigue crack initiation was not determined. |
Additional Details
Last Known Position
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC