Aircraft Description
N2091W is a Piper PA-28RT-201, a single-engine reciprocating (piston) aircraft registered to Destefano Patrick in Adamsville, TN. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on February 21, 1979. The registration certificate was issued on May 31, 2024. The registration is set to expire on May 31, 2031. Powered by a Lycoming I0360 SER engine producing 180 horsepower, N2091W is. The aircraft's Mode S transponder code is A1B602 (hex), used for ADS-B identification and flight tracking. N2091W was last tracked by AviatorDB at coordinates 35.9513, -85.0850 on May 30, 2024. The FAA registry record for N2091W was last updated on May 31, 2024. 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 N2091W. 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 |
|---|---|---|---|---|
| Aug 31, 2013 | ERA13IA396 | Unknown | None | Maintenance personnel’s inadequate inspection and compliance with a Federal Aviation Administration airworthiness directive, which resulted in an undetected corroded and cracked stabilator turnbuckle and the subsequent failure of the turnbuckle and loss of elevator control during takeoff. |
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