Aircraft Description
N83894 is a 1981 Piper PA-32-301T, a single-engine reciprocating (piston) aircraft registered to Smith Lot P in Grangeville, ID. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on June 11, 1982. The registration certificate was issued on July 8, 2024. The registration is set to expire on July 31, 2031. Powered by a Lycoming TI0-540 SER engine producing 310 horsepower, N83894 is. The aircraft's Mode S transponder code is AB79C2 (hex), used for ADS-B identification and flight tracking. N83894 was last tracked by AviatorDB at coordinates 32.9549, -111.7670 on April 15, 2024. The FAA registry record for N83894 was last updated on July 8, 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 N83894. 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 |
|---|---|---|---|---|
| Sep 27, 1998 | FTW98LA415 | Substantial | None | The collision with deer during the landing roll. Factors were the dark night light condition and the separation of the lower strut assembly from the right main landing gear, on the subsequent flight. |
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