Aircraft Description
N3774Z is a Piper PA-18-150, a single-engine reciprocating (piston) aircraft registered to Owen Matthew L in Kasilof, AK. The registration certificate was issued on August 12, 2021. The registration is set to expire on August 31, 2028. Powered by a Lycoming 0-320 SERIES engine producing 180 horsepower, N3774Z is. The aircraft's Mode S transponder code is A450C8 (hex), used for ADS-B identification and flight tracking. The FAA registry record for N3774Z was last updated on June 3, 2023. 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 N3774Z. 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 (3)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| May 6, 2010 | ANC10CA037 | Substantial | None | The loss of the left rudder cable retaining bolt during base to final turn, resulting in a loss of control and impact with terrain. |
| Sep 5, 2000 | ANC00LA114 | Substantial | None | The pilot's inadvertent ground loop/swerve during the landing roll. |
| Jul 5, 1995 | ANC95LA098 | Substantial | None | THE PILOT'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL, DURING AN OFF-AIRPORT LANDING ON ROUGH/UNEVEN TERRAIN, WHICH RESULTED IN AN INADVERTENT GROUND SWERVE. THE TERRAIN CONDITION WAS A RELATED FACTOR. |
The loss of the left rudder cable retaining bolt during base to final turn, resulting in a loss of control and impact with terrain.
The pilot's inadvertent ground loop/swerve during the landing roll.
THE PILOT'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL, DURING AN OFF-AIRPORT LANDING ON ROUGH/UNEVEN TERRAIN, WHICH RESULTED IN AN INADVERTENT GROUND SWERVE. THE TERRAIN CONDITION WAS A RELATED FACTOR.
Additional Details
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC