Aircraft Description
N6465V is a 1969 Helio H-295, a single-engine reciprocating (piston) aircraft registered to Cornice LLC in Fairbanks, AK. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on September 15, 1969. The registration certificate was issued on February 17, 2021. The registration is set to expire on February 29, 2028. Powered by a Lycoming GO-480 SERIES engine producing 295 horsepower, N6465V is. The aircraft's Mode S transponder code is A87EA0 (hex), used for ADS-B identification and flight tracking. The FAA registry record for N6465V was last updated on April 21, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
Helio is an aircraft manufacturer with aircraft registered in the FAA database tracked by AviatorDB. AviatorDB tracks 142 Helio aircraft currently registered in the FAA database, including the H-295 model.
AviatorDB has found no NTSB accident or incident reports involving N6465V. 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 |
|---|---|---|---|---|
| Nov 15, 2014 | ANC15LA004 | Substantial | None | The partial loss of engine power for reasons that could not be determined because postaccident examination of the engine revealed no evidence of any preimpact mechanical anomalies. |
| Feb 28, 2005 | ANC05LA045 | Substantial | None | The pilot's delay in performing a go-around, and his failure to maintain obstacle clearance. |
| Aug 23, 1997 | ANC97LA128 | Substantial | None | failure of the pilot to maintain directional control of the airplane, which resulted in a swerve and collision with a tree as the pilot continued the takeoff, subsequently jamming the stabilator and causing the plane to crash in water. |
The partial loss of engine power for reasons that could not be determined because postaccident examination of the engine revealed no evidence of any preimpact mechanical anomalies.
The pilot's delay in performing a go-around, and his failure to maintain obstacle clearance.
failure of the pilot to maintain directional control of the airplane, which resulted in a swerve and collision with a tree as the pilot continued the takeoff, subsequently jamming the stabilator and causing the plane to crash in water.
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