N805EH - Aircraft Aircraft Registration
R22Aircraft Description
N805EH is a , a reciprocating (piston) aircraft registered to Pope James D in Lewiston, ID. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on July 8, 1993. The registration certificate was issued on February 18, 2026. The registration is set to expire on February 28, 2033. Powered by a Lycoming 0-320 SERIES engine producing 180 horsepower, N805EH is. The aircraft's Mode S transponder code is AAF4DC (hex), used for ADS-B identification and flight tracking. The FAA registry record for N805EH was last updated on February 18, 2026. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
Cessna Aircraft Company, now a subsidiary of Textron Aviation based in Wichita, Kansas, is one of the most prolific aircraft manufacturers in history. Known for iconic models like the Cessna 172 Skyhawk, the world's most-produced aircraft, Cessna has been building general aviation aircraft since 1927. The is one of the aircraft types tracked by AviatorDB in the FAA registry database.
AviatorDB has found no NTSB accident or incident reports involving N805EH. 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 (2)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Dec 4, 2007 | LAX08IA032 | Unknown | None | Failure of the tail rotor system support bracket during landing. |
| Apr 28, 1998 | LAX98LA146 | Substantial | None | the CFI's failure to follow procedures and directives, and the use of an improper technique to transition from an autorotative descent to a hover, which exceeded the aircraft's performance capabilities and resulted in a unplanned hard landing. The soft terrain was a factor in the nose over and rollover. |
Failure of the tail rotor system support bracket during landing.
the CFI's failure to follow procedures and directives, and the use of an improper technique to transition from an autorotative descent to a hover, which exceeded the aircraft's performance capabilities and resulted in a unplanned hard landing. The soft terrain was a factor in the nose over and rollover.
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