N480EH - 2002 Enstrom Helicopter CORP 480B Aircraft Registration
EN482002 ENSTROM HELICOPTER CORP 480B
Aircraft Description
N480EH is a 2002 Enstrom Helicopter Corp 480B, a single-engine turbo-shaft aircraft registered to Sloflight LLC in Ogden, UT. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on January 23, 2002. The registration certificate was issued on January 23, 2024. The registration is set to expire on January 31, 2031. Powered by a Rolls-royc 250-C20W engine producing 420 horsepower, N480EH is. The aircraft's Mode S transponder code is A5E905 (hex), used for ADS-B identification and flight tracking. N480EH was last tracked by AviatorDB at coordinates 41.1966, -112.0029 on March 18, 2026. The FAA registry record for N480EH was last updated on January 23, 2024. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Enstrom 480 is a five-seat turbine-powered helicopter that represented the company's ambitious entry into the military training market during the early 1990s. First flown on October 7, 1989, it features a single Rolls-Royce 250-C20 turboshaft engine producing 277 horsepower continuous power, welded steel-tube fuselage construction, and distinctive left-seat pilot controls. With a service ceiling of 15,600 feet and range of 685 kilometers, approximately 142 aircraft have been manufactured by Enstrom Helicopter Corporation since production began in 1993. AviatorDB tracks 133 Enstrom Helicopter Corp aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is EN48.
AviatorDB has found no NTSB accident or incident reports involving N480EH. 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 |
|---|---|---|---|---|
| Jun 29, 2005 | DEN05LA102 | Substantial | None | the pilot's failure to maintain control of the helicopter. Contributing factor's include the pilot's failure to maintain clearance from terrain. |
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