N80140 - 1989 Robinson Helicopter R22 Beta Aircraft Registration
R221989 ROBINSON HELICOPTER R22 BETA
Aircraft Description
N80140 is a 1989 Robinson Helicopter R22 BETA, a single-engine reciprocating (piston) aircraft registered to Emerald City Aircraft Leasing INC in Port Orchard, WA. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on May 4, 1989. The registration certificate was issued on January 11, 2012. The registration is set to expire on January 31, 2028. Powered by a Lycoming 0-320 SERIES engine producing 180 horsepower, N80140 is. The aircraft's Mode S transponder code is AAE891 (hex), used for ADS-B identification and flight tracking. The FAA registry record for N80140 was last updated on April 14, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Robinson R-22, the world's most prolific light training helicopter, revolutionized civil aviation by making helicopter flight training affordable for ordinary pilots. First flown on August 28, 1975, it featured a two-seat configuration with a teetering rotor system and lightweight aluminum construction. Powered by a 150-horsepower Lycoming O-320 piston engine, the R-22 achieved a maximum cruise speed of 96 knots and could carry 516 pounds of payload. Robinson Helicopter Company manufactured over 4,800 units between 1979 and 2016. AviatorDB tracks 1,247 Robinson Helicopter aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is R22.
AviatorDB has found no NTSB accident or incident reports involving N80140. 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 |
|---|---|---|---|---|
| Oct 3, 2012 | WPR13LA003 | Substantial | None | The pilot's failure to maintain sufficient rotor rpm during a precautionary landing, which resulted in a hard landing. |
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