N931SH - 2005 Robinson Helicopter R22 Beta Aircraft Registration
R222005 ROBINSON HELICOPTER R22 BETA
Aircraft Description
N931SH is a 2005 Robinson Helicopter R22 BETA, a single-engine reciprocating (piston) aircraft registered to Dodson International Parts INC in Rantoul, KS. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on August 22, 2005. Powered by a Lycoming O-360 SERIES engine producing 180 horsepower, N931SH is. The aircraft's Mode S transponder code is ACEAF8 (hex), used for ADS-B identification and flight tracking. The FAA registry record for N931SH was last updated on January 31, 2017. 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 N931SH. 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 7, 2016 | GAA16CA296 | Substantial | None | The flight instructor's delayed remedial action and his failure to remain vigilant as the helicopter entered the weathercock stability region, in gusting wind conditions, resulting in loss of tail rotor effectiveness and ground impact. |
Additional Details
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-15 01:32:20 UTC