N184SH - 2007 Robinson Helicopter R22 Beta Aircraft Registration
R222007 ROBINSON HELICOPTER R22 BETA
Aircraft Description
N184SH is a 2007 Robinson Helicopter R22 BETA, a single-engine reciprocating (piston) aircraft registered to Silverhawk Aviation Academy LLC in Caldwell, ID. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on September 10, 2007. The registration certificate was issued on December 29, 2016. The registration is set to expire on December 31, 2029. Powered by a Lycoming O-360-J2A engine producing 145 horsepower, N184SH is. The aircraft's Mode S transponder code is A15120 (hex), used for ADS-B identification and flight tracking. N184SH was last tracked by AviatorDB at coordinates 43.6340, -116.6358 on March 19, 2026. The FAA registry record for N184SH was last updated on September 22, 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 N184SH. 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 |
|---|---|---|---|---|
| Jul 13, 2015 | GAA15CA181 | Substantial | None | Abnormal ground contact during a 180 degree autorotation, resulting in a severed tail rotor driveshaft by a main rotor blade. A factor contributing to the accident was the rotor blowback condition due to the aft tilting of the main rotor disk. |
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