The Hornet is a development of the
Taggart GyroBee and was introduced in 1997. The Hornet was designed to comply with the US
FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of . The aircraft has a standard empty weight of . It features a single main rotor, a single-seat, open cockpit without a windshield,
tricycle landing gear and a twin cylinder, air-cooled,
two-stroke, single-ignition
Rotax 447 engine in
pusher configuration. The
Rotax 503 engine can also be fitted. ==Specifications (Hornet) ==