The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 2540NaN0. The aircraft has a standard empty weight of 2500NaN0. Early models feature a cable-braced hang glider-style high-wing, weight-shift controls, a single-seat or two-seats-in-tandem open cockpit, tricycle landing gear and a single engine in pusher configuration. Later Coyote models use the strut-braced North Wing Mustang wing made by North Wing Design.
The aircraft is made from bolted-together 6061-T6 aluminum and welded 4130 steel tubing, with its original TC Trikes Super D-16 single surface wing covered in Dacron sailcloth. The 172square feet area wing is supported by a single tube-type kingpost and uses an "A" frame control bar.
The standard engine supplied was the 400NaN0 twin cylinder, two-stroke, air-cooled Rotax 447, with the 500NaN0 Rotax 503 optional. The standard single seat can be replaced with a tandem seat for two occupants.