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 2490NaN0. It features a cable-braced hang glider-style high-wing, weight-shift controls, a single-seat open cockpit, tricycle landing gear with wheel pants and a single engine in pusher configuration.
The aircraft is made from bolted-together aluminum tubing, with its wing covered in Dacron sailcloth. Its 7.91NaN1 span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The powerplant is a twin cylinder, air-cooled, two-stroke, dual-ignition 400NaN0 Rotax 447 engine. The aircraft has an empty weight of 1130NaN0 and a gross weight of 2940NaN0, giving a useful load of 1810NaN0. With full fuel of the payload is 1590NaN0.
The carriage comes with brakes, full suspension and a cockpit fairing, but is also available in nanotrike form without the fairings.
A number of different wings can be fitted to the basic carriage, including the BB Microlight BB-03 Trya and the US-made 40% double surface Manta RST. The Manta RST comes in four sizes, graded by wing area: 12.5m2, 15.5m2, 17m2 and 19m2.
In the United States the aircraft is imported by Manta Aircraft and fitted with the Manta RST wing.