The aircraft was designed as a lower-cost touring trike than the Mainair Blade. It complies with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 4500NaN0 and is certified to UK BCAR Section "S". The aircraft has a maximum gross weight of 3700NaN0. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem, open cockpit, tricycle landing gear and a single engine in pusher configuration.
The aircraft is made from bolted-together aluminium tubing, with its double-surface wing covered in Dacron sailcloth. Its 10.61NaN1 span wing is supported by a single tube-type kingpost and uses an "A" frame control bar. The occupants are accommodated in tandem seating, with a fibreglass cockpit fairing that includes a small windshield. To keep costs down, the factory supplied engine was the 370NaN0 Rotax 503 twin cylinder, two-stroke, air cooled powerplant. The twin cylinder, two-stroke, liquid cooled 480NaN0 Rotax 582 was an available option.