The aircraft features a cantilever low-wing, a single-seat enclosed cockpit under a bubble canopy, retractable conventional landing gear and a single engine in tractor configuration.
The aircraft is made from welded steel tubing covered in a shell of polyurethane foam and fiberglass. Its 241NaN1 span wing, mounts flaps and has a wing area of 100square feet. The cockpit width is 21inches. The standard engine used is the 2300NaN0 Ford Motor Company V-6 automotive conversion powerplant.
The aircraft has a typical empty weight of 1354lb and a gross weight of 1954lb, giving a useful load of 600lb. With full fuel of the payload for pilot and baggage is 354lb.
The aircraft has fairly lengthy runway requirements with a standard day sea level take-off distance of 12000NaN0 and a landing distance of 15000NaN0.
The kit included prefabricated assemblies, the engine and scale fixed pitch propeller, instruments and avionics. The manufacturer estimated the construction time from the supplied kit as 2000 hours.