The MD-II featured a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit accessed via doors, fixed conventional landing gear with wheel pants and a single tractor engine.
The aircraft was fabricated from 2024-T3 aluminum sheet. Its 29.51NaN1 span wing employed a USA 35B airfoil, mounted flaps and had an area of 177square feet. The cabin width was 41inches. The acceptable power range was 65to and the standard powerplant used was the 1400NaN0 Avia M 332 (LOM) four cylinder, inverted, air-cooled, supercharged, inline aircraft engine.
With the Avia engine the MD-II had a typical empty weight of 1150lb and a gross weight of 2000lb, giving a useful load of 850lb. With full fuel of the payload for pilot, passenger and baggage was 592lb.
The manufacturer estimated the construction time from the supplied kit at 1500 hours.
By 1998, the company reported two kits had been sold with two aircraft complete and flying.
In December 2013, no examples were registered with the US Federal Aviation Administration.[2]