When it was available the aircraft was supplied as a kit or in the form of plans for amateur construction.

[2] Designed as a high-speed, long-range cross country and aerobatic aircraft, the Acro 1 features a cantilever low-wing, a single-seat enclosed cockpit under a bubble canopy, fixed conventional landing gear and a single engine in tractor configuration.

A fuel capacity of 47 U.S. gallons (180 L; 39 imp gal) provides a range of 1,000 mi (1,600 km).

With full fuel of 47 U.S. gallons (180 L; 39 imp gal) the payload is 188 lb (85 kg).

[1] In November 2014 three examples were registered in the United States with the Federal Aviation Administration.