[3] The John Doe features a strut-braced high-wing, a two-seats-in-tandem enclosed cabin, fixed conventional landing gear and a single engine in tractor configuration.
Its 30.6 ft (9.3 m) span wing mounts flaps, leading edge slats, drooping ailerons, stall fences, winglets and has a wing area of 130.6 sq ft (12.13 m2).
With full fuel of 26 U.S. gallons (98 L; 22 imp gal) the payload for the pilot, passenger and baggage is 366 lb (166 kg).
[1] The manufacturer estimated the construction time from the supplied kit as 400 hours.
[5] Data from AeroCrafter, All-Aero and EAA Experimenter[1][2][3]General characteristics Performance