The Pairadigm features a strut-braced high-wing, a two-seats-in-side-by-side configuration semi-enclosed cockpit with a windshield, fixed tricycle landing gear and two fuselage-mounted engines, one in tractor configuration in the nose and the other in pusher configuration in the rear fuselage.[1]
The aircraft is made from bolted-together aluminum tubing, with its flying surfaces covered in doped aircraft fabric. Its 321NaN1 span high-lift wing mounts flaps, is supported by V-struts and has a wing area of 160square feet. The tail is a conventional low-tail design. The cabin width is 43inches. The acceptable power range is 40to and the standard engines used are two 450NaN0 2si 460 in-line twin-cylinder, two-stroke, single ignition powerplants.[1]
The aircraft has a typical empty weight of 700lb and a gross weight of 1400lb, giving a useful load of 700lb. With full fuel of the payload for the pilot, passenger and baggage is 556lb.[1]
The standard day, sea level, no wind, take off with twin 450NaN0 engines is 1000NaN0 and the landing roll is 2000NaN0.[1]
The manufacturer estimated the construction time from the supplied kit as 250 hours.[1]
By 1998 the company reported that 10 kits had been sold and one aircraft had been completed and was flying, with the design generally available from July 1998.[1]
As of May 2015 no examples were registered in the United States with the Federal Aviation Administration.[2]