The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 2540NaN0. The aircraft has a standard empty weight of 2500NaN0.
Mr Easy features a strut-braced and cable-braced biplane layout, a single-seat, open cockpit, fixed conventional landing gear and a single engine in pusher configuration, mounted above the tail boom tube.
The aircraft is made from bolted-together aluminum tubing, with its flying surfaces covered in doped aircraft fabric. Its 241NaN1 span wing has a wing area of 145square feet. The standard engine used is the 400NaN0 Rotax 447 two-stroke twin-cylinder powerplant.
Mr Easy has a typical empty weight of 250lb and a gross weight of 485lb, giving a useful load of 235lb. With full fuel of the payload for the pilot and baggage is 205lb.
The standard day, sea level, no wind, take off and landing roll with a 400NaN0 engine is 1750NaN0.
The designer estimates the construction time from the supplied plans as 250 hours.
In the United States ultralights are not required to be registered, and in April 2014 no examples were in fact registered in the United States with the Federal Aviation Administration, although a total of two had been registered at one time.[3]