The aircraft was marketed in Austria and Germany under the name Amigo.[2]
The aircraft was designed to comply with the European Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 4500NaN0. It was also marketed in the United States as a kit only for the US homebuilt category.[2]
The Tulak features 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 engine in tractor configuration.[2]
The aircraft fuselage is made from welded steel tubing, with the whole aircraft covered in doped aircraft fabric. Its 101NaN1 span wing employs a Clark Y airfoil, mounts flaps, has a wing area of 13.01m2 and is supported by "V" struts and jury struts. The standard engine used is the 500NaN0 Rotax 503 two-stroke and 800NaN0 Rotax 912 four-stroke powerplant, although a four-stroke BMW boxer engine was also available as a factory option[2] [3]
The Tulak has a typical empty weight of 230kg (510lb) and a gross weight of 450kg (990lb), giving a useful load of 220kg (490lb).
The manufacturer estimated the construction time from the supplied kit as 700 hours.
By 1998 the company reported that 10 aircraft were completed and flying.
In September 2014 no examples were registered in the United States with the Federal Aviation Administration.[4]