Designed as a trainer for the unlimited class, the TR 200 features a cantilever low-wing, a two-seats-in-tandem enclosed cockpit under a bubble canopy, fixed conventional landing gear with wheel pants and a single engine in tractor configuration.
The aircraft is made from wood. Its 7.421NaN1 span wing has a wing area of 10m2. The cabin width is 71cm (28inches). The acceptable power range is 200to and the standard engine used is the 2000NaN0 Lycoming AEIO-360 powerplant.
The TR 200 has a typical empty weight of 570kg (1,260lb) and a gross weight of 870kg (1,920lb), giving a useful load of 300kg (700lb). With full fuel of the payload for pilot, passenger and baggage is 186kg (410lb).
The standard day, sea level, no wind, take off with a 2000NaN0 engine is 4000NaN0 and the landing roll is 4500NaN0.
The manufacturer estimated the construction time from the supplied kit as 800 hours.