Single-engine low-wing business aircraft in the premium class. For its time unique streamlined solid metal construction, with retractable landing gear. Adjustable propeller - variable pitch, in later models constant speed.

The aircraft is characterized by very high quality and advanced design. Over time, it has been produced in several different versions with 165-225 hp for four persons. Later models have up to 300 hp and can accommodate five or six persons.

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The V-tail lacks vertical fin and the tail rudder works through a brilliant differential mechanism, both as elevator and rudder. The V-tail created some problems and gradually the fin surfaces were increased and some of the criticism was silenced. But various incidents and a comparison of accident statistics between the straight tail (mod 33) and the V-tail (mod 35) led to production stop for model 35.

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This individual aircraft was pilot tested in 1947 at Wichita, Kansas, and imported from the United States in 1987.

Classed as a veteran plan in 1997 - experimental class in 1998 after extensive renovation.