* Basic configuration:

  Aircraft includes the following:  cockpit, lower bean with engine control system, fuel system, flaps, ailerons, elevator and rudder; upper beam, engine bed with cowls and fillets; wing bracing struts, outer wing panels with hinged flaps and ailerons, tail fin with rudder, stabilizer with elevator; circuit breaker panel, pitot static tube, pilot’s seats with harnesses, flight intercom; flight navigation instruments: speed indicator US-350, altimeter VD-10К, vertical speed indicator VR-10М, magnetic compass KI-13, sideslip indicator, fuel indicator, aviation clock, direct-current voltmeter 0..30V, electrical battery 12V with capacity of 26 А/h, FIAMM GSF 22703, technical documentation and manuals.

  Engine Rotax 912 ULS (Austria) coming with integrated engine control electronic device FLYdat. Three-blade propeller R101 manufactured in Lugansk with ground-adjusted variable pitch, air-intake covers.

  Wheeled landing gear (nose and main landing gear units) with hydraulic brakes.

  Instrumentation panel prepared for installation of aircraft instruments.