(one conventional unit corresponds to one USD at the exchange rate on the day of payment)

Basic configuration:

  Aircraft includes the following:  cockpit, engine control system, fuel system, flaps, ailerons, elevator and rudder; 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.

  The aircraft surfaces are covered with primer coating and prepared for painting.