TECHNICAL DESCRIPTION: Empty Weight Max. GTOW Length Height Prop. Diameter Rotor Diameter Chord Diameter Fuel Consumption Fuel Type Fuel Tank Capacity Airframe Fuselage Propeller Rotor Head Pre-rotator Power Outlet Engine Type Rotax 912 ULS/ 914 UL 283 kg Power 100 hp/ 115 hp 500 kg Max. Speed 190 km 4740 mm Min. Speed 35 km/ h 2850 mm Cruise Speed 160 km/ h 1,75 m Vertical Speed 3 - 7 m/s 8,5 m Max. Altitude 3000 m/ s 0,20 m Take-off Roll 0-150 m 15 l/ h Lading Roll 0-20 m Regular Endurance 3,5 h with 30 min reserve 2x33 l Carbon Composite Produced by Niki Rotor Aviation Inc. 200 – 220 rpm 12 Volt

BASIC EQUIPMENT Aluminum Rotor Blades Altimeter Dual controls Propeller E-prop/DUC/Luga Prop Airspeed Indicator Magnetic Compass Rotor Brakes Wheels Brakes Rotor rpm tachometer Two side Doors Electric Starter and Trims Engine Mount Instruments OPTIONAL EQUIPMENT: Kanardia Nesis EFIS/ EMS and GPS Transponder Com Radio Metallic Color Color with Décor & Design Landing Lights Luxury Interior Strobe and NAV Lights Wheel Pants Cabin Heating School Set Head Set Shading 21 Industrial Area “Praveshki Hanove” 2161, Pravets, Bulgaria Т: +359 887 31 00 05 | E: info@nikiaviation.