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

21 Industrial Area “Praveshki Hanove" 2161, Pravets, Bulgaria T: +359 887 31 00 05 | E: info@nikiaviation.com 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 Decor & Design Landing Lights Luxury Interior Strobe and NAV Lights Wheel Pants Cabin Heating School Set Head Set Shading