TECHNICAL DESCRIPTION:Empty Weight 283 kgMax. GTOW 500 kgLength 4740 mmHeight 2850 mmProp. Diameter 1,75 mRotor Diameter 8,5 mChord Diameter 0,20 mFuel Consumption 15 l/ hFuel Type RegularFuel Tank Capacity 2x33 lAirframe Fuselage CarbonPropeller CompositeRotor Head Produced by Niki Rotor Aviation Inc.Pre-rotator 200 – 220 rpmPower Outlet 12 Volt

PERFORMANCEEngine Type Rotax 912 ULS/ 914 ULPower 100 hp/ 115 hpMax. Speed 190 kmMin. Speed 35 km/ hCruise Speed 160 km/ hVertical Speed 3 - 7 m/sMax. Altitude 3000 m/ sTake-off Roll 0-150 mLading Roll 0-20 mEndurance 3,5 h with 30 min reserve

The Art of Flying

BASIC EQUIPMENTAluminum Rotor Blades Altimeter Dual controlsPropeller E-prop/DUC/Luga Prop Airspeed IndicatorMagnetic CompassRotor Brakes Wheels Brakes Rotor rpm tachometerTwo side Doors Electric Starter and TrimsEngine Mount Instruments

OPTIONAL EQUIPMENT:Kanardia Nesis EFIS/ EMS and GPSTransponderCom RadioMetallic ColorColor with Décor & DesignLanding LightsLuxury InteriorStrobe and NAV LightsWheel PantsCabin HeatingSchool SetHead SetShading

21 Industrial Area “Praveshki Hanove” 2161, Pravets, BulgariaТ: +359 887 31 00 05 | E: info@nikiaviation.com