Empty Weight | 285 kg |
Max. GTOW | 560 kg |
Lenght | 4550 mm |
Height | 2850 mm |
Prop. Diameter | 1,75 m |
Rotor Diameter | 8,5 m |
Chord Diameter | 0,21 m |
Fuel Consumption | 15 l/h |
Fuel Type | Regular |
Fuel System | Dual Carbs/ Fuel Injection (iS Series) |
Fuel Tank Capacity | 70 Liter (18.5 US gallons) |
Airframe Fuselage | Carbon |
Propeller | Composite |
Rotor Head | Produced by Niki Ltd. |
Pre-rotator | 200 – 220 rpm |
Power Outlet | 12 Volt |
Engine Type | Rotax 912 ULS/ 914 UL |
Power | 100 hp |
Speed Vne | 180 km |
Min. Speed | 35 km/ h |
Cruise Speed | 135 km/ h |
Vertical Speed | 3 – 5 m/s |
Max. Altitude | 3000 m |
Take-off Roll | 0-150 m |
Lading Roll | 0-20 m |
Endurance | 4 h with 30 min reserve |
Aluminum Rotor Blades Trendak | Propeller E-prop | Front Glass (transparent) |
Rotor Brakes | Two-sided Doors | Altimeter |
Aircraft tires | Leather interior | Wheels Brakes |
Electric Starter and Trims | Double controls | Airspeed indicator |
Magnetic Compass | Rotor rpm tachometer |