| 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 |

