Names and dates
| Market original model designation | СА | | Market model designation (english translation or spelling) | SA | | Project start date | 1995 | | Date of prototype completion | 1999 | | Country of manufacture | Ukraine |
People involved
| Anatoly Stafiychuk {Анатолий Стафийчук} | Constructor, Test pilot | | Vasily Artemchuk {Васили Артемчук} | Consultant |
Config info
| Rotorcraft type | Helicopter |
Weights
| Maximum Takeoff Weight (MTOW) | | | Manufacturers empty weight (MEW) | |
External dimensions
| Main landing gear wheel diameter | | | Nose landing gear wheel diameter | |
Main rotor
| Cyclic pitch control | Yes | | Collective control | Yes | | Main rotor diameter | | | Main rotor angular speed | | | Number of blades | 2 | | Main rotor blade tip chord | | | Main rotor blade root chord | | | Main rotor blade airfoil | NACA 23012 |
Tail rotor
| Tail rotor diameter | | | Tail rotor angular speed | | | Number of blades | 2 | | Tail rotor blade chord | |
Powerplant
| Engine model | К-750 / МТ-10 | | Engine model (english translation or spelling) | K-750 / MT-10 | | Engine type | Piston | | Number of engines | 1 | | Total maximum power | | | Angular speed at max power | |
Fuel system
Performance
| Maximum horizontal flight speed (Vh) | | | Best rate of climb | | | Maximum service ceiling | | | Maximum flight endurance | |
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