

Flight Performance:
| VNE | 105 kt |
| NORMAL CRUISE | 90-95 kt |
| RANGE | 380 Miles (700Km) |
| RATE OF CLIMB | 1250 F.P.M. AT 2300 Lb |
| SERVICE CEILING | 14000ft |
| POWERPLANT | Fuel Injected Lycoming IO-540, 320 Hp |
Specifications
| GROSS WEIGHT | 1270 Kg (2800 Lb) |
| EMPTY WEIGHT | 817 Kg (1800 Lb) |
| USEFUL LOAD | 454 Kg (1000 Lb) |
| FUEL CAPACITY | 215 Lt (57 Gal) |
| MAIN ROTOR DIMENSION | 10.05m (33′ 0″) |
| TAIL ROTOR DIMENSION | 1.75m (5′ 9″) |
| FUSELAGE LENGTH | 9.3m (30′ 6″) |
| HEIGHT | 2.61m (8′ 7″) |
| WIDTH | 1.52m (5′) |
| SEATS | 4 or 4.5 |
| MAX CREW | 1 |
| Wing Area | 4 |