The two-seat R22 Beta II helicopter is a proven workhorse that has delivered exceptional performance in a variety of applications for over forty years. The R22 has a two-bladed rotor system which requires minimum hangar space, T-bar cyclic for easy entry and exit, and a crashworthy fuel system. An aluminum monocoque and powder-coated steel tube structure provides a lightweight, yet robust airframe while the aerodynamic fuselage optimizes airspeed and fuel economy. The R22 is powered by Lycoming’s proven O-360 engine that is derated to provide reserve power and better performance at high altitudes and in hot weather.
Specifications
| Engine | Lycoming O-360, four cylinder, carbureted |
| Horsepower | Derated to 131 hp for takeoff and 124 continuous |
| Maximum Gross Weight | 1370 lb (622 kg) |
| Approximate Empty Weight (including oil & standard avionics) | 880 lb (399 kg) |
| Main Fuel | 16.9 gal (64 L) capacity / 101 lb (46 kg) |
| Auxiliary Fuel | 9.4 gal (35.9 L) capacity / 56 lb (25 kg) |
| Pilot, Passengers, and Baggage (with maximum fuel) | 389 lb (176 kg) |
| Cruise Speed at Maximum Gross Weight | Up to 96 kts (178 km/h) |
| Maximum Range (no reserve) | Approximately 250 nm (460 km) |
| Hover Ceiling IGE at Maximum Gross Weight | 9400 ft |
| Hover Ceiling OGE at Maximum Gross Weight | 8000 ft |
| Maximum Operating Altitude | 14,000 ft |
| Electrical System | 14 volt |