R22
BETA II
SPECIFICATIONS
Rating | |
---|---|
Engine | Lycoming O-540, six 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) |
Standard Fuel (16.9 gal) | 101 lb (46 kg) |
Auxiliary Fuel (9.4 gal) | 56 lb (25 kg) |
Pilot, Passengers, and Baggage (with standard fuel) | 389 lb (176 kg) |
Max Airspeed (Vne) | 102 kts (189 km/h) |
Cruise Speed | up to 96 kts (178 km/h) |
Maximum Range (no reserve) | approx 250 nm (460 km) |
Hover Ceiling IGE at 1370 lb | 9400 ft |
Hover Ceiling OGE at 1300 lb | 8000 ft |
Maximum Operating Altitude | 14,000 ft |
Electrical System | 14 volt |