The R22 is a single-engine helicopter, mostly used for utility, passenger transport, surveys, and training.
The two-seat R22 Beta II helicopter has been a reliable workhorse for over 40 years, excelling in various applications. Its compact, two-bladed rotor system minimizes hangar space, while the T-bar cyclic allows easy access. Featuring a lightweight yet durable aluminum and steel structure, its aerodynamic design enhances speed and fuel efficiency. Powered by Lycoming’s derated O-360 engine, it offers reserve power and improved performance in hot weather and high altitudes.
Capacity | |
Passenger transportation | 1 pilot + 3 passengers |
Engine | Lycoming O-360, four cylinder, carbureted |
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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 (29.5 gal) | 16.9 gal (64 L) capacity / 101 lb (46 kg) |
Auxiliary Fuel (17.0 gal) | 16.9 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 |