Single engine utility helicopter

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.

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Technical Specifications

Capacity
Passenger transportation1 pilot + 3 passengers
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)
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
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