Robinson R 22 BETA II

The Robinson R22 Beta II is flown throughout the world for many applications, ranging from flight training to livestock mustering to patrolling pipelines that require dependability, low operating costs and performance.

The R22 Beta II incorporates a Lycoming O-360 four-cylinder, carburetor-equipped engine fueled with 100L grade aviation gasoline. This 145 hp engine is derated to 131 hp for five minutes at takeoff and 124 hp for continuous operation. A powerful engine, a lightweight steel-tube airframe, and aerodynamic shape gives the R22 a cruise speed of up to 90 kts and an average fuel consumption of only 7-10 gallons per hour.

The R22 seats two adults and occupants have panoramic views due to R22’s large windows. Acoustical foam lowers cabin noise. A heavy-duty muffler and low tail-rotor tip speed lessen flyover noise.

  ⇒   R22 BETA II Specification    ⇐  R22 BETA II Price configuration   ⇐


R 22 ENG

R22 BETA II Specifications
Engine TypeLycoming O-360 four-cylinder, carbureted
Horsepowerderated to 131 hp for takeoff and 124 for continuous
Maximum Gross Weight622 kg
Approximate Empty Weight
(including oil and standard avionics)
399 kg
Standard Fuel (64 l)46 kg
Auxiliary Fuel (36 l)25 kg
Passengers and Baggage with Standard Fuel176 kg
Max Airspeed (Vne)212,4 km/h
Cruise Speedup to 198 km/h
Maximum Range
(with Auxiliary Fuel)
approx 425 km
Hover Ceiling (IGE) at 622 kg2900 m
Hover Ceiling (OGE) at 590 kg2440 m
Max Operating Altitudeok. 4300 m
Electrical System14 volt