New Robinson R22 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.
|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 and 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, Passenger and Baggage
with Standard Fuel
|389 lb (176 kg)|
|Max Airspeed (Vne)||102 kts (117 mph)|
|Cruise Speed||up to 96 kts (110 mph)|
|approx 250 nm (288 sm)|
|Hover Ceiling IGE @ 1370 lb||9400 ft|
|Hover Ceiling OGE @ 1300 lb||8000 ft|
|Max Operating Altitude||14,000 ft|
|Electrical System||14 volt|
Price and specifications subject to change without notice. Aircraft is subject to prior sale or withdrawal from market. It is the buyer responsibility to verify data herein prior to purchase.