Colossal performance in a compact package: The R22 features exceptional tail rotor authority for precise maneuvering. An aluminum monocoque and powder-coated steel tube structure provides a lightweight, yet robust airframe while the aerodynamic fuselage optimizes airspeed and fuel economy. The Lycoming’s proven O-360 engine is derated to provide reserve power and better performance at high altitudes and in hot weather. It comes with the Robinson’s signature Cyclic and efficient two-bladed rotor system, and a crashworthy fuel system. In other words: it’s anything but "Beta".
The R22 is powered by a Lycoming O-360 four-cylinder piston engine that is derated to 131 horsepower for takeoff and 124 horsepower for cruise at 2652 RPM, giving the engine long life and unmatched reliability.
The R22 features a Crashworthy Fuel System with a Bladder Tank designed to prevent fuel leakage and reduce the risk of fire in the event of a crash. The system incorporates several features and design elements to enhance safety for both the helicopter and its occupants. The R66's fuel tank is constructed of an aluminum enclosure containing a flexible, puncture- and tear-resistant bladder that can withstand significant impact without rupturing. Additionally, the fuel system includes flexible joints or self-sealing breakaway couplings that absorb energy and prevent breakage. These are designed to disconnect safely and seal off the fuel line if excessive force is applied, preventing fuel spillage.
Automatic Clutch Engagement simplifies the starting procedure and reduces the possibility of overspeed during startup.
The Low Voltage Light informs the pilot of a low voltage condition and check the operation of the alternator, generator, or voltage regulator.
The R22's Carburetor Heat Assist feature enhances safety and reduces pilot workload by automatically adding carb heat when the collective is lowered and reducing carb heat when the collective is raised.
The RPM Governor monitors the rotor and engine's RPMs and adjusts them to keep the rotor's RPM constant. This allows the pilot to maintain the rotor's RPM in the green at all times during flight without having to make throttle adjustments.
The Low Fuel Light (LOW FUEL) alerts the pilot to the need to monitor the aircraft's fuel level. It is actuated by sensors in the fuel system and are independent of gage indicators Fuel exhaustion is a major cause of helicopter accidents, so it's important to pay attention to the low fuel light.
ITEM | Beta II |
---|---|
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 (16.9 gal) | 101 lb (46 kg) |
Auxiliary Fuel (17.0 gal) | 102 lb (46 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 |