LOOKING TO PURCHASE A NEW ROBINSON HELICOPTER IN 2023?

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Four-seat R44 RAVEN II and CLIPPER II helicopters are high performing, reliable, and easy to maintain. R44s have a two-bladed rotor system, T-bar cyclic, streamlined instrument panels, and a crashworthy fuel system. An aluminum monocoque and powder-coated steel tube structure provides a lightweight, yet robust airframe while the aerodynamic fuselage optimizes airspeed and fuel economy. Hydraulically boosted controls eliminate cyclic and collective feedback forces and provide responsive handling. A low tail-rotor tip speed and large cambered tail reduce flyover noise. Raven II and Clipper II helicopters are powered by Lycoming’s IO-540 fuel injected engine. The IO-540 delivers improved altitude performance, increased payload, and eliminates the need for carburetor heat.

Four-seat R44 RAVEN I and CLIPPER I helicopters are high performing, reliable, and easy to maintain. R44s have a two-bladed rotor system, T-bar cyclic, streamlined instrument panels, and a crashworthy fuel system. An aluminum monocoque and powder-coated steel tube structure provides a lightweight, yet robust airframe while the aerodynamic fuselage optimizes airspeed and fuel economy. Hydraulically boosted controls eliminate cyclic and collective feedback forces and provide responsive handling. A low tail-rotor tip speed and large cambered tail reduce flyover noise. Raven I and Clipper I helicopters are powered by Lycoming’s O-540 carbureted engine with carburetor heat assist that automatically adjusts carburetor heat, enhancing safety and reducing pilot workload.

The two-seat R44 CADET is a versatile helicopter ideally suited for flight schools and operators who want the economy of a small helicopter without sacrificing the power and performance of a large helicopter.

The Cadet has the same airframe, rotor system and Lycoming O-540 engine as the proven R44 Raven I. The differences are the Cadet’s aft compartment is reconfigured for cargo, the maximum gross weight is reduced to 2200 lb, and the engine power is derated to 210 hp take-off and 185 hp continuous. The lower weight and derated power provide increased performance margins at high altitudes and extend the time between overhauls to 2400 hours.

Cadets feature streamlined instrument panels and a crashworthy fuel system.