New R44 Raven II Helicopter

AIM HIGHER

Safety | Luxury | Support

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.

R44 Clipper II

The CLIPPER II may be equipped with either fixed utility or pop-out floats, offering safety for over-water travel. Designed for emergencies, pop-out floats inflate within 2-3 seconds of activation. When not in use, pop-out floats roll-up and stow in protective covers along the aircraft’s landing skids. The streamlined, low profile design minimizes drag and allows for easy entry and exit of the cabin. Fixed utility floats remain fully inflated, add approximately 50 pounds to the aircraft’s empty weight, and reduce cruise speed by approximately ten knots.

R44 Raven II Specifications

Engine: Lycoming IO-540, six cylinder, fuel injected

Horsepower: Derated to 245 for takeoff and 205 continuous

Fuel Capacity: 177 lb (80 kg) Main + 102lb (46kg) Aux Fuel

Range: Approximately 300 nm (550 km)

Rate of Climb: Over 1000 fpm

Max Altitude: 14,000 ft

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