R44 RAVEN I / CLIPPER I

It’s the perfect balance of cost and capability. A Lycoming O-540 carbureted engine with carburetor heat assist keeps operating expenses and pilot workloads low. The Raven I and Clipper I are built on an aluminum monocoque and powder-coated steel tube structure — providing a light and sturdy airframe, while an aerodynamic fuselage optimizes airspeed and fuel economy. Responsive handling is provided by hydraulically boosted controls that eliminate cyclic and collective feedback. A roomy cabin maximizes visibility for every passenger, and our two bladed rotor system frees up hangar space upon landing.

Our patented Cyclic design offers increased safety, comfort and ease of operation for pilots:

• Minimizes the risk of interference from passengers or objects in the cockpit.
• Requires minimal physical effort to operate, reducing pilot fatigue during long flights.
• Eliminates the need for dual independent controls, simplifying operation and reducing mechanical complexity

The Clipper I can be equipped with fixed-utility floats to provide an extra layer of safety for over water operations. These floats remain fully inflated, add approximately 50 lbs to the aircraft’s empty weight and reduce cruise speed by approximately 10 knots.