Chayair Sycamore

The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.

[1][2] The Sycamore features a single main rotor, a two-seats-in-tandem open or optionally enclosed cockpit, tricycle landing gear with wheel pants and a four-cylinder, liquid and air-cooled, four-stroke, dual-ignition turbocharged 115 hp (86 kW) Rotax 914F engine in pusher configuration.

[1][2] The aircraft fuselage is made from bolted-together aluminum tubing and mounts a 9.10 m (29.9 ft) diameter Advanced Kinetics rotor.

The tailplane features five vertical tail surfaces for improved directional stability.

[1][2] By December 2012 one example had been registered in the United States with the Federal Aviation Administration in the Experimental - Amateur-built category.