2006 Aerocomp Comp Air 8 Turbine

The Aerocomp Comp Air 8 is a single-engine turboprop aircraft that was manufactured by the Aerocomp company. It was designed as a light utility aircraft and was first flown in 2006. The aircraft is powered by a Pratt & Whitney PT6 turbine engine and is capable of carrying up to six passengers. The aircraft features a pressurized cabin, retractable landing gear, and a modern avionics suite. The Comp Air 8 is capable of cruising at speeds of up to 285 knots and has a maximum range of 1,400 nautical miles. The aircraft is also capable of operating at altitudes of up to 25,000 feet and is one of the most fuel-efficient turboprop aircraft in its class.