1986 Piper JetProp

The Piper JetProp is a twin-engine turboprop aircraft produced by Piper Aircraft. It was introduced in 1984 and was in production until late 1986. The aircraft is powered by two Pratt & Whitney Canada PT6A-21 turbines, each producing 650 shaft horsepower. It has a maximum cruise speed of 260 knots and a range of 1,400 nm. The aircraft can carry up to nine passengers and has a maximum takeoff weight of 8,000 lbs. The Piper JetProp is equipped with a three blade propeller system and is capable of taking off and landing on short runways.