1986 Piper JetProp

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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.


  • Total Time: 3366
  • Engine 1 Time: 1310 SNEW
  • Prop 1 Time: 15 SPOH
  • Garmin panel
  • G600 with SVT
  • GTN750/GTN650
  • King KFC150 Autopilot
  • Garmin GTX 345 transponder
  • Shadin Engine Monitor

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