1978 Aerostar 600A

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The Aerostar 600A is a twin-engine, light business aircraft that was manufactured by Piper Aircraft Corporation. It is derived from the earlier Piper PA-60 Aerostar 601. The 600A features a wider cabin, more powerful engines, and improved avionics. The Aerostar 600A has a maximum speed of 294 mph, a range of 1,600 miles, and a service ceiling of 25,000 feet. It can accommodate up to seven passengers and has a maximum takeoff weight of 6,000 lbs.


  • Total Time: 5300
  • The Engines are Lycoming IO-540-K1J5 rated 290 HP overhauled in 2007.
  • Both engines compression in the 70s.
  • Both RE magnetos were replaced last year.
  • Both engines have fine wire spark plugs.
  • Garmin GMA 340 Audio Panel
  • Garmin GTN 750 w/Century Flight Systems NSD-360A
  • Garmin GTX 345 Transponder
  • Garmin GNC 255A Nav/Com w/ Garmin GI-106B VOR/ILS/GS
  • King KN64 DME
  • Century IV Autopolit
  • Avidyne FlightMax 850
  • Shaden Digiflow-L Fuel Flow Management System
  • JPI EDM 760 Engine Monitoring System w/EGT/CHT

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