1974 Piper Aztec PA-23-250E turbo

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Description

The Piper PA-23 Aztec is a twin-engined light aircraft that was first introduced in 1950. It was developed as a commercial aircraft, but has also been widely used as a personal transport and in military service. The PA-23-250E Turbo is a turbocharged version of the Aztec, which was produced from 1974 to 1984. It is powered by two Lycoming TIO-540-C1A6 turbocharged engines, each producing 250 hp. The aircraft is equipped with a retractable tricycle landing gear, has a maximum speed of 211 mph, and a range of 1,231 miles. It can carry up to 6 passengers and has a useful load of 1,106 lbs.

Features

  • Total Time: 4161
  • Engine(s):
  • Engine 1
  • LYCOMING
  • 250 HP
  • 256 SMOH
  • 2000 TBO
  • Engine 2
  • LYCOMING
  • 250 HP
  • 1440 SMOH
  • 2000 TBO
  • Prop(s):
  • HARTZELL
  • 55 SPOH
  • 55 SPOH
  • Modifications/Conversions:
  • Metro Long Range Fuel system
  • JPI EDM 730 Digital engine monitor
  • JPI fuel flow
  • New 406 ELT
  • Recent Glass including Speed Slope one piece WS
  • Avionics:
  • Garmin GTN 750 Txi Touchscreen GPS WAAS
  • Garmin GNS430 GPS Com/Nav
  • Aspen 1000 PFD with HSI
  • Garmin G 5 Indicator
  • Appereo Status ESG Transponder with ADSB
  • HSI
  • Garmin GMA 345 Audio panel
  • Bendix Alitmatic V with FD
  • Additional Equipment:
  • Speed slope one piece windshield
  • LR fuel
  • Strobe lights
  • Beacon light
  • Position lights
  • Landing light
  • Taxi light

1974 Piper Aztec PA-23-250E turbo 0 reviews

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