1973 Piper Seneca I

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Description

Piper Seneca I is a twin-engine light aircraft developed by Piper Aircraft. It was introduced in 1973 and is powered by two Lycoming IO-360 engines. It is an all-metal, low-wing, six-seat aircraft with retractable tricycle landing gear. The Seneca I has a cruise speed of 145 knots and a range of 615 nautical miles. It has stall speeds of 64 knots and is capable of performing short field takeoffs and landings. The Piper Seneca I is a great option for pilots looking for a reliable and economical twin-engine aircraft.

Features

  • Total Time: 11278
  • Engine 1 Time: 3019 SMOH
  • Engine 2 Time: 2861 SMOH
  • Prop 1 Time: 623 SMOH
  • Prop 2 Time: 371 SMOH
  • IO-360 C1E6 3019 SMOH
  • LIO-360 C1E6 SMOH 2861.7
  • Compressions mid to high 70's
  • Garmin 430WAAS
  • King KX-160
  • GMA 330 Transponder
  • GMA 327 Audio Panel
  • ADSB-out
  • 6 place intercom
  • MX-20 GPS map

Location

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