1978 Cessna 414A Chancellor

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The Cessna 414A Chancellor is a twin-engine, high-performance aircraft that was introduced in the 1970s. It was designed to be a fast, comfortable, and efficient business and personal aircraft. It can seat up to six passengers and has a range of around 1,500 miles. It is powered by two TSIO-520-J engines, which produce around 310 horsepower each. The Cessna 414A Chancellor has a cruising speed of around 250 knots (288 mph) and a maximum altitude of 25,000 feet. It is known for its reliability and ease of maintenance, and it has a strong safety record.


  • Total Time: 4810 Hours
  • Engine Hours:
  • 680 Hours SMOH Left/Right
  • Prop Hours:
  • 3-Blade McCauley Props
  • Hot Props
  • Polished Spinners
  • Avionics:
  • Garmin GNS430 IFR GPS/NAV/COM
  • Cessna NAV/COM
  • Cessna 400 Autopilot
  • Cessna RMI
  • Cessna DME
  • Cessna ADF
  • Radio Altimeter
  • Collins Color Weather Radar
  • Shadin Fuel Flow Computer
  • Bendix-King KT76A Transponder
  • Copilot Instruments
  • Additional Features:
  • Air Conditioning
  • Overhead Air Vents & Reading Lamps
  • Electric Pitch Trim
  • Hobbs Meter
  • Dual Push-to-Talk Switches
  • Dual Toe Brakes

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