1978 Cessna 414A Chancellor
Description
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.
Features
- 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
Location
