Aircraft › Cessna › Cessna 414 › Cessna 414A Chancellor
Cessna 414A Chancellor
The FAA approved the 414A Chancellor in September 1977. Two turbocharged Continental TSIO-520-NB engines of 310 horsepower, or TSIO-520-N engines on the first 200 airplanes, turn three-blade propellers up to 76.5 inches across. The data sheet gives a maximum take-off weight of 6,750 lb, or 3,062 kg, six, seven or eight seats, and 204 or 206 US gallons of usable fuel in the two wing tanks, depending on the serial number. Its ICAO code is C414. No acceptable source read gives its dimensions or speeds, so this page has no drawing.
- Seats
- About 6 (up to 8)
- Engines
- Two piston engines on the wings: Continental TSIO-520-NB (TSIO-520-N on early airplanes)
- Max takeoff weight
- 6,800 lb (3,062 kg)
Photos from members
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Specifications
| Fuel capacity | 200 US gal (772 L) |
|---|---|
| Status | Still flying with a few operators |
| Type codes | ICAO C414 |