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| Exterior view |
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| Interior view |
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Cessna 414
| Passenger Capacity: |
4-6 |
Lavatory Style: |
- |
| Airspeed (mph): |
271 |
Range (miles): |
1528 |
| Cabin Width (ft): |
- |
Cabin Height (ft): |
- |
| Cabin Length (ft): |
- |
Baggage Capacity: |
- |
The Cessna 414 is a light, pressurized, twin-engine transport aircraft built by Cessna.
The Cessna 414 was developed to appeal to the current users of un-pressurized twin-engine aircraft and is based on the fuselage of the Cessna 421. The Cessna 414 is a low-wing cantilever monoplane with a conventional tail unit and a retractable tricycle landing gear. It is powered by two wing mounted 310hp (231kW) Continental TSIO-520-J flat-six piston engines.
An improved variant, the Cessna 414A Chancellor, was later introduced with the major change being a re-designed and increased-span wing with integral fuel tanks and an extended nose to give more baggage space.
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