Cessna 414 Chancellor [+]Compare [E]dit [H]istory
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Object «Cessna 414 Chancellor» has attributes [Show empty attributes][Hide empty attributes]
| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Cessna |
| Model | Cessna 414 Chancellor |
| Country | United States |
| Manufactured from | 1968 year |
| Manufactured to | 1985 year |
| Type | Twin Turboprops |
| Icao | C414 |
| Performance | |
| Engine | 2x Continental TSIO-520-NB |
| Power, hp | 310 hp |
| Power, lbf | Add |
| Avionics | Add |
| Max cruise speed | 435 km/h |
| Approach speed | 126 km/h |
| Travel range | 2,459 km |
| Fuel economy | Add |
| Service ceiling | 9,388 m |
| Rate of climb | 7.72 m/sec |
| Take off distance | 665 m |
| Landing distance | 718 m |
| Weights | |
| Max take off weight | 3,061 kg |
| Max landing weight | 2,697 kg |
| Max payload | 802 kg |
| Fuel tank capacity | 806 l |
| Baggage volume | 2.4 m³ |
| Dimensions | |
| Seats | 1 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | 1.3 m |
| Cabin width | 1.4 m |
| Cabin length | 3.5 m |
| Exterior length | 11.1 m |
| Tail height | 3.5 m |
| Fuselage diameter | 1.5 m |
| Wing span | 13.46 m |
| Wing tips | No Winglets |
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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 25, 2021 (45 fields were changed)
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