Attribute | ![]() Cessna 414 Chancellor × | ![]() Cessna 411 × |
---|---|---|
General | ||
Manufacturer | Cessna | Cessna |
Model | Cessna 414 Chancellor | Cessna 411 |
Country | United States | United States |
Manufactured from (year) | 1968 | 1962 |
Manufactured to (year) | 1985 | 1968 |
Type | Twin Turboprops | Twin Turboprops |
Icao | C414 | C411 |
Performance | ||
Engine | 2x Continental TSIO-520-NB | 2x Continental GTSIO-520 |
Power, hp (hp) | 310 | 340 |
Max cruise speed (km/h) | 435 | 432 |
Approach speed (km/h) | 126 | 135 |
Travel range (km) | 2,459 | 2,037 |
Service ceiling (m) | 9,388 | 7,925 |
Rate of climb (m/sec) | 7.72 | 8.13 |
Take off distance (m) | 665 | 580 |
Landing distance (m) | 718 | 553 |
Weights | ||
Max take off weight (kg) | 3,061 | 2,948 |
Max landing weight (kg) | 2,697 | 1,973 |
Max payload (kg) | 802 | 975 |
Fuel tank capacity (l) | 806 | 742 |
Baggage volume (m³) | 2.4 | 0.9 |
Dimensions | ||
Seats | 1 | 6 |
Cabin height (m) | 1.3 | 1.3 |
Cabin width (m) | 1.4 | 1.4 |
Cabin length (m) | 3.5 | 3.42 |
Exterior length (m) | 11.1 | 10.2 |
Tail height (m) | 3.5 | 3.52 |
Fuselage diameter (m) | 1.5 | 1.6 |
Wing span (m) | 13.46 | 12.15 |
Wing tips | No Winglets | No Winglets |