| 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 |