Attribute | Cessna 310 × | Cessna 411 × |
---|---|---|
General | ||
Manufacturer | Cessna | Cessna |
1↑Model | Cessna 310 | Cessna 411 |
Country | United States | United States |
Manufactured from (year) | 1954 | 1962 |
Manufactured to (year) | 1980 | 1968 |
Type | Twin Turboprops | Twin Turboprops |
Icao | C310 | C411 |
Performance | ||
Engine | 2x Continental IO-470-M | 2x Continental GTSIO-520 |
Power, hp (hp) | 240 | 340 |
Max cruise speed (km/h) | 352 | 432 |
Approach speed (km/h) | 126 | 135 |
Travel range (km) | 1,611 | 2,037 |
Service ceiling (m) | 6,096 | 7,925 |
Rate of climb (m/sec) | 8.64 | 8.13 |
Take off distance (m) | 507 | 580 |
Landing distance (m) | 546 | 553 |
Weights | ||
Max take off weight (kg) | 2,087 | 2,948 |
Max landing weight (kg) | 1,293 | 1,973 |
Max payload (kg) | 790 | 975 |
Fuel tank capacity (l) | 473 | 742 |
Baggage volume (m³) | 1 | 0.9 |
Dimensions | ||
Seats | 5 | 6 |
Cabin height (m) | 1.2 | 1.3 |
Cabin width (m) | 1.2 | 1.4 |
Cabin length (m) | 2.4 | 3.42 |
Exterior length (m) | 8.3 | 10.2 |
Tail height (m) | 3.25 | 3.52 |
Fuselage diameter (m) | 1.3 | 1.6 |
Wing span (m) | 10.7 | 12.15 |
Wing tips | No Winglets | No Winglets |