Attribute | Cessna 414 Chancellor × | Cessna T303 Crusader × |
---|---|---|
General | ||
Manufacturer | Cessna | Cessna |
Model | Cessna 414 Chancellor | Cessna T303 Crusader |
Country | United States | United States |
Manufactured from (year) | 1968 | 1979 |
Manufactured to (year) | 1985 | 1986 |
Type | Twin Turboprops | Twin Turboprops |
Icao | C414 | C303 |
Performance | ||
Engine | 2x Continental TSIO-520-NB | 2x Continental TSIO-520AE |
Power, hp (hp) | 310 | 250 |
Max cruise speed (km/h) | 435 | 400 |
Approach speed (km/h) | 126 | 115 |
Travel range (km) | 2,459 | 1,889 |
Service ceiling (m) | 9,388 | 7,620 |
Rate of climb (m/sec) | 7.72 | 7.52 |
Take off distance (m) | 665 | 530 |
Landing distance (m) | 718 | 440 |
Weights | ||
Max take off weight (kg) | 3,061 | 2,336 |
Max landing weight (kg) | 2,697 | 1,635 |
Max payload (kg) | 802 | 836 |
Fuel tank capacity (l) | 806 | 579 |
Baggage volume (m³) | 2.4 | 1.5 |
Dimensions | ||
Seats | 1 | 6 |
Cabin height (m) | 1.3 | 1.25 |
Cabin width (m) | 1.4 | 1.25 |
Cabin length (m) | 3.5 | 2.8 |
Exterior length (m) | 11.1 | 9.27 |
Tail height (m) | 3.5 | 4.06 |
Fuselage diameter (m) | 1.5 | 1.4 |
Wing span (m) | 13.46 | 11.9 |
Wing tips | No Winglets | No Winglets |