Attribute | ![]() Cessna 425 Conquest I × | ![]() Cessna 402 Businessliner × |
---|---|---|
General | ||
Manufacturer | Cessna | Cessna |
Model | Cessna 425 Conquest I | Cessna 402 Businessliner |
Country | United States | United States |
Manufactured from (year) | 1980 | 1966 |
Manufactured to (year) | 1986 | 1985 |
Type | Twin Turboprops | Twin Turboprops |
Icao | C425 | C402 |
Performance | ||
Engine | 2x Pratt & Whitney Canada PT6A-112 | 2x Continental TSIO-520-VB |
Power, hp (hp) | 450 | 325 |
Avionics | - | Bendix King Avionics |
Max cruise speed (km/h) | 491 | 428 |
Approach speed (km/h) | 146 | 126 |
Travel range (km) | 3,048 | 2,358 |
Service ceiling (m) | 10,577 | 8,199 |
Rate of climb (m/sec) | 9.45 | 7.37 |
Take off distance (m) | 741 | 669 |
Landing distance (m) | 654 | 757 |
Weights | ||
Max take off weight (kg) | 3,719 | 3,107 |
Max landing weight (kg) | 2,970 | 2,546 |
Max payload (kg) | 725 | 950 |
Fuel tank capacity (l) | 1,385 | 780 |
Baggage volume (m³) | 1.8 | 1.9 |
Dimensions | ||
Seats | 8 | 8 |
Cabin height (m) | 1.3 | 1.3 |
Cabin width (m) | 1.4 | 1.4 |
Cabin length (m) | 3.2 | 3.4 |
Exterior length (m) | 10.9 | 11.1 |
Tail height (m) | 3.8 | 3.5 |
Fuselage diameter (m) | 1.55 | 1.55 |
Wing span (m) | 13.4 | 13.5 |
Wing tips | No Winglets | No Winglets |