Attribute | ![]() Cessna 421 Golden Eagle × | ![]() Cessna 402 Businessliner × |
---|---|---|
General | ||
Manufacturer | Cessna | Cessna |
Model | Cessna 421 Golden Eagle | Cessna 402 Businessliner |
Country | United States | United States |
Manufactured from (year) | 1967 | 1966 |
Manufactured to (year) | 1985 | 1985 |
Type | Twin Turboprops | Twin Turboprops |
Icao | C421 | C402 |
Performance | ||
Engine | 2x Continental GTSIO-520-H | 2x Continental TSIO-520-VB |
Power, hp (hp) | 375 | 325 |
Avionics | - | Bendix King Avionics |
Max cruise speed (km/h) | 474 | 428 |
Approach speed (km/h) | 141 | 126 |
Travel range (km) | 2,754 | 2,358 |
Service ceiling (m) | 9,205 | 8,199 |
Rate of climb (m/sec) | 9.86 | 7.37 |
Take off distance (m) | 708 | 669 |
Landing distance (m) | 699 | 757 |
Weights | ||
Max take off weight (kg) | 3,379 | 3,107 |
Max landing weight (kg) | 2,330 | 2,546 |
Max payload (kg) | 764 | 950 |
Fuel tank capacity (l) | 780 | 780 |
Baggage volume (m³) | 2.3 | 1.9 |
Dimensions | ||
Seats | 8 | 8 |
Cabin height (m) | 1.3 | 1.3 |
Cabin width (m) | 1.4 | 1.4 |
Cabin length (m) | 3.45 | 3.4 |
Exterior length (m) | 11.2 | 11.1 |
Tail height (m) | 3.5 | 3.5 |
Fuselage diameter (m) | 1.55 | 1.55 |
Wing span (m) | 12.5 | 13.5 |
Wing tips | No Winglets | No Winglets |