Comparison of Cessna 402 Businessliner and Cessna 414 Chancellor [S]ave
| Attribute |  Cessna 414 Chancellor × |  Cessna 402 Businessliner × |
|---|---|---|
| General | ||
| Manufacturer | Cessna | Cessna |
| Model | Cessna 414 Chancellor | Cessna 402 Businessliner |
| Country | United States | United States |
| Manufactured from (year) | 1968 | 1966 |
| Manufactured to (year) | 1985 | 1985 |
| Type | Twin Turboprops | Twin Turboprops |
| Icao | C414 | C402 |
| Performance | ||
| Engine | 2x Continental TSIO-520-NB | 2x Continental TSIO-520-VB |
| Power, hp (hp) | 310 | 325 |
| Avionics | - | Bendix King Avionics |
| Max cruise speed (km/h) | 435 | 428 |
| Approach speed (km/h) | 126 | 126 |
| Travel range (km) | 2,459 | 2,358 |
| Service ceiling (m) | 9,388 | 8,199 |
| Rate of climb (m/sec) | 7.72 | 7.37 |
| Take off distance (m) | 665 | 669 |
| Landing distance (m) | 718 | 757 |
| Weights | ||
| Max take off weight (kg) | 3,061 | 3,107 |
| Max landing weight (kg) | 2,697 | 2,546 |
| Max payload (kg) | 802 | 950 |
| Fuel tank capacity (l) | 806 | 780 |
| Baggage volume (m³) | 2.4 | 1.9 |
| Dimensions | ||
| Seats | 1 | 8 |
| Cabin height (m) | 1.3 | 1.3 |
| Cabin width (m) | 1.4 | 1.4 |
| Cabin length (m) | 3.5 | 3.4 |
| Exterior length (m) | 11.1 | 11.1 |
| Tail height (m) | 3.5 | 3.5 |
| Fuselage diameter (m) | 1.5 | 1.55 |
| Wing span (m) | 13.46 | 13.5 |
| Wing tips | No Winglets | No Winglets |
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