Attribute | ![]() Cessna 210 Centurion × | ![]() Piper PA-24 Comanche × |
---|---|---|
General | ||
Manufacturer | Cessna | Piper Aircraft |
Model | Cessna 210 Centurion | Piper PA-24 Comanche |
Country | United States | United States |
Manufactured from (year) | 1957 | 1957 |
Manufactured to (year) | 1986 | 1972 |
Type | Private Single Engine | Private Single Engine |
Icao | C210 | PA24 |
Performance | ||
Engine | 1x Continental IO-520L | 1x Lycoming IO-540 |
Power, hp (hp) | 300 | 260 |
Max cruise speed (km/h) | 378 | 313 |
Approach speed (km/h) | 107 | 102 |
Travel range (km) | 1,667 | 1,971 |
Service ceiling (m) | 8,230 | 6,706 |
Rate of climb (m/sec) | 4.72 | 7.62 |
Take off distance (m) | 660 | 430 |
Landing distance (m) | 460 | 370 |
Weights | ||
Max take off weight (kg) | 1,814 | 1,315 |
Max landing weight (kg) | 1,577 | 1,315 |
Max payload (kg) | 769 | 622 |
Fuel tank capacity (l) | 329 | 341 |
Baggage volume (m³) | 0.6 | - |
Dimensions | ||
Seats | 6 | 6 |
Cabin height (m) | 1.2 | 1.19 |
Cabin width (m) | 1.1 | 1.14 |
Cabin length (m) | 2.4 | 2.7 |
Exterior length (m) | 8.6 | 7.62 |
Tail height (m) | 2.95 | 2.29 |
Fuselage diameter (m) | 1.2 | 1.25 |
Wing span (m) | 11.2 | 11 |
Wing tips | No Winglets | No Winglets |