| 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 |