Comparison of Cirrus SR20 and Pilatus PC-6 Turbo Porter [S]ave
| Attribute |  Cirrus SR20 × |  Pilatus PC-6 Turbo Porter × |
|---|---|---|
| General | ||
| Manufacturer | Cirrus Aircraft | Pilatus Aircraft |
| Model | Cirrus SR20 | Pilatus PC-6 Turbo Porter |
| Country | United States | Switzerland |
| Manufactured from (year) | 1999 | 1961 |
| Type | Private Single Engine | Private Single Engine |
| Performance | ||
| Engine | 1 X Continental IO-360-ES | 1× Pratt & Whitney PT6A-27 |
| Power, hp (hp) | 200 | 550 |
| Avionics | Cirrus Airframe Parachute System™ | Honeywell Avionics Suite |
| Max cruise speed (km/h) | 289 | 154 |
| Fuel economy (km/l) | 16.135 | 1.429 |
| Take off distance (m) | 450 | 59 |
| Landing distance (m) | 260 | 40 |
| Weights | ||
| Max take off weight (kg) | 6,724 | 6,107 |
| Max payload (kg) | 440 | 694 |
| Baggage volume (m³) | - | 0.03 |
| Dimensions | ||
| Seats | 3 | 1 |
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