| Attribute | Pilatus PC-7 Mk II × | Cirrus SR20 × |
|---|---|---|
| General | ||
| Manufacturer | Pilatus Aircraft | Cirrus Aircraft |
| Model | Pilatus PC-7 Mk II | Cirrus SR20 |
| Country | Switzerland | United States |
| Manufactured from (year) | 1978 | 1999 |
| Type | Military Propellor Planes | Private Single Engine |
| Performance | ||
| Engine | 1 × Pratt & Whitney PT6A-25C | 1 X Continental IO-360-ES |
| Power, hp (hp) | 700 | 200 |
| Avionics | Honeywell Avionics | Cirrus Airframe Parachute System™ |
| Max cruise speed (km/h) | 291 | 289 |
| Fuel economy (km/l) | 4.697 | 16.135 |
| Take off distance (m) | 1,180 | 450 |
| Landing distance (m) | 800 | 260 |
| Weights | ||
| Max take off weight (kg) | 5,952 | 6,724 |
| Max payload (kg) | 472 | 440 |
| Baggage volume (m³) | 0.03 | - |
| Dimensions | ||
| Seats | 2 | 3 |