Comparison of Diamond DA-40 and Pilatus PC-6 Turbo Porter [S]ave
| Attribute |  Diamond DA-40 × |  Pilatus PC-6 Turbo Porter × |
|---|---|---|
| General | ||
| Manufacturer | Diamond Aircraft | Pilatus Aircraft |
| Model | Diamond DA-40 | Pilatus PC-6 Turbo Porter |
| Country | Austria | Switzerland |
| Manufactured from (year) | 2006 | 1961 |
| Type | Private Single Engine | Private Single Engine |
| Performance | ||
| Engine | 1 X Lycoming IO-360-M1A - | 1× Pratt & Whitney PT6A-27 |
| Power, hp (hp) | 180 | 550 |
| Avionics | Garmin G1000 | Honeywell Avionics Suite |
| Max cruise speed (km/h) | 181 | 154 |
| Fuel economy (km/l) | 18.053 | 1.429 |
| Take off distance (m) | 358 | 59 |
| Landing distance (m) | 352 | 40 |
| Weights | ||
| Max take off weight (kg) | 5,831 | 6,107 |
| Max payload (kg) | 390 | 694 |
| Baggage volume (m³) | - | 0.03 |
| Dimensions | ||
| Seats | 3 | 1 |
| Wing tips | No Winglets | - |
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