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Lancair Evolution
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| SPECIFICATIONS | ||
| Price as flown: | Approx. $1.4 million | |
| Engine: | Pratt & Whitney PT6A-135A | |
| Max horsepower (shp): | 750 | |
| Max torque (lbs. ft.): | 2080 | |
| Propeller: | Hartzell 82.5-inch four-blade w/ deice | |
| Length (ft.): | 30 | |
| Height (ft.): | 10 | |
| Wingspan (ft.): | 37 | |
| Seating: | 4 | |
| Cargo volume (cu. ft.): | 39 | |
| Baggage capacity (lbs.): | 225 | |
| Fuel capacity (gals.): | 168 | |
| Full fuel payload (lbs.): | 800 | |
| Design empty weight (lbs.): | 2650 | |
| Max takeoff weight (lbs.): | 4550 | |
| PERFORMANCE | ||
| Vne (KIAS): | 256 | |
| Va: | 190 | |
| Vno: | 76-220 | |
| Vfe: | 160 | |
| Vle: | 165 | |
| Vso: | 61 | |
| Vs: | 76 | |
| Min takeoff distance (ft.): | 1200 | |
| Min landing distance (ft.): | 1200 | |
| Rate of climb (fpm): | 4000 | |
| Cruise speed (max, KIAS): | 300 | |
| Range w/ reserve (nm): | 1100 | |
| Fuel flow (gph): | 37 | |
| Economy cruise (KTAS): | 270 | |
| Range (w/ reserve, nm): | 1300 | |
| Fuel flow (gph): | 25 gph | |
| Max op alt (RVSM limited, ft.): | 28,000 | |
