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Pilatus PC-12
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| Engine make/model: | P&WC PT6A-67P | |
| Thermodynamic power (shp): | 1744 | |
| Flat-rated power (shp): | 1,200 | |
| Fuel type: | Jet A, Jet A1, Jet B, JP4 | |
| TBO (hrs.): | 3500 | |
| Propeller: | four-blade Hartzell, full reversing | |
| Propeller speed (rpm): | 1,700 | |
| Max takeoff weight (lbs.): | 10,450 | |
| Wingspan (ft.): | 53.4 | |
| Overall length (ft.): | 47.3 | |
| Height (ft.): | 14.0 | |
| Wing area (ft.): | 277.8 | |
| Maximum seating capacity: | 2+9 | |
| Cabin width (in.): | 60 | |
| Cabin height (in.): | 58 | |
| Baggage capacity (lbs.): | 400 | |
| Useable fuel (gals): | 402 | |
| Payload, full std. fuel, with 200-pound pilot aboard (lbs.): | 1009 | |
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PERFORMANCE
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| Max cruise Speed (kts.): | 280 | |
| Max cruise IFR range: | 1560 | |
| Fuel burn at max cruise (gph): | 66 | |
| Max operating altitude (ft.): | 30,000 | |
| Max cabin differential (psi): | 5.75 | |
| Best rate of climb (fpm): | 1,920 | |
| Takeoff ground roll (ft.): | 1,650 | |
| Landing over a 50-foot obstacle (ft): | 1,830 | |
| Vso (kts.): | 67 | |
| Source: Pilatus |
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