Cessna 206 Turbo Stationair vs Pilatus Pc 12 Ngx
The Cessna Turbo Stationair is a single‑engine piston aircraft often categorized as a high‑performance utility/light personal transport, while the Pilatus PC‑12 NGX is a single‑engine turboprop designed for executive, charter, and rugged utility operations. In range, the Turbo Stationair generally suits regional trips and shorter cross‑countries, with typical real‑world legs commonly in the mid‑hundreds of nautical miles depending on load, power settings, and reserves, whereas the PC‑12 NGX is built for substantially longer missions, commonly over 1,500 nautical miles with appropriate configuration and fuel planning. Passenger capacity also differs: the Turbo Stationair is typically arranged for about six seats including the pilot, making it practical for families or small teams with moderate baggage, while the PC‑12 NGX is usually configured for one pilot plus six to nine passengers, offering a larger cabin, more payload flexibility, and a more “aircraft-as-a-platform” capability for mixed passengers, baggage, or special mission interiors.
| Spec | Cessna Turbo Stationair | Pilatus PC-12 NGX |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 1.08 | $ 2.78 |
| Total Seats | 6 | 8 |
| Flight Rules | VFR | IFR |
| Manufacturer | Cessna | Pilatus |
| Aircraft Name | 206 Turbo Stationair | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 703 | 1803 |
| DOC / nm / Seat | $ 0.18 | $ 0.46 |
| OEM Verification | Un-Verified | VERIFIED |
| Standard Cabin Seats | 4 | 6 |
| Direct Operating Cost | $ 174 | $ 793 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 161 | 290 |
| Base Aircraft Price (USD) | $745,000 | $5,350,000 |
| Min Crew | — | 1 |
| Max Cabin Seats | — | 9 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Total Seats | 6 | 8 |
| Standard Cabin Seats | 4 | 6 |
| Lavatory | — | Optional |
| Min Crew | — | 1 |
| Cargo Door | — | Yes |
| Max Cabin Seats | — | 9 |
| Lavatory Location | — | FWD |
| Cabin Pressure (psi) | — | 5.8 |
| Galley / Refreshment | — | No |
| SL Cabin Altitude (ft) | — | 13100 |
| Engine | ||
| FADEC | No | Yes |
| Model | TIO-540-AJ1A | PT6E-67XP |
| Fuel Type | AvGas | — |
| TBO (hrs) | 2000 | 5000 |
| TBO (yrs) | 12 | — |
| Horsepower | 350 | 1200 |
| Fuel Delivery | Fuel Injected | — |
| No. of Engines | 1 | 1 |
| Fuel Capacity (gal) | 87 | — |
| Flat Rating | — | ISA + 35 |
| Usable Fuel (gal) | — | 402 |
| Dimensions | ||
| Length (ft) | 28.3 | 47.25 |
| Wingspan (ft) | 36 | 53.33 |
| Cabin Width (ft) | 3.6 | 5 |
| Cabin Height (ft) | 4.2 | 4.9 |
| Cabin Length (ft) | 12.1 | 16.9 |
| Overall Height (ft) | 9.4 | 14 |
| Baggage Volume Int. (cu. ft) | 11 | 40 |
| Cabin Width - Floor (ft) | — | 4.25 |