Cessna 206 Turbo Stationair vs Cessna Grand Caravan Ex vs Pilatus Pc 12 Ngx vs Piper M600 Sls
The Cessna Turbo Stationair (pressurized piston/turbocharged single) sits in the light-utility category, typically offering shorter regional range and a practical cabin for about four to six passengers depending on load and configuration. The Cessna Grand Caravan EX is a single‑engine turboprop utility aircraft optimized for hauling people or cargo; it generally carries the most occupants in this group, commonly up to nine passengers in commuter seating, with midrange legs that favor short-to-medium routes and rugged strips. The Pilatus PC‑12 NGX is a higher-performance single‑engine turboprop in the “executive utility” class, usually configured for six to nine passengers with more comfort and baggage flexibility, and it typically delivers the longest range of the turboprops here, making it well suited to longer point‑to‑point missions. The Piper M600 SLS is a smaller, pressurized personal turboprop focused on owner‑pilot travel; it usually seats five to six, prioritizing speed and efficient medium-to-long range over maximum passenger count.
| Spec | Cessna Turbo Stationair | Cessna Grand Caravan EX | Pilatus PC-12 NGX | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 1.08 | $ 3.15 | $ 2.78 | $ 2.19 |
| Total Seats | 6 | 10 | 8 | 6 |
| Flight Rules | VFR | VFR | IFR | IFR |
| Manufacturer | Cessna | Cessna | Pilatus | Piper |
| Aircraft Name | 206 Turbo Stationair | Grand Caravan EX | PC-12 NGX | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 703 | 964 | 1803 | 1406 |
| DOC / nm / Seat | $ 0.18 | $ 0.39 | $ 0.46 | $ 0.55 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Standard Cabin Seats | 4 | 8 | 6 | 4 |
| Direct Operating Cost | $ 174 | $ 614 | $ 793 | $ 603 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Honeywell Primus Apex | Garmin G3000 |
| Max Cruise Speed (ktas) | 161 | 195 | 290 | 274 |
| Base Aircraft Price (USD) | $745,000 | $2,695,000 | $5,350,000 | $3,081,400 |
| Min Crew | — | 1 | 1 | 1 |
| Max Cabin Seats | — | 12 | 9 | — |
| Useful Load (lbs) | — | 3332 | — | 2200 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Total Seats | 6 | 10 | 8 | 5 |
| Standard Cabin Seats | 4 | 8 | 6 | 4 |
| Lavatory | — | No | Optional | No |
| Min Crew | — | 1 | 1 | 1 |
| Cargo Door | — | Yes | Yes | — |
| Max Cabin Seats | — | 12 | 9 | — |
| Cabin Pressure (psi) | — | Un-Pressurized | 5.8 | 5.6 |
| Galley / Refreshment | — | No | No | Refreshment Centre |
| Lavatory Location | — | — | FWD | — |
| SL Cabin Altitude (ft) | — | — | 13100 | 12600 |
| Galley Location | — | — | — | MID |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | No | Yes | Yes | No |
| Model | TIO-540-AJ1A | PT6A-140 | PT6E-67XP | PT6A-42A |
| Fuel Type | AvGas | — | — | — |
| TBO (hrs) | 2000 | 4000 | 5000 | 3600 |
| TBO (yrs) | 12 | — | — | — |
| Horsepower | 350 | 867 | 1200 | 600 |
| Fuel Delivery | Fuel Injected | — | — | — |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 87 | 335 | — | 260 |
| Flat Rating | — | ISA + 24 | ISA + 35 | ISA + 55 |
| Usable Fuel (gal) | — | — | 402 | — |
| Dimensions | ||||
| Length (ft) | 28.3 | 41.6 | 47.25 | 29.7 |
| Wingspan (ft) | 36 | 52.1 | 53.33 | 43.2 |
| Cabin Width (ft) | 3.6 | 5.4 | 5 | 4.1 |
| Cabin Height (ft) | 4.2 | 4.5 | 4.9 | 4 |
| Cabin Length (ft) | 12.1 | 16.8 | 16.9 | 12.3 |
| Overall Height (ft) | 9.4 | 15.1 | 14 | 11.3 |
| Baggage Volume Int. (cu. ft) | 11 | 32 | 40 | 20 |
| Cabin Width - Floor (ft) | — | — | 4.25 | — |
| Cabin Volume (cu. ft) | — | — | — | 165 |