Cessna 206 Turbo Stationair vs Daher Tbm 910
The Cessna Turbo Stationair and the Daher TBM 910 sit in different turboprop categories and are aimed at different missions. The Turbo Stationair is a single‑engine, high‑wing utility turboprop typically positioned as a rugged, backcountry‑friendly personal and light commercial aircraft, often used for short to medium trips with an emphasis on load flexibility and unimproved‑strip capability. The TBM 910 is a high‑performance, single‑engine turboprop in the “fast personal transport” class, optimized for speed, altitude, and efficient point‑to‑point travel. On range, the Turbo Stationair generally offers solid midrange capability suited to regional flying, while the TBM 910 is designed for longer legs and typically provides substantially greater range, enabling more nonstop trips between major city pairs. For passenger capacity, the Turbo Stationair is commonly configured with more seats and a more utility‑oriented cabin, often accommodating up to about six to eight occupants depending on configuration and payload. The TBM 910 is usually arranged for around four to six occupants, prioritizing comfort and performance over maximum seating.
| Spec | Cessna Turbo Stationair | Daher TBM 910 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 1.08 | $ 2.25 |
| Total Seats | 6 | 6 |
| Flight Rules | VFR | IFR |
| Manufacturer | Cessna | Daher TBM |
| Aircraft Name | 206 Turbo Stationair | TBM 910 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 703 | 1730 |
| DOC / nm / Seat | $ 0.18 | $ 0.56 |
| OEM Verification | Un-Verified | Un-Verified |
| Standard Cabin Seats | 4 | 4 |
| Direct Operating Cost | $ 174 | $ 744 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 161 | 330 |
| Base Aircraft Price (USD) | $745,000 | $4,250,000 |
| Min Crew | — | 1 |
| Useful Load (lbs) | — | 2908 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Total Seats | 6 | 6 |
| Standard Cabin Seats | 4 | 4 |
| Lavatory | — | No |
| Min Crew | — | 1 |
| Galley Location | — | MID |
| Cabin Pressure (psi) | — | 6.2 |
| Galley / Refreshment | — | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 14390 |
| Engine | ||
| FADEC | No | Yes |
| Model | TIO-540-AJ1A | PT6A-66D |
| Fuel Type | AvGas | — |
| TBO (hrs) | 2000 | 3500 |
| TBO (yrs) | 12 | — |
| Horsepower | 350 | 850 |
| Fuel Delivery | Fuel Injected | — |
| No. of Engines | 1 | 1 |
| Fuel Capacity (gal) | 87 | 291 |
| Flat Rating | — | ISA + 49 |
| Fuel Burn (gph) | — | 37 |
| Dimensions | ||
| Length (ft) | 28.3 | 35.3 |
| Wingspan (ft) | 36 | 42.1 |
| Cabin Width (ft) | 3.6 | 4 |
| Cabin Height (ft) | 4.2 | 4.1 |
| Cabin Length (ft) | 12.1 | 13.4 |
| Overall Height (ft) | 9.4 | 14.3 |
| Baggage Volume Int. (cu. ft) | 11 | 30 |
| Cabin Volume (cu. ft) | — | 123 |