Cessna 206 Turbo Stationair vs Cessna Citation M2 vs Daher Tbm 910
The Cessna Turbo Stationair is a single‑engine, high‑wing piston aircraft typically used for utility, short‑field work, and general personal or small‑business travel. It offers the shortest range of the three, generally on the order of roughly 700–900 nautical miles depending on load and reserves, and it commonly seats about 4–6 passengers in addition to the pilot (with configurations varying by model and interior). The Daher TBM 910 is a single‑engine turboprop positioned as a high‑performance personal and business aircraft. It typically delivers substantially more range than the Stationair, often around 1,400–1,700 nautical miles, and usually carries about 4–6 passengers plus a pilot with a more executive‑style cabin. The Cessna Citation M2 is a light twin‑engine business jet aimed at faster point‑to‑point travel with jet comfort and higher cruise speeds. Its range is generally comparable to, or somewhat below, the TBM 910 in many real‑world missions (often around 1,200–1,500 nautical miles), and typical seating is about 4–6 passengers plus one or two pilots.
| Spec | Cessna Turbo Stationair | Cessna Citation M2 | Daher TBM 910 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 1.08 | $ 3.45 | $ 2.25 |
| Total Seats | 6 | 8 | 6 |
| Flight Rules | VFR | — | IFR |
| Manufacturer | Cessna | Cessna Citation | Daher TBM |
| Aircraft Name | 206 Turbo Stationair | M2 | TBM 910 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 703 | 1400 | 1730 |
| DOC / nm / Seat | $ 0.18 | $ 0.58 | $ 0.56 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Standard Cabin Seats | 4 | 6 | 4 |
| Direct Operating Cost | $ 174 | $ 1,395 | $ 744 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G3000 | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 161 | 404 | 330 |
| Base Aircraft Price (USD) | $745,000 | $5,150,000 | $4,250,000 |
| Min Crew | — | 1 | 1 |
| Max Cabin Seats | — | 7 | — |
| Useful Load (lbs) | — | 3810 | 2908 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Total Seats | 6 | 8 | 6 |
| Standard Cabin Seats | 4 | 6 | 4 |
| Lavatory | — | 1 Enclosed Belted Flushing | No |
| Min Crew | — | 1 | 1 |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Max Cabin Seats | — | 7 | — |
| Lavatory Location | — | AFT | — |
| Cabin Pressure (psi) | — | 8.5 | 6.2 |
| Galley / Refreshment | — | No | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 22027 | 14390 |
| Galley Location | — | — | MID |
| Engine | |||
| FADEC | No | Yes | Yes |
| Model | TIO-540-AJ1A | FJ44-1AP-21 | PT6A-66D |
| Fuel Type | AvGas | — | — |
| TBO (hrs) | 2000 | 3500 | 3500 |
| TBO (yrs) | 12 | — | — |
| Horsepower | 350 | — | 850 |
| Fuel Delivery | Fuel Injected | — | — |
| No. of Engines | 1 | 2 | 1 |
| Fuel Capacity (gal) | 87 | 492 | 291 |
| Flat Rating | — | ISA + 7 | ISA + 49 |
| Thrust (lbs) | — | 1965 | — |
| Fuel Burn (lbph) | — | 516 | — |
| Fuel Burn (gph) | — | — | 37 |
| Dimensions | |||
| Length (ft) | 28.3 | 42.6 | 35.3 |
| Wingspan (ft) | 36 | 47.3 | 42.1 |
| Cabin Width (ft) | 3.6 | 4.8 | 4 |
| Cabin Height (ft) | 4.2 | 4.8 | 4.1 |
| Cabin Length (ft) | 12.1 | 11 | 13.4 |
| Overall Height (ft) | 9.4 | 14 | 14.3 |
| Baggage Volume Int. (cu. ft) | 11 | — | 30 |
| Aisle Step (ft) | — | 0.4 | — |
| Cabin Width - Floor (ft) | — | 3.1 | — |
| Cabin Length - Seating (ft) | — | 8.8 | — |
| Baggage Volume Ext. (cu. ft) | — | 46 | — |
| Cabin Volume (cu. ft) | — | — | 123 |