Cessna 206 Turbo Stationair vs Cessna Citation M2 vs Daher Tbm 910 vs Honda Aircraft Hondajet Elite
The Cessna Turbo Stationair is a pressurized single‑engine piston utility aircraft, typically used for short regional missions and backcountry-capable travel. It carries about 5–6 passengers (plus a pilot) and offers the shortest range of this group, generally in the roughly 700–1,000 nautical mile class depending on configuration and reserves. The Daher TBM 910 is a high‑performance single‑engine turboprop that bridges owner‑flown practicality and near–light‑jet cruise speeds. It usually seats 4–6 passengers (plus a pilot) and has the longest range here, commonly around 1,500+ nautical miles. The Cessna Citation M2 is an entry‑level light jet aimed at fast point‑to‑point business travel. It typically accommodates 4–5 passengers (plus one or two pilots) and delivers midpack range, roughly around 1,200–1,500 nautical miles. The Honda Aircraft HondaJet Elite is a very light jet emphasizing efficiency and cabin innovation. It generally seats 4–5 passengers (plus one or two pilots) and offers a similar range class to the M2, often about 1,200–1,400 nautical miles.
| Spec | Cessna Turbo Stationair | Cessna Citation M2 | Daher TBM 910 | Honda Aircraft HondaJet Elite |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 1.08 | $ 3.45 | $ 2.25 | $ 2.73 |
| Total Seats | 6 | 8 | 6 | 6 |
| Flight Rules | VFR | — | IFR | — |
| Manufacturer | Cessna | Cessna Citation | Daher TBM | Honda Aircraft |
| Aircraft Name | 206 Turbo Stationair | M2 | TBM 910 | HondaJet Elite |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 703 | 1400 | 1730 | 1495 |
| DOC / nm / Seat | $ 0.18 | $ 0.58 | $ 0.56 | $ 0.68 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Standard Cabin Seats | 4 | 6 | 4 | 4 |
| Direct Operating Cost | $ 174 | $ 1,395 | $ 744 | $ 1,135 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G3000 | Garmin G1000 NXi | Garmin G3000 |
| Max Cruise Speed (ktas) | 161 | 404 | 330 | 419 |
| Base Aircraft Price (USD) | $745,000 | $5,150,000 | $4,250,000 | $ 5,400,000 |
| Min Crew | — | 1 | 1 | 1 |
| Max Cabin Seats | — | 7 | — | 6 |
| Useful Load (lbs) | — | 3810 | 2908 | 3432 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Total Seats | 6 | 8 | 6 | 6 |
| Standard Cabin Seats | 4 | 6 | 4 | 4 |
| Lavatory | — | 1 Enclosed Belted Flushing | No | 1 Enclosed Flushing |
| Min Crew | — | 1 | 1 | 1 |
| Crew Rest | — | No | — | No |
| Jump Seat | — | No | — | No |
| Max Cabin Seats | — | 7 | — | 6 |
| Lavatory Location | — | AFT | — | AFT |
| Cabin Pressure (psi) | — | 8.5 | 6.2 | 8.8 |
| Galley / Refreshment | — | No | Refreshment Centre | Galley |
| SL Cabin Altitude (ft) | — | 22027 | 14390 | 23060 |
| Galley Location | — | — | MID | FWD |
| Engine | ||||
| FADEC | No | Yes | Yes | Yes |
| Model | TIO-540-AJ1A | FJ44-1AP-21 | PT6A-66D | HF120-H1A |
| Fuel Type | AvGas | — | — | — |
| TBO (hrs) | 2000 | 3500 | 3500 | 5000 |
| TBO (yrs) | 12 | — | — | — |
| Horsepower | 350 | — | 850 | — |
| Fuel Delivery | Fuel Injected | — | — | — |
| No. of Engines | 1 | 2 | 1 | 2 |
| Fuel Capacity (gal) | 87 | 492 | 291 | 439 |
| Flat Rating | — | ISA + 7 | ISA + 49 | ISA + 10 |
| Thrust (lbs) | — | 1965 | — | 2050 |
| Fuel Burn (lbph) | — | 516 | — | — |
| Fuel Burn (gph) | — | — | 37 | — |
| Dimensions | ||||
| Length (ft) | 28.3 | 42.6 | 35.3 | 42.7 |
| Wingspan (ft) | 36 | 47.3 | 42.1 | 39.8 |
| Cabin Width (ft) | 3.6 | 4.8 | 4 | 5 |
| Cabin Height (ft) | 4.2 | 4.8 | 4.1 | 4.8 |
| Cabin Length (ft) | 12.1 | 11 | 13.4 | 12.1 |
| Overall Height (ft) | 9.4 | 14 | 14.3 | 14.9 |
| Baggage Volume Int. (cu. ft) | 11 | — | 30 | — |
| Aisle Step (ft) | — | 0.4 | — | 0.4 |
| Cabin Width - Floor (ft) | — | 3.1 | — | — |
| Cabin Length - Seating (ft) | — | 8.8 | — | 10.2 |
| Baggage Volume Ext. (cu. ft) | — | 46 | — | 66 |
| Cabin Volume (cu. ft) | — | — | 123 | — |