Bell 407gxi vs Cessna 206 Turbo Stationair
The Bell 407GXi is a single‑engine turbine helicopter, while the Cessna Turbo Stationair (commonly the 206H Turbo) is a single‑engine turbocharged piston fixed‑wing airplane. In category terms, the Bell excels where vertical lift and hover matter—point‑to‑point access to confined sites, rooftop pads, unimproved clearings, and low‑speed observation—whereas the Stationair is oriented to runway‑based travel with efficient cruise and straightforward cross‑country utility. For range, the Turbo Stationair generally offers the longer legs in typical operations, often around 600–800 nautical miles depending on load, reserves, and conditions. The Bell 407GXi’s practical range is usually shorter, commonly on the order of roughly 300–400 nautical miles, varying with fuel configuration and mission profile. Passenger capacity is broadly similar but used differently. The Bell 407GXi typically carries one pilot plus up to five passengers (six total seats) with flexible cabin access. The Turbo Stationair commonly seats one pilot plus up to five passengers (six total), and can also be configured to emphasize cargo and utility loading.
| Spec | Bell 407GXi | Cessna Turbo Stationair |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 4.43 | $ 1.08 |
| Min Crew | 1 | — |
| Total Seats | 6 | 6 |
| Flight Rules | VFR | VFR |
| Manufacturer | Bell | Cessna |
| Aircraft Name | 407GXi | 206 Turbo Stationair |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 337 | 703 |
| DOC / nm / Seat | $ 0.74 | $ 0.18 |
| Max Cabin Seats | 5 | — |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2300 | — |
| Standard Cabin Seats | 5 | 4 |
| Direct Operating Cost | $ 589 | $ 174 |
| Flight Deck (Base Spec) | Garmin G1000H NXI | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 133 | 161 |
| Base Aircraft Price (USD) | $3,225,000 | $745,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | — |
| Total Seats | 6 | 6 |
| Max Cabin Seats | 5 | — |
| Standard Cabin Seats | 5 | 4 |
| Engine | ||
| FADEC | Yes | No |
| Model | M250-C47E/4 | TIO-540-AJ1A |
| Fuel Type | JetFuel | AvGas |
| TBO (hrs) | 3500 | 2000 |
| Horsepower | 862 | 350 |
| No. of Engines | 1 | 1 |
| Fuel Burn (gph) | 46 | — |
| Fuel Capacity (gal) | 127.8 | 87 |
| TBO (yrs) | — | 12 |
| Fuel Delivery | — | Fuel Injected |
| Dimensions | ||
| Width (ft) | 25.4 | — |
| Length (ft) | 41.4 | 28.3 |
| Cabin Width (ft) | 5 | 3.6 |
| Cabin Height (ft) | 3.9 | 4.2 |
| Overall Height (ft) | 10.2 | 9.4 |
| Rotor Diameter (ft) | 35 | — |
| Cabin Volume (cu. ft) | 125 | — |
| Baggage Volume Ext. (cu. ft) | 16 | — |
| Wingspan (ft) | — | 36 |
| Cabin Length (ft) | — | 12.1 |
| Baggage Volume Int. (cu. ft) | — | 11 |