Airbus Helicopters H125 vs Cessna 182 Skylane vs Cessna 206 Turbo Stationair
The Airbus Helicopters H125 is a single‑engine light helicopter focused on vertical lift and access to confined or unimproved sites, while the Cessna Skylane (typically the 182) and the Cessna Turbo Stationair (typically the 206) are fixed‑wing, single‑engine utility airplanes optimized for point‑to‑point travel from runways and short strips. In range, the H125 is generally the shortest‑legged of the three, typically operating in the few‑hundred‑nautical‑mile class depending on tanking and payload, whereas the Skylane commonly reaches the high‑hundreds of nautical miles, and the Turbo Stationair is broadly similar or somewhat greater, especially at altitude where the turbocharged engine helps maintain cruise performance. For passenger capacity, the H125 is usually configured for a pilot plus up to about five passengers depending on layout and mission equipment. The Skylane is commonly a four‑seat airplane (sometimes with a small optional fifth seat), while the Turbo Stationair is usually a six‑seat utility platform and often carries the most people and cargo in typical configurations.
| Spec | AIRBUS H125 | Cessna Skylane | Cessna Turbo Stationair |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | — | 2 |
| DOC / nm | $ 4.61 | $ 1.01 | $ 1.08 |
| Min Crew | 1 | — | — |
| Total Seats | 6 | 4 | 6 |
| Flight Rules | VFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Cessna | Cessna |
| Aircraft Name | H125 | 182 Skylane | 206 Turbo Stationair |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 915 | 703 |
| DOC / nm / Seat | $ 0.77 | $ 0.25 | $ 0.18 |
| Max Cabin Seats | 5 | — | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | — | — |
| Standard Cabin Seats | 4 | — | 4 |
| Direct Operating Cost | $ 627 | $ 146 | $ 174 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 136 | 145 | 161 |
| Base Aircraft Price (USD) | $3,200,000 | $530,000 | $745,000 |
| Cabin | |||
| Cockpit | 2 | — | 2 |
| Min Crew | 1 | — | — |
| Total Seats | 6 | 4 | 6 |
| Max Cabin Seats | 5 | — | — |
| Standard Cabin Seats | 4 | — | 4 |
| Engine | |||
| FADEC | Yes | No | No |
| Model | Arriel 2D | IO-540-AB1A5 | TIO-540-AJ1A |
| Fuel Type | JetFuel | AvGas | AvGas |
| TBO (hrs) | 5000 | 2000 | 2000 |
| Horsepower | 847 | 245 | 350 |
| No. of Engines | 1 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 87 | 87 |
| TBO (yrs) | — | 12 | 12 |
| Fuel Delivery | — | Fuel Injected | Fuel Injected |
| Dimensions | |||
| Length (ft) | 42.5 | 29 | 28.3 |
| Overall Height (ft) | 10 | 9.4 | 9.4 |
| Rotor Diameter (ft) | 36.1 | — | — |
| Wingspan (ft) | — | 36 | 36 |
| Cabin Width (ft) | — | 3.5 | 3.6 |
| Cabin Height (ft) | — | 4.1 | 4.2 |
| Cabin Length (ft) | — | 11.2 | 12.1 |
| Baggage Volume Int. (cu. ft) | — | 32 | 11 |