Airbus Helicopters H125 vs Leonardo Aw139"
The Airbus H125 and the Leonardo AW139 sit in different helicopter classes, so their category, range, and passenger capacity reflect different missions. The H125 is a single‑engine light utility helicopter, widely used for aerial work, patrol, and operations in high‑and‑hot environments where simplicity and operating cost matter. It typically carries a pilot plus about five to six passengers depending on configuration and weights, and its practical range is generally in the mid‑hundreds of nautical miles, varying with fuel, payload, and reserves. The AW139 is a twin‑engine intermediate/medium helicopter designed for higher speed, greater payload, and enhanced redundancy, making it common in offshore transport, SAR, and executive/VIP roles. It typically carries one or two pilots plus around 12 to 15 passengers in a standard cabin layout, and its range is generally longer than the H125, often reaching the upper‑hundreds of nautical miles with standard tanks and extending further with optional auxiliary fuel. In short, the H125 prioritizes light, cost‑effective utility and performance in demanding conditions, while the AW139 prioritizes capacity, redundancy, and longer‑range, higher‑tempo transport.
| Spec | AIRBUS H125 |
|---|---|
| Summary | |
| Cockpit | 2 |
| DOC / nm | $ 4.61 |
| Min Crew | 1 |
| Total Seats | 6 |
| Flight Rules | VFR |
| Manufacturer | Airbus Helicopters |
| Aircraft Name | H125 |
| Certification | FAA / EASA |
| Max Range (nm) | 341 |
| DOC / nm / Seat | $ 0.77 |
| Max Cabin Seats | 5 |
| OEM Verification | VERIFIED |
| Useful Load (lbs) | 2189 |
| Standard Cabin Seats | 4 |
| Direct Operating Cost | $ 627 |
| Flight Deck (Base Spec) | Garmin G500H |
| Max Cruise Speed (ktas) | 136 |
| Base Aircraft Price (USD) | $3,200,000 |
| Cabin | |
| Cockpit | 2 |
| Min Crew | 1 |
| Total Seats | 6 |
| Max Cabin Seats | 5 |
| Standard Cabin Seats | 4 |
| Engine | |
| FADEC | Yes |
| Model | Arriel 2D |
| Fuel Type | JetFuel |
| TBO (hrs) | 5000 |
| Horsepower | 847 |
| No. of Engines | 1 |
| Fuel Capacity (gal) | 143 |
| Dimensions | |
| Length (ft) | 42.5 |
| Overall Height (ft) | 10 |
| Rotor Diameter (ft) | 36.1 |