Airbus Helicopters H125 vs Leonardo Aw139
The Airbus Helicopters H125 and the Leonardo AW139 sit in different categories and are typically chosen for different missions. The H125 is a light single‑engine helicopter, valued for utility work, high‑and‑hot performance, and lower operating complexity. The AW139 is a medium twin‑engine helicopter, designed for higher payload, redundancy, and demanding passenger, offshore, and EMS-style operations. In range, the H125 generally offers a shorter mission radius than the AW139, reflecting its lighter class and single‑engine design, though actual endurance varies with payload, altitude, and fuel configuration. The AW139 typically provides longer range and better high‑speed cruise capability, making it more suitable for longer overwater legs and regional transport missions. For passenger capacity, the H125 commonly carries a pilot plus about five to six passengers in typical configurations, while the AW139 is built to move larger groups, often seating around twelve to fifteen passengers depending on interior layout and mission equipment. Overall, the H125 fits lighter, cost‑sensitive utility roles, while the AW139 fits higher-capacity, longer-range transport needs.
| Spec | AIRBUS H125 | AGUSTA / LEONARDO AW139 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 4.61 | $ 11.69 |
| Min Crew | 1 | 2 |
| Total Seats | 6 | 17 |
| Flight Rules | VFR | IFR |
| Manufacturer | Airbus Helicopters | Leonardo |
| Aircraft Name | H125 | AW139 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 573 |
| DOC / nm / Seat | $ 0.77 | $ 0.69 |
| Max Cabin Seats | 5 | 15 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2189 | 4701 |
| Standard Cabin Seats | 4 | 15 |
| Direct Operating Cost | $ 627 | $ 1,929 |
| Flight Deck (Base Spec) | Garmin G500H | EFIS |
| Max Cruise Speed (ktas) | 136 | 165 |
| Base Aircraft Price (USD) | $3,200,000 | $15,900,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 2 |
| Total Seats | 6 | 17 |
| Max Cabin Seats | 5 | 15 |
| Standard Cabin Seats | 4 | 15 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Arriel 2D | PT6C-67C |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 5000 |
| Horsepower | 847 | 1679 |
| No. of Engines | 1 | 2 |
| Fuel Capacity (gal) | 143 | 414 |
| Dimensions | ||
| Length (ft) | 42.5 | 54.7 |
| Overall Height (ft) | 10 | 16.4 |
| Rotor Diameter (ft) | 36.1 | 54.7 |
| Cabin Volume (cu. ft) | — | 282 |
| Baggage Volume Ext. (cu. ft) | — | 120 |