Airbus Helicopters H125 vs Leonardo Aw139
The Airbus Helicopters H125 and the Leonardo AW139 sit in different market categories and are optimized for different missions. The H125 is a light single‑engine helicopter commonly used for utility work, training, aerial observation, and operations in hot‑and‑high environments; it is typically configured for about 5 to 6 passengers plus a pilot, depending on interior and mission equipment. The AW139 is a medium twin‑engine helicopter aimed at offshore transport, EMS, search and rescue, and corporate/VIP shuttle; it generally carries around 12 to 15 passengers, again depending on seating layout and role. In range, the AW139 typically offers a longer and more flexible mission radius than the H125, especially when configured for transport with appropriate fuel reserves, reflecting its larger airframe and twin‑engine design. The H125’s range is usually shorter but still well suited to local and regional missions, with an emphasis on simplicity, lower operating complexity, and strong performance in demanding conditions.
| 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 |