Airbus Helicopters H125 vs Bell 407gxi vs Leonardo Aw119kx
The Airbus Helicopters H125, Bell 407GXi, and Leonardo AW119Kx all sit in the light single‑engine utility category, commonly used for passenger transport, tourism, aerial work, and public‑service roles, but they emphasize different strengths. In passenger capacity, all are typically configured around a pilot plus up to six passengers in standard layouts, though exact seating depends on interior options and mission equipment. For range, they are broadly comparable in typical operations, with the Bell 407GXi and AW119Kx generally offering strong cross‑country capability for the class, while the H125 is often selected as much for its utility performance as for outright distance. Overall, if you want a widely proven workhorse with a strong utility reputation, the H125 is often the reference point; the 407GXi is frequently positioned as a fast, efficient light single for passenger missions; and the AW119Kx is notable for combining single‑engine simplicity with a spacious cabin feel and solid touring range in many configurations.
| Spec | AIRBUS H125 | Bell 407GXi | AGUSTA / LEONARDO AW119Kx |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 4.43 | $ 6.76 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 |
| Flight Rules | VFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Bell | Leonardo |
| Aircraft Name | H125 | 407GXi | AW119Kx |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 337 | 515 |
| DOC / nm / Seat | $ 0.77 | $ 0.74 | $ 0.84 |
| Max Cabin Seats | 5 | 5 | 6 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2189 | 2300 | — |
| Standard Cabin Seats | 4 | 5 | 6 |
| Direct Operating Cost | $ 627 | $ 589 | $ 885 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G1000H NXI | Garmin G1000H |
| Max Cruise Speed (ktas) | 136 | 133 | 131 |
| Base Aircraft Price (USD) | $3,200,000 | $3,225,000 | $3,850,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 |
| Max Cabin Seats | 5 | 5 | 6 |
| Standard Cabin Seats | 4 | 5 | 6 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Arriel 2D | M250-C47E/4 | PT6B-37A |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 3500 | 4500 |
| Horsepower | 847 | 862 | 917 |
| No. of Engines | 1 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 127.8 | 160 |
| Fuel Burn (gph) | — | 46 | — |
| Dimensions | |||
| Length (ft) | 42.5 | 41.4 | 42.5 |
| Overall Height (ft) | 10 | 10.2 | 11.9 |
| Rotor Diameter (ft) | 36.1 | 35 | 35.5 |
| Width (ft) | — | 25.4 | — |
| Cabin Width (ft) | — | 5 | — |
| Cabin Height (ft) | — | 3.9 | — |
| Cabin Volume (cu. ft) | — | 125 | — |
| Baggage Volume Ext. (cu. ft) | — | 16 | — |