Airbus Helicopters H125 vs Bell 407gxi vs Leonardo Aw119kx vs Leonardo Sh09
The Airbus Helicopters H125 and Bell 407GXi sit in the same general category: light single‑engine utility helicopters commonly used for tourism, EMS support roles, police, and general lift. Both typically carry a pilot plus around five to six passengers depending on interior and mission fit, and both offer broadly comparable operational range in the “few hundred nautical miles” class, with actual endurance varying significantly with payload, altitude, and fuel configuration. The H125 is often favored where hot‑and‑high performance and external‑load utility work are priorities, while the 407GXi is frequently positioned as a fast, smooth, modernized evolution of the 407 line for multi‑mission use. The Leonardo SH09 is also a light single‑engine helicopter, but it is a newer program still progressing toward broad commercial availability, so final certified specifications and typical cabin layouts can vary by configuration and certification status. Conceptually it targets a similar passenger class to the H125/407GXi (pilot plus roughly six passengers) and a comparable light‑single mission range, aiming to compete in the same utility and passenger-transport niche.
| Spec | AIRBUS H125 | Bell 407GXi | AGUSTA / LEONARDO SH09 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 4.43 | $4.48 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 |
| Flight Rules | VFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Bell | Leonardo |
| Aircraft Name | H125 | 407GXi | SH09 |
| Certification | FAA / EASA | FAA / EASA | In-Development |
| Max Range (nm) | 341 | 337 | 430 |
| DOC / nm / Seat | $ 0.77 | $ 0.74 | $0.56 |
| 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 | $627 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G1000H NXI | EFIS |
| Max Cruise Speed (ktas) | 136 | 133 | 140 |
| Base Aircraft Price (USD) | $3,200,000 | $3,225,000 | $3,500,000 |
| Max Passengers | — | — | 7 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 |
| Max Cabin Seats | 5 | 5 | — |
| Standard Cabin Seats | 4 | 5 | 6 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Arriel 2D | M250-C47E/4 | HTS 900 |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 3500 | 5500 |
| Horsepower | 847 | 862 | 1020 |
| No. of Engines | 1 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 127.8 | — |
| Fuel Burn (gph) | — | 46 | — |
| Dimensions | |||
| Length (ft) | 42.5 | 41.4 | — |
| Overall Height (ft) | 10 | 10.2 | — |
| Rotor Diameter (ft) | 36.1 | 35 | — |
| Width (ft) | — | 25.4 | — |
| Cabin Width (ft) | — | 5 | — |
| Cabin Height (ft) | — | 3.9 | — |
| Cabin Volume (cu. ft) | — | 125 | — |
| Baggage Volume Ext. (cu. ft) | — | 16 | — |