Airbus Helicopters H125 vs Bell 407gxi vs Leonardo Aw119kx vs Leonardo Aw119kx
All three are single‑engine light utility helicopters in the same broad category, commonly used for passenger transport, tourism, EMS support, and utility work. The Airbus Helicopters H125 (AS350) is typically positioned as the most “workhorse” utility option, known for strong hot‑and‑high performance and a roomy cabin for its class. The Bell 407GXi is a light single that emphasizes speed, smooth handling, and efficient operations, often favored for corporate and public‑service missions. The Leonardo AW119Kx is also a light single, notable for a relatively spacious cabin and IFR‑capable variants, making it attractive where mission flexibility is important. In passenger capacity, all are broadly similar: typical configurations are around 5–6 passengers plus a pilot, though exact seating depends on interior layout, mission equipment, and weight limits. In range, they are also in the same general band, with typical mission ranges roughly in the 300–400 nautical mile class depending heavily on fuel fit, payload, reserves, and operating conditions; the Bell 407GXi and AW119Kx are often quoted toward the higher end of that band, while the H125 varies widely with configuration and mission profile.
| Spec | AIRBUS H125 | Bell 407GXi | AGUSTA / LEONARDO AW119Kx | AGUSTA / LEONARDO AW119Kx |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 4.43 | $ 6.76 | $ 6.76 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 | 8 |
| Flight Rules | VFR | VFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Bell | Leonardo | Leonardo |
| Aircraft Name | H125 | 407GXi | AW119Kx | AW119Kx |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 337 | 515 | 515 |
| DOC / nm / Seat | $ 0.77 | $ 0.74 | $ 0.84 | $ 0.84 |
| Max Cabin Seats | 5 | 5 | 6 | 6 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | 2300 | — | — |
| Standard Cabin Seats | 4 | 5 | 6 | 6 |
| Direct Operating Cost | $ 627 | $ 589 | $ 885 | $ 885 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G1000H NXI | Garmin G1000H | Garmin G1000H |
| Max Cruise Speed (ktas) | 136 | 133 | 131 | 131 |
| Base Aircraft Price (USD) | $3,200,000 | $3,225,000 | $3,850,000 | $3,850,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 | 8 |
| Max Cabin Seats | 5 | 5 | 6 | 6 |
| Standard Cabin Seats | 4 | 5 | 6 | 6 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Arriel 2D | M250-C47E/4 | PT6B-37A | PT6B-37A |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 3500 | 4500 | 4500 |
| Horsepower | 847 | 862 | 917 | 917 |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 127.8 | 160 | 160 |
| Fuel Burn (gph) | — | 46 | — | — |
| Dimensions | ||||
| Length (ft) | 42.5 | 41.4 | 42.5 | 42.5 |
| Overall Height (ft) | 10 | 10.2 | 11.9 | 11.9 |
| Rotor Diameter (ft) | 36.1 | 35 | 35.5 | 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 | — | — |