Airbus Helicopters H125 vs Bell 407gxi vs Leonardo Aw109 Grand New vs Leonardo Aw119kx vs Leonardo Sh09
In category, the Airbus Helicopters H125 and Leonardo AW119Kx are single‑engine light helicopters typically used for utility, tourism, and high/hot operations, while the Bell 407GXi is also a single‑engine light helicopter but often positioned as a higher‑speed, smooth‑riding platform for corporate and public‑service roles. The Leonardo AW109 GrandNew is a twin‑engine light/intermediate helicopter aimed at executive transport and mission flexibility with higher redundancy and generally higher cruise performance. The Leonardo SH09 sits in the modern light single‑engine class, targeting multi‑role utility and passenger transport with contemporary avionics and efficiency. On range, these aircraft broadly overlap, with the single‑engine light models (H125, 407GXi, AW119Kx, SH09) typically offering mid‑hundreds of nautical miles depending on configuration, reserves, and payload, while the twin‑engine AW109 GrandNew generally provides comparable or better mission radius at higher cruise speeds, again strongly dependent on tanks and cabin fit. For passenger capacity, the H125 and 407GXi commonly seat a pilot plus about five to six passengers, the AW119Kx and SH09 are similar in typical layouts, and the AW109 GrandNew usually accommodates a pilot (or two) plus around six to seven passengers in executive or utility configurations.
| Spec | AIRBUS H125 | Bell 407GXi | AGUSTA / LEONARDO AW109 Grand New | AGUSTA / LEONARDO AW119Kx | AGUSTA / LEONARDO SH09 |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 4.43 | $ 7.31 | $ 6.76 | $4.48 |
| Min Crew | 1 | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 | 8 | 8 |
| Flight Rules | VFR | VFR | VFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Bell | Leonardo | Leonardo | Leonardo |
| Aircraft Name | H125 | 407GXi | AW109 Grand New | AW119Kx | SH09 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | In-Development |
| Max Range (nm) | 341 | 337 | 464 | 515 | 430 |
| DOC / nm / Seat | $ 0.77 | $ 0.74 | $ 0.91 | $ 0.84 | $0.56 |
| Max Cabin Seats | 5 | 5 | 6 | 6 | 6 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | 2300 | — | — | — |
| Standard Cabin Seats | 4 | 5 | 6 | 6 | 6 |
| Direct Operating Cost | $ 627 | $ 589 | $ 1,140 | $ 885 | $627 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G1000H NXI | EFIS | Garmin G1000H | EFIS |
| Max Cruise Speed (ktas) | 136 | 133 | 156 | 131 | 140 |
| Base Aircraft Price (USD) | $3,200,000 | $3,225,000 | $ 7,800,000 | $3,850,000 | $3,500,000 |
| Max Passengers | — | — | — | — | 7 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 | 8 | 8 |
| Max Cabin Seats | 5 | 5 | 6 | 6 | — |
| Standard Cabin Seats | 4 | 5 | 6 | 6 | 6 |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | Yes |
| Model | Arriel 2D | M250-C47E/4 | PW207C | PT6B-37A | HTS 900 |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 3500 | 4000 | 4500 | 5500 |
| Horsepower | 847 | 862 | 735 | 917 | 1020 |
| No. of Engines | 1 | 1 | 2 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 127.8 | 152 | 160 | — |
| Fuel Burn (gph) | — | 46 | — | — | — |
| Dimensions | |||||
| Length (ft) | 42.5 | 41.4 | 42.5 | 42.5 | — |
| Overall Height (ft) | 10 | 10.2 | 11.5 | 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 | — | — | — |