Airbus Helicopters H125 vs Airbus Helicopters H130 vs Leonardo Aw119kx vs Leonardo Sh09
Airbus Helicopters’ H125 and H130 are both single‑engine light helicopters, but they emphasize different missions. The H125 is typically positioned as a high‑performance utility aircraft for lifting and work in hot‑and‑high conditions, with a practical range in the roughly 600 km class depending on fuel fit and reserves, and usually configured for about 5 to 6 passengers plus a pilot. The H130 is more passenger‑centric and quieter, aimed at tourism and private/VIP use, commonly offering 6 to 7 passengers plus a pilot and a similar mid‑hundreds‑of‑kilometers range. Leonardo’s AW119Kx is also a single‑engine light helicopter, often described as a strong all‑rounder with a larger cabin feel in its class. It typically seats around 6 passengers plus a pilot and offers range broadly comparable to the Airbus singles, again typically in the mid‑hundreds of kilometers depending on configuration. The Leonardo SH09 (still in development/early program status) targets the same light single‑engine segment, aiming for a modern, efficient platform with seating generally expected around 6 passengers plus a pilot and a comparable short‑to‑medium range profile. Actual SH09 figures depend on final certification and customer options.
| Spec | AIRBUS H125 | AIRBUS H130 | AGUSTA / LEONARDO AW119Kx | AGUSTA / LEONARDO SH09 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 5.00 | $ 6.76 | $4.48 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 7 | 8 | 8 |
| Flight Rules | VFR | VFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Leonardo | Leonardo |
| Aircraft Name | H125 | H130 | AW119Kx | SH09 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | In-Development |
| Max Range (nm) | 341 | 333 | 515 | 430 |
| DOC / nm / Seat | $ 0.77 | $ 0.71 | $ 0.84 | $0.56 |
| Max Cabin Seats | 5 | 5 | 6 | 6 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | 2299 | — | — |
| Standard Cabin Seats | 4 | 4 | 6 | 6 |
| Direct Operating Cost | $ 627 | $ 640 | $ 885 | $627 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G500H | Garmin G1000H | EFIS |
| Max Cruise Speed (ktas) | 136 | 128 | 131 | 140 |
| Base Aircraft Price (USD) | $3,200,000 | $3,450,000 | $3,850,000 | $3,500,000 |
| Max Passengers | — | — | — | 7 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 7 | 8 | 8 |
| Max Cabin Seats | 5 | 5 | 6 | — |
| Standard Cabin Seats | 4 | 4 | 6 | 6 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Arriel 2D | Arriel 2D | PT6B-37A | HTS 900 |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 5000 | 4500 | 5500 |
| Horsepower | 847 | 952 | 917 | 1020 |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 143 | 160 | — |
| Dimensions | ||||
| Length (ft) | 42.5 | 41.5 | 42.5 | — |
| Overall Height (ft) | 10 | 11.1 | 11.9 | — |
| Rotor Diameter (ft) | 36.1 | 35.1 | 35.5 | — |