Airbus Helicopters H125 vs Leonardo Aw119kx vs Robinson Helicopters R44 Raven I vs Robinson Helicopters R44 Raven Ii
The Airbus Helicopters H125 and Leonardo AW119Kx are single‑engine light utility helicopters in a higher performance class than the Robinson R44 variants. In category terms, the H125 is commonly used for utility, lifting, and high‑hot operations; the AW119Kx is a fast, spacious single‑engine light helicopter often positioned toward executive and EMS support roles. Both typically offer longer range than the Robinsons, with the AW119Kx and H125 generally in the roughly 400–600 km class depending on tanks, payload, and reserves, while the R44s are usually closer to roughly 450–560 km depending on configuration and operating conditions. For passenger capacity, the H125 and AW119Kx are typically configured for about 5–6 passengers plus a pilot (layouts vary), whereas the Robinson R44 Raven I and Raven II are four‑seat aircraft in total, commonly one pilot plus up to three passengers. Between the Robinson models, the Raven II is the updated, higher‑gross‑weight, more powerful variant, which can translate into better performance and practical range flexibility than the Raven I, though both remain in the same basic light piston category.
| Spec | AIRBUS H125 | AGUSTA / LEONARDO AW119Kx | ROBINSON R44 Raven I | ROBINSON R44 Raven II |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | — | — |
| DOC / nm | $ 4.61 | $ 6.76 | $ 2.30 | $ 2.36 |
| Min Crew | 1 | 1 | — | — |
| Total Seats | 6 | 8 | 4 | 4 |
| Flight Rules | VFR | VFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Leonardo | Robinson Helicopters | Robinson Helicopters |
| Aircraft Name | H125 | AW119Kx | R44 Raven I | R44 Raven II |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 515 | 300 | 300 |
| DOC / nm / Seat | $ 0.77 | $ 0.84 | $ 0.57 | $ 0.59 |
| Max Cabin Seats | 5 | 6 | — | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | — | 950 | 995 |
| Standard Cabin Seats | 4 | 6 | — | — |
| Direct Operating Cost | $ 627 | $ 885 | $ 248 | $ 257 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G1000H | Gyro / Analog | Gyro / Analog |
| Max Cruise Speed (ktas) | 136 | 131 | 108 | 109 |
| Base Aircraft Price (USD) | $3,200,000 | $3,850,000 | $ 412,000 | $ 490,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | — | — |
| Min Crew | 1 | 1 | — | — |
| Total Seats | 6 | 8 | 4 | 4 |
| Max Cabin Seats | 5 | 6 | — | — |
| Standard Cabin Seats | 4 | 6 | — | — |
| Engine | ||||
| FADEC | Yes | Yes | No | No |
| Model | Arriel 2D | PT6B-37A | O-540 | IO-540 |
| Fuel Type | JetFuel | JetFuel | AvGas | AvGas |
| TBO (hrs) | 5000 | 4500 | 2200 | 2200 |
| Horsepower | 847 | 917 | 225 | 245 |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 160 | 29.5 | 29.5 |
| TBO (yrs) | — | — | 12 | 12 |
| Fuel Delivery | — | — | Carbureted | Fuel Injected |
| Dimensions | ||||
| Length (ft) | 42.5 | 42.5 | 38.3 | 38.3 |
| Overall Height (ft) | 10 | 11.9 | 10.8 | 10.8 |
| Rotor Diameter (ft) | 36.1 | 35.5 | 33 | 33 |
| Baggage Volume Int. (cu. ft) | — | — | 2.5 | 2.5 |