Airbus Helicopters H125 vs Daher Kodiak 100 Series Iii vs Daher Tbm 960 vs Leonardo Aw119kx
The Airbus Helicopters H125 and Leonardo AW119Kx are single‑engine helicopters focused on short‑range utility, aerial work, and flexible point‑to‑point access where runways aren’t available. In category terms, both are light single‑engine rotorcraft; the H125 is typically optimized for high‑altitude/hot‑and‑high performance and external‑load missions, while the AW119Kx emphasizes a roomy cabin and IFR‑capable operations depending on configuration. Their practical ranges are generally in the few‑hundred‑nautical‑mile class, varying with payload, fuel, and reserves, and passenger capacity is commonly around five to six passengers plus a pilot in typical layouts. The Daher Kodiak 100 Series III is a single‑engine turboprop STOL utility airplane, aimed at rugged short‑field operations with longer legs than the helicopters. It typically seats up to about 9 passengers (plus pilot), with range commonly in the roughly 1,000‑nautical‑mile class depending on load. The Daher TBM 960 is a high‑performance, pressurized single‑engine turboprop airplane in the personal/business category, trading utility for speed and efficiency. It generally carries 4 to 6 passengers (plus pilot) and offers the longest range here, typically around the mid‑1,000‑nautical‑mile class.
| Spec | AIRBUS H125 | Daher TBM 960 | AGUSTA / LEONARDO AW119Kx |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 2.25 | $ 6.76 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 |
| Flight Rules | VFR | IFR | VFR |
| Manufacturer | Airbus Helicopters | Daher TBM | Leonardo |
| Aircraft Name | H125 | TBM 960 | AW119Kx |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 1730 | 515 |
| DOC / nm / Seat | $ 0.77 | $ 0.56 | $ 0.84 |
| Max Cabin Seats | 5 | — | 6 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | 2908 | — |
| Standard Cabin Seats | 4 | 4 | 6 |
| Direct Operating Cost | $ 627 | $ 744 | $ 885 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G3000 | Garmin G1000H |
| Max Cruise Speed (ktas) | 136 | 330 | 131 |
| Base Aircraft Price (USD) | $3,200,000 | $4,450,000 | $3,850,000 |
| Aircraft Type | — | Turbo Prop | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 |
| Max Cabin Seats | 5 | — | 6 |
| Standard Cabin Seats | 4 | 4 | 6 |
| Lavatory | — | No | — |
| Galley Location | — | MID | — |
| Cabin Pressure (psi) | — | 6.2 | — |
| SL Cabin Altitude (ft) | — | 14390 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Arriel 2D | TBM 960 | PT6B-37A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 5000 | 3500 | 4500 |
| Horsepower | 847 | 850 | 917 |
| No. of Engines | 1 | — | 1 |
| Fuel Capacity (gal) | 143 | — | 160 |
| Flat Rating | — | ISA + 49 | — |
| Dimensions | |||
| Length (ft) | 42.5 | 35.3 | 42.5 |
| Overall Height (ft) | 10 | — | 11.9 |
| Rotor Diameter (ft) | 36.1 | — | 35.5 |
| Wingspan (ft) | — | 42.1 | — |
| Cabin Width (ft) | — | 4 | — |
| Cabin Height (ft) | — | 4.1 | — |
| Cabin Length (ft) | — | 13.4 | — |
| Cabin Volume (cu. ft) | — | 123 | — |