Airbus Helicopters H130 vs Dassault Falcon 8x vs Leonardo Aw109 Trekker vs Leonardo Aw119kx
By category, the Airbus Helicopters H130, Leonardo AW109 Trekker, and Leonardo AW119Kx are light single- or twin‑engine helicopters suited to short-range utility, tourism, EMS, and private transport, while the Dassault Falcon 8X is a long-range, large-cabin tri‑jet business aircraft designed for intercontinental missions. In range terms, the Falcon 8X is in a different class, typically capable of roughly 6,400–6,450 nautical miles, enabling nonstop routes such as New York–Dubai under favorable conditions. The helicopters are measured in hundreds of nautical miles rather than thousands: the H130 commonly offers around 330–350 nm, the AW109 Trekker roughly 450–500 nm depending on configuration and reserves, and the AW119Kx typically around 300–350 nm. Passenger capacity also separates them: the Falcon 8X typically carries about 12–16 passengers in an executive layout (with maximums higher depending on certification), whereas the H130 is generally configured for up to 6–7 passengers plus pilot, the AW109 Trekker for about 6–7 passengers plus crew, and the AW119Kx for up to 6–7 passengers plus pilot, with layouts varying by mission equipment and seating choices.
| Spec | AIRBUS H130 | Dassault Falcon 8X | AGUSTA / LEONARDO AW109 Trekker | AGUSTA / LEONARDO AW119Kx |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| DOC / nm | $ 5.00 | $ 7.66 | $ 7.40 | $ 6.76 |
| Min Crew | 1 | 2 | 1 | 1 |
| Total Seats | 7 | 17 | 8 | 8 |
| Flight Rules | VFR | — | VFR | VFR |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Leonardo | Leonardo |
| Aircraft Name | H130 | 8X | AW109 Trekker | AW119Kx |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 333 | 6450 | 450 | 515 |
| DOC / nm / Seat | $ 0.71 | $ 0.64 | $ 0.93 | $ 0.84 |
| Max Cabin Seats | 5 | 16 | 6 | 6 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2299 | 36900 | — | — |
| Standard Cabin Seats | 4 | 14 | 6 | 6 |
| Direct Operating Cost | $ 640 | $ 3,805 | $ 1,125 | $ 885 |
| Flight Deck (Base Spec) | Garmin G500H | Honeywell Primus EASy II | Genesys Aerosystems | Garmin G1000H |
| Max Cruise Speed (ktas) | 128 | 516 | 152 | 131 |
| Base Aircraft Price (USD) | $3,450,000 | $ 62,500,000 | $6,950,000 | $3,850,000 |
| Cabin | ||||
| Cockpit | 3 | 3 | 2 | 2 |
| Min Crew | 1 | 2 | 1 | 1 |
| Total Seats | 7 | 17 | 8 | 8 |
| Max Cabin Seats | 5 | 16 | 6 | 6 |
| Standard Cabin Seats | 4 | 14 | 6 | 6 |
| Lavatory | — | 2 Enclosed Flushing | — | — |
| Crew Rest | — | No | — | — |
| Jump Seat | — | Yes | — | — |
| Galley Location | — | FWD | — | — |
| Lavatory Location | — | FWD / AFT | — | — |
| Cabin Pressure (psi) | — | 10.2 | — | — |
| Galley / Refreshment | — | Galley | — | — |
| SL Cabin Altitude (ft) | — | 29200 | — | — |
| Max Cabin Altitude (ft) | — | 3900 | — | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Arriel 2D | PW307D | PW207C | PT6B-37A |
| Fuel Type | JetFuel | — | JetFuel | JetFuel |
| TBO (hrs) | 5000 | On-Condition | 4000 | 4500 |
| Horsepower | 952 | — | 735 | 917 |
| No. of Engines | 1 | 3 | 2 | 1 |
| Fuel Capacity (gal) | 143 | — | 152 | 160 |
| Flat Rating | — | ISA + 17 | — | — |
| Thrust (lbs) | — | 6722 | — | — |
| Dimensions | ||||
| Length (ft) | 41.5 | 80.2 | 42.5 | 42.5 |
| Overall Height (ft) | 11.1 | 26.1 | 11.5 | 11.9 |
| Rotor Diameter (ft) | 35.1 | — | 35.5 | 35.5 |
| Wingspan (ft) | — | 86.3 | — | — |
| Cabin Width (ft) | — | 7.7 | — | — |
| Cabin Height (ft) | — | 6.2 | — | — |
| Cabin Length (ft) | — | 42.7 | — | — |
| Cabin Volume (cu. ft) | — | 1695 | — | — |
| Cabin Width - Floor (ft) | — | 6.3 | — | — |
| Cabin Length - Seating (ft) | — | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | — | 140 | — | — |