Airbus Helicopters H125 vs Leonardo Aw109 Trekker vs Leonardo Aw119kx vs Leonardo Aw169
Airbus Helicopters’ H125 is a light single‑engine utility helicopter, typically carrying a pilot plus about five to six passengers (configuration dependent). It is valued for simple operation and strong performance in hot‑and‑high conditions, with a practical range commonly in the roughly 300–350 nautical mile class depending on fuel fit and reserves. Leonardo’s AW109 Trekker is a light twin‑engine helicopter positioned for faster point‑to‑point transport and premium utility missions. It generally seats six to seven passengers (plus crew) and tends to offer a similar or somewhat greater practical range than light singles, often around the mid‑300‑nautical‑mile range depending on configuration. The Leonardo AW119Kx is a light single‑engine helicopter with a roomy cabin for its class. It typically carries about six to seven passengers and delivers range broadly comparable to other light singles, commonly around 300 nautical miles depending on equipment and mission profile. The Leonardo AW169 is a larger, intermediate twin‑engine helicopter with higher payload and cabin volume. It typically accommodates around eight to ten passengers and offers longer legs in many configurations, often roughly 400 nautical miles or more depending on fuel and reserves.
| Spec | AIRBUS H125 | AGUSTA / LEONARDO AW109 Trekker | AGUSTA / LEONARDO AW119Kx | AGUSTA / LEONARDO AW169 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 7.40 | $ 6.76 | $ 11.84 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 8 | 12 |
| Flight Rules | VFR | VFR | VFR | IFR |
| Manufacturer | Airbus Helicopters | Leonardo | Leonardo | Leonardo |
| Aircraft Name | H125 | AW109 Trekker | AW119Kx | AW169 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 450 | 515 | 440 |
| DOC / nm / Seat | $ 0.77 | $ 0.93 | $ 0.84 | $ 0.99 |
| Max Cabin Seats | 5 | 6 | 6 | 10 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | — | — | — |
| Standard Cabin Seats | 4 | 6 | 6 | 10 |
| Direct Operating Cost | $ 627 | $ 1,125 | $ 885 | $ 1,658 |
| Flight Deck (Base Spec) | Garmin G500H | Genesys Aerosystems | Garmin G1000H | EFIS |
| Max Cruise Speed (ktas) | 136 | 152 | 131 | 140 |
| Base Aircraft Price (USD) | $3,200,000 | $6,950,000 | $3,850,000 | $9,450,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 8 | 12 |
| Max Cabin Seats | 5 | 6 | 6 | 10 |
| Standard Cabin Seats | 4 | 6 | 6 | 10 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Arriel 2D | PW207C | PT6B-37A | PW210A |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 4000 | 4500 | 4000 |
| Horsepower | 847 | 735 | 917 | 1000 |
| No. of Engines | 1 | 2 | 1 | 2 |
| Fuel Capacity (gal) | 143 | 152 | 160 | — |
| Dimensions | ||||
| Length (ft) | 42.5 | 42.5 | 42.5 | 48.1 |
| Overall Height (ft) | 10 | 11.5 | 11.9 | 14.8 |
| Rotor Diameter (ft) | 36.1 | 35.5 | 35.5 | — |
| Cabin Volume (cu. ft) | — | — | — | 222.5 |
| Baggage Volume Ext. (cu. ft) | — | — | — | 49.5 |