Airbus Helicopters H125 vs Leonardo Aw109 Trekker vs Leonardo Aw139 vs Leonardo Aw169 vs Leonardo Aw609 Tiltrotor
The Airbus Helicopters H125 is a light single‑engine utility helicopter, best suited to short to medium missions, with typical seating for about five to six passengers plus a pilot and a range roughly in the 300–350 nautical mile class depending on fit and reserves. The Leonardo AW109 Trekker is a light twin‑engine helicopter aimed at faster point‑to‑point travel, usually carrying about six to seven passengers with ranges commonly around 400–500 nautical miles. The Leonardo AW169 sits in the light‑intermediate twin category, offering a larger cabin for about eight to ten passengers and a broadly similar mid‑range profile, often around 400–500 nautical miles. The Leonardo AW139 is a medium twin, optimized for offshore, SAR, and corporate shuttle roles, typically accommodating about 12–15 passengers and delivering mid to longer ranges, commonly around 500–650 nautical miles. The Leonardo AW609 is a tiltrotor rather than a conventional helicopter, combining vertical takeoff with airplane‑like cruise; it generally seats about six to nine passengers and is designed for substantially longer legs, roughly in the 700–1,000+ nautical mile range, depending on configuration.
| Spec | AIRBUS H125 | AGUSTA / LEONARDO AW109 Trekker | AGUSTA / LEONARDO AW139 | AGUSTA / LEONARDO AW169 | AGUSTA / LEONARDO AW609 Tiltrotor |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | — |
| DOC / nm | $ 4.61 | $ 7.40 | $ 11.69 | $ 11.84 | — |
| Min Crew | 1 | 1 | 2 | 1 | — |
| Total Seats | 6 | 8 | 17 | 12 | — |
| Flight Rules | VFR | VFR | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Leonardo | Leonardo | Leonardo | Leonardo |
| Aircraft Name | H125 | AW109 Trekker | AW139 | AW169 | AW609 Tiltrotor |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | — |
| Max Range (nm) | 341 | 450 | 573 | 440 | — |
| DOC / nm / Seat | $ 0.77 | $ 0.93 | $ 0.69 | $ 0.99 | — |
| Max Cabin Seats | 5 | 6 | 15 | 10 | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified | — |
| Useful Load (lbs) | 2189 | — | 4701 | — | — |
| Standard Cabin Seats | 4 | 6 | 15 | 10 | — |
| Direct Operating Cost | $ 627 | $ 1,125 | $ 1,929 | $ 1,658 | — |
| Flight Deck (Base Spec) | Garmin G500H | Genesys Aerosystems | EFIS | EFIS | — |
| Max Cruise Speed (ktas) | 136 | 152 | 165 | 140 | — |
| Base Aircraft Price (USD) | $3,200,000 | $6,950,000 | $15,900,000 | $9,450,000 | $20,000,000 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | — |
| Min Crew | 1 | 1 | 2 | 1 | — |
| Total Seats | 6 | 8 | 17 | 12 | — |
| Max Cabin Seats | 5 | 6 | 15 | 10 | — |
| Standard Cabin Seats | 4 | 6 | 15 | 10 | — |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | — |
| Model | Arriel 2D | PW207C | PT6C-67C | PW210A | — |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | — |
| TBO (hrs) | 5000 | 4000 | 5000 | 4000 | — |
| Horsepower | 847 | 735 | 1679 | 1000 | — |
| No. of Engines | 1 | 2 | 2 | 2 | — |
| Fuel Capacity (gal) | 143 | 152 | 414 | — | — |
| Dimensions | |||||
| Length (ft) | 42.5 | 42.5 | 54.7 | 48.1 | — |
| Overall Height (ft) | 10 | 11.5 | 16.4 | 14.8 | — |
| Rotor Diameter (ft) | 36.1 | 35.5 | 54.7 | — | — |
| Cabin Volume (cu. ft) | — | — | 282 | 222.5 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 120 | 49.5 | — |