Airbus Helicopters H125 vs Leonardo Aw109 Trekker vs Leonardo Aw119kx vs Leonardo Aw139 vs Leonardo Aw169
The Airbus Helicopters H125 is a light single‑engine utility helicopter, typically carrying about 5–6 passengers (plus pilot) with a practical range around 330–360 nm depending on configuration. The Leonardo AW109 Trekker is a light twin, generally used for faster transport and light EMS/corporate missions, commonly seating about 6–7 passengers with an approximate range of roughly 420–480 nm. The Leonardo AW119Kx is a light single with a roomy cabin for its class, often arranged for about 6–7 passengers and offering about 340–380 nm of range. Moving up, the Leonardo AW169 is a light‑intermediate twin intended for EMS, offshore support, and corporate transport, typically accommodating around 8–10 passengers with roughly 440–500 nm range. The Leonardo AW139 is a medium twin with substantially higher payload and cabin volume, commonly configured for about 12–15 passengers and offering approximately 550–650 nm range. Actual figures vary with fuel reserves, interiors, weight, and mission profile.
| Spec | AIRBUS H125 | AGUSTA / LEONARDO AW109 Trekker | AGUSTA / LEONARDO AW119Kx | AGUSTA / LEONARDO AW139 | AGUSTA / LEONARDO AW169 |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 7.40 | $ 6.76 | $ 11.69 | $ 11.84 |
| Min Crew | 1 | 1 | 1 | 2 | 1 |
| Total Seats | 6 | 8 | 8 | 17 | 12 |
| Flight Rules | VFR | VFR | VFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Leonardo | Leonardo | Leonardo | Leonardo |
| Aircraft Name | H125 | AW109 Trekker | AW119Kx | AW139 | AW169 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 450 | 515 | 573 | 440 |
| DOC / nm / Seat | $ 0.77 | $ 0.93 | $ 0.84 | $ 0.69 | $ 0.99 |
| Max Cabin Seats | 5 | 6 | 6 | 15 | 10 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | — | — | 4701 | — |
| Standard Cabin Seats | 4 | 6 | 6 | 15 | 10 |
| Direct Operating Cost | $ 627 | $ 1,125 | $ 885 | $ 1,929 | $ 1,658 |
| Flight Deck (Base Spec) | Garmin G500H | Genesys Aerosystems | Garmin G1000H | EFIS | EFIS |
| Max Cruise Speed (ktas) | 136 | 152 | 131 | 165 | 140 |
| Base Aircraft Price (USD) | $3,200,000 | $6,950,000 | $3,850,000 | $15,900,000 | $9,450,000 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 2 | 1 |
| Total Seats | 6 | 8 | 8 | 17 | 12 |
| Max Cabin Seats | 5 | 6 | 6 | 15 | 10 |
| Standard Cabin Seats | 4 | 6 | 6 | 15 | 10 |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | Yes |
| Model | Arriel 2D | PW207C | PT6B-37A | PT6C-67C | PW210A |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 4000 | 4500 | 5000 | 4000 |
| Horsepower | 847 | 735 | 917 | 1679 | 1000 |
| No. of Engines | 1 | 2 | 1 | 2 | 2 |
| Fuel Capacity (gal) | 143 | 152 | 160 | 414 | — |
| Dimensions | |||||
| Length (ft) | 42.5 | 42.5 | 42.5 | 54.7 | 48.1 |
| Overall Height (ft) | 10 | 11.5 | 11.9 | 16.4 | 14.8 |
| Rotor Diameter (ft) | 36.1 | 35.5 | 35.5 | 54.7 | — |
| Cabin Volume (cu. ft) | — | — | — | 282 | 222.5 |
| Baggage Volume Ext. (cu. ft) | — | — | — | 120 | 49.5 |