Airbus Helicopters H125 vs Leonardo Aw109 Trekker vs Md Helicopters Md 520n
Airbus Helicopters’ H125 sits in the light single-engine utility category, optimized for high-altitude and hot-and-high work. It typically carries a pilot plus up to five or six passengers depending on configuration, and offers a mid-range mission profile suited to regional transport, tourism, and utility flying, generally a few hundred nautical miles with reserves (often extendable with auxiliary fuel). The Leonardo AW109 Trekker is a light twin-engine, multi-role helicopter positioned a step up in performance and redundancy. It usually accommodates a pilot (or two) plus about six to seven passengers in an executive or utility layout, and it generally delivers the longest range of the three, making it well suited to longer point-to-point trips and IFR-capable operations. The MD Helicopters MD 520N is a light single-engine helicopter notable for its NOTAR anti-torque system and low external noise signature. Passenger capacity is typically lower than the H125 and AW109 Trekker, commonly around four passengers plus a pilot, and its practical range is generally shorter to mid-range compared with the AW109 Trekker, aligning it with training, patrol, and short-hop utility missions.
| Spec | AIRBUS H125 | AGUSTA / LEONARDO AW109 Trekker | MD Helicopters MD 520N |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 7.40 | $ 3.38 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 4 |
| Flight Rules | VFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Leonardo | MD Helicotpers |
| Aircraft Name | H125 | AW109 Trekker | MD 520N |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 450 | 210 |
| DOC / nm / Seat | $ 0.77 | $ 0.93 | $ 0.85 |
| Max Cabin Seats | 5 | 6 | 3 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | — | 1764 |
| Standard Cabin Seats | 4 | 6 | 2 |
| Direct Operating Cost | $ 627 | $ 1,125 | $ 416 |
| Flight Deck (Base Spec) | Garmin G500H | Genesys Aerosystems | Gyro / Analog |
| Max Cruise Speed (ktas) | 136 | 152 | 123 |
| Base Aircraft Price (USD) | $3,200,000 | $6,950,000 | $ 2,900,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 4 |
| Max Cabin Seats | 5 | 6 | 3 |
| Standard Cabin Seats | 4 | 6 | 2 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | Arriel 2D | PW207C | 250-C20R |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 4000 | 3500 |
| Horsepower | 847 | 735 | 450 |
| No. of Engines | 1 | 2 | 1 |
| Fuel Capacity (gal) | 143 | 152 | 64 |
| Fuel Burn (gph) | — | — | 35 |
| Dimensions | |||
| Length (ft) | 42.5 | 42.5 | 31.4 |
| Overall Height (ft) | 10 | 11.5 | 8.8 |
| Rotor Diameter (ft) | 36.1 | 35.5 | 27.4 |