Airbus Helicopters H125 vs Bell 407gxi vs Md Helicopters Md 600n
The Airbus Helicopters H125 (AS350) and Bell 407GXi sit in the same general light single‑engine utility class, while the MD Helicopters MD 600N is also a light single but differentiated by its NOTAR anti‑torque system aimed at reducing tail‑rotor risk and perceived noise. In typical missions, the H125 is often chosen for high/hot and lifting utility work, the 407GXi for fast, smooth general transport and corporate/public‑service roles, and the 600N for operations that value NOTAR’s handling and safety characteristics. On range, all three are broadly comparable in practical terms, but the H125 and 407GXi commonly deliver the longer legs depending on fuel configuration and operating profile, with the 600N generally a bit shorter in typical real‑world planning. Passenger capacity is similar across the set: they are usually configured to carry one pilot plus about five to six passengers, with exact seating depending on interior layout, mission equipment, and weight limits.
| Spec | AIRBUS H125 | Bell 407GXi | MD Helicopters MD 600N |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 4.43 | $ 4.06 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 6 |
| Flight Rules | VFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Bell | MD Helicotpers |
| Aircraft Name | H125 | 407GXi | MD 600N |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 337 | 341 |
| DOC / nm / Seat | $ 0.77 | $ 0.74 | $ 0.68 |
| Max Cabin Seats | 5 | 5 | 5 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2189 | 2300 | 2000 |
| Standard Cabin Seats | 4 | 5 | 5 |
| Direct Operating Cost | $ 627 | $ 589 | $ 545 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G1000H NXI | Gyro / Analog |
| Max Cruise Speed (ktas) | 136 | 133 | 134 |
| Base Aircraft Price (USD) | $3,200,000 | $3,225,000 | $3,400,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 6 |
| Max Cabin Seats | 5 | 5 | 5 |
| Standard Cabin Seats | 4 | 5 | 5 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | Arriel 2D | M250-C47E/4 | 250-C47 |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 3500 | 2000 |
| Horsepower | 847 | 862 | 715 |
| No. of Engines | 1 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 127.8 | 118 |
| Fuel Burn (gph) | — | 46 | 41 |
| Dimensions | |||
| Length (ft) | 42.5 | 41.4 | 36.9 |
| Overall Height (ft) | 10 | 10.2 | 9.7 |
| Rotor Diameter (ft) | 36.1 | 35 | 27.5 |
| Width (ft) | — | 25.4 | — |
| Cabin Width (ft) | — | 5 | — |
| Cabin Height (ft) | — | 3.9 | — |
| Cabin Volume (cu. ft) | — | 125 | — |
| Baggage Volume Ext. (cu. ft) | — | 16 | — |