Airbus Helicopters H125 vs Md Helicopters Md 600n
The Airbus Helicopters H125 (AS350 B3e) and the MD Helicopters MD 600N are both single‑engine utility helicopters often used for law enforcement, EMS support roles, tourism, and general lift, but they differ in emphasis. The H125 is generally positioned as a higher‑payload, high‑altitude/hot‑and‑high capable utility platform, widely chosen for mountain and external‑load work, while the MD 600N is often valued for its quieter operation thanks to its NOTAR (no tail rotor) anti‑torque system, which can be attractive in urban, noise‑sensitive, or confined‑area operations. In range, both are broadly comparable for typical mission profiles, with the H125 commonly offering slightly more practical endurance/range depending on configuration, fuel options, and payload. Passenger capacity is similar overall: each can be configured for around six occupants including the pilot in common layouts, though exact seating and usable load vary notably with equipment, fuel, and operating conditions.
| Spec | AIRBUS H125 | MD Helicopters MD 600N |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 4.61 | $ 4.06 |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 6 |
| Flight Rules | VFR | VFR |
| Manufacturer | Airbus Helicopters | MD Helicotpers |
| Aircraft Name | H125 | MD 600N |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 341 |
| DOC / nm / Seat | $ 0.77 | $ 0.68 |
| Max Cabin Seats | 5 | 5 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2189 | 2000 |
| Standard Cabin Seats | 4 | 5 |
| Direct Operating Cost | $ 627 | $ 545 |
| Flight Deck (Base Spec) | Garmin G500H | Gyro / Analog |
| Max Cruise Speed (ktas) | 136 | 134 |
| Base Aircraft Price (USD) | $3,200,000 | $3,400,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 6 |
| Max Cabin Seats | 5 | 5 |
| Standard Cabin Seats | 4 | 5 |
| Engine | ||
| FADEC | Yes | No |
| Model | Arriel 2D | 250-C47 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 2000 |
| Horsepower | 847 | 715 |
| No. of Engines | 1 | 1 |
| Fuel Capacity (gal) | 143 | 118 |
| Fuel Burn (gph) | — | 41 |
| Dimensions | ||
| Length (ft) | 42.5 | 36.9 |
| Overall Height (ft) | 10 | 9.7 |
| Rotor Diameter (ft) | 36.1 | 27.5 |