Airbus Helicopters H145 vs Md Helicopters Md 600n
The Airbus Helicopters H145 and the MD Helicopters MD 600N both sit in the light twin/turbine utility space, but they target different mission priorities. The H145 is a modern light twin‑engine helicopter commonly used for EMS, law enforcement, offshore support, and corporate transport, emphasizing redundancy, high useful load, and a spacious cabin. The MD 600N is a light single‑engine helicopter, often favored for lower operating complexity and roles such as utility work, patrol, and aerial observation, with its NOTAR anti‑torque system reducing tail‑rotor hazards and noise. In range, the H145 generally offers a longer practical mission radius and better performance margins across varied conditions, especially when configured with auxiliary fuel, while the MD 600N typically provides a shorter overall range consistent with its lighter, single‑engine class. For passenger capacity, the H145 usually carries more people in typical transport layouts, commonly accommodating a pilot plus several passengers with flexible cabin arrangements. The MD 600N generally seats fewer, typically a pilot plus a smaller passenger load, reflecting its smaller cabin and mission focus.
| Spec | AIRBUS H145 | MD Helicopters MD 600N |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 9.31 | $ 4.06 |
| Min Crew | 1 | 1 |
| Total Seats | 10 | 6 |
| Flight Rules | IFR | VFR |
| Manufacturer | Airbus Helicopters | MD Helicotpers |
| Aircraft Name | H145 | MD 600N |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 341 |
| DOC / nm / Seat | $ 0.93 | $ 0.68 |
| Max Cabin Seats | 9 | 5 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4200 | 2000 |
| Standard Cabin Seats | 8 | 5 |
| Direct Operating Cost | $ 1,210 | $ 545 |
| Flight Deck (Base Spec) | EFIS | Gyro / Analog |
| Max Cruise Speed (ktas) | 130 | 134 |
| Base Aircraft Price (USD) | $10,200,000 | $3,400,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 10 | 6 |
| Configuration | Green Interior | — |
| Max Cabin Seats | 9 | 5 |
| Standard Cabin Seats | 8 | 5 |
| Engine | ||
| FADEC | Yes | No |
| Model | Arriel 2E | 250-C47 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 2000 |
| Horsepower | 894 | 715 |
| No. of Engines | 2 | 1 |
| Fuel Burn (gph) | — | 41 |
| Fuel Capacity (gal) | — | 118 |
| Dimensions | ||
| Length (ft) | 44.8 | 36.9 |
| Overall Height (ft) | 13 | 9.7 |
| Rotor Diameter (ft) | 36.1 | 27.5 |
| Cabin Volume (cu. ft) | 166 | — |
| Baggage Volume Ext. (cu. ft) | 46.8 | — |