Airbus Helicopters H225 vs Daher Tbm 960 vs Embraer Legacy 650 E
The Airbus H225 is a heavy, twin‑engine helicopter suited to offshore transport, SAR, and utility missions. It typically carries around 16 to 19 passengers in a high‑density configuration (fewer for VIP layouts) and offers roughly 450 to 500 nautical miles of range depending on payload and reserves, trading speed and range for vertical‑lift access and hover capability. The Daher TBM 960 is a single‑engine turboprop airplane optimized for fast, efficient point‑to‑point travel. It is generally configured for 4 to 6 passengers plus a pilot, with a practical range around 1,400 to 1,700 nautical miles (mission dependent), making it ideal for regional and medium‑length trips into smaller airports. The Embraer Legacy 650E is a large‑cabin business jet designed for long‑range corporate travel. It typically seats about 12 to 13 passengers in executive layouts and can fly roughly 3,900 to 4,000 nautical miles, focusing on comfort, baggage volume, and nonstop intercity or transcontinental missions.
| Spec | AIRBUS H225 | Daher TBM 960 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 6 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Daher TBM |
| Aircraft Name | H225 | TBM 960 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 |
| Max Cabin Seats | 28 | — |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 2908 |
| Standard Cabin Seats | 19 | 4 |
| Direct Operating Cost | $ 2,963 | $ 744 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 330 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 |
| Aircraft Type | — | Turbo Prop |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 6 |
| Max Cabin Seats | 28 | — |
| Standard Cabin Seats | 19 | 4 |
| Lavatory | — | No |
| Galley Location | — | MID |
| Cabin Pressure (psi) | — | 6.2 |
| SL Cabin Altitude (ft) | — | 14390 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 2A1 | TBM 960 |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | 3500 |
| Horsepower | 2100 | 850 |
| No. of Engines | 2 | — |
| Fuel Capacity (gal) | 684 | — |
| Flat Rating | — | ISA + 49 |
| Dimensions | ||
| Length (ft) | 63.4 | 35.3 |
| Overall Height (ft) | 16.3 | — |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | 123 |
| Wingspan (ft) | — | 42.1 |
| Cabin Width (ft) | — | 4 |
| Cabin Height (ft) | — | 4.1 |
| Cabin Length (ft) | — | 13.4 |