Airbus Helicopters H225 vs Daher Tbm 960 vs Dassault Falcon 8x vs Embraer Legacy 650 E
The Airbus H225 is a heavy twin‑engine helicopter, suited to short-to-medium missions where vertical lift matters more than speed and altitude. Its practical range is roughly 400–500 nautical miles depending on payload and reserves, and it typically carries about 16–19 passengers in transport layouts. The Daher TBM 960 is a single‑engine turboprop airplane optimized for owner‑pilot efficiency and short-field access. It offers about 1,700–1,800 nautical miles of range and usually seats 4–6 passengers in comfort (up to about 6–7 including pilot, depending on configuration). The Dassault Falcon 8X is an ultra‑long‑range large‑cabin business jet designed for intercontinental travel. It delivers about 6,400 nautical miles of range and is commonly configured for 12–16 passengers, with some layouts accommodating more. The Embraer Legacy 650E is a long‑range large‑cabin business jet, typically used for transcontinental missions. Its range is about 3,900–4,000 nautical miles and it generally seats 13 passengers in standard executive configurations (often up to 14).
| Spec | AIRBUS H225 | Daher TBM 960 | Dassault Falcon 8X |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | $ 7.66 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 6 | 17 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Daher TBM | Dassault Falcon |
| Aircraft Name | H225 | TBM 960 | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | $ 0.64 |
| Max Cabin Seats | 28 | — | 16 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 2908 | 36900 |
| Standard Cabin Seats | 19 | 4 | 14 |
| Direct Operating Cost | $ 2,963 | $ 744 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 330 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $ 62,500,000 |
| Aircraft Type | — | Turbo Prop | — |
| Cabin | |||
| Cockpit | 2 | 2 | 3 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 6 | 17 |
| Max Cabin Seats | 28 | — | 16 |
| Standard Cabin Seats | 19 | 4 | 14 |
| Lavatory | — | No | 2 Enclosed Flushing |
| Galley Location | — | MID | FWD |
| Cabin Pressure (psi) | — | 6.2 | 10.2 |
| SL Cabin Altitude (ft) | — | 14390 | 29200 |
| Crew Rest | — | — | No |
| Jump Seat | — | — | Yes |
| Lavatory Location | — | — | FWD / AFT |
| Galley / Refreshment | — | — | Galley |
| Max Cabin Altitude (ft) | — | — | 3900 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | TBM 960 | PW307D |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 3500 | On-Condition |
| Horsepower | 2100 | 850 | — |
| No. of Engines | 2 | — | 3 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 49 | ISA + 17 |
| Thrust (lbs) | — | — | 6722 |
| Dimensions | |||
| Length (ft) | 63.4 | 35.3 | 80.2 |
| Overall Height (ft) | 16.3 | — | 26.1 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | 1695 |
| Wingspan (ft) | — | 42.1 | 86.3 |
| Cabin Width (ft) | — | 4 | 7.7 |
| Cabin Height (ft) | — | 4.1 | 6.2 |
| Cabin Length (ft) | — | 13.4 | 42.7 |
| Cabin Width - Floor (ft) | — | — | 6.3 |
| Cabin Length - Seating (ft) | — | — | 29.2 |
| Baggage Volume Int. (cu. ft) | — | — | 140 |