Airbus Helicopters H225 vs Dassault Falcon 8x
The Airbus H225 and the Dassault Falcon 8X sit in different aircraft categories and are optimized for different missions. The H225 is a large twin‑engine helicopter typically used for offshore energy support, search and rescue, and utility transport, offering vertical takeoff and landing and the ability to operate where runways are unavailable. The Falcon 8X is a long‑range, three‑engine business jet designed for high‑speed, high‑altitude intercontinental travel between airports. In range, the Falcon 8X is far superior for point‑to‑point distance, with an advertised range around 6,450 nautical miles, enabling nonstop long‑haul routes. The H225’s range is much shorter—generally a few hundred nautical miles depending on payload and fuel configuration—reflecting typical helicopter mission profiles. Passenger capacity also differs by use case: the H225 is commonly configured to carry roughly 16 to 19 passengers in transport layouts (and can be arranged for specialized roles), while the Falcon 8X usually carries about 8 to 16 passengers in executive cabin configurations, prioritizing comfort and amenities over maximum seating density.
| Spec | AIRBUS H225 | Dassault Falcon 8X |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 17 |
| Flight Rules | IFR | — |
| Manufacturer | Airbus Helicopters | Dassault Falcon |
| Aircraft Name | H225 | 8X |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 |
| Max Cabin Seats | 28 | 16 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 36900 |
| Standard Cabin Seats | 19 | 14 |
| Direct Operating Cost | $ 2,963 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 |
| Cabin | ||
| Cockpit | 2 | 3 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 17 |
| Max Cabin Seats | 28 | 16 |
| Standard Cabin Seats | 19 | 14 |
| Lavatory | — | 2 Enclosed Flushing |
| Crew Rest | — | No |
| Jump Seat | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | FWD / AFT |
| Cabin Pressure (psi) | — | 10.2 |
| Galley / Refreshment | — | Galley |
| SL Cabin Altitude (ft) | — | 29200 |
| Max Cabin Altitude (ft) | — | 3900 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 2A1 | PW307D |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | On-Condition |
| Horsepower | 2100 | — |
| No. of Engines | 2 | 3 |
| Fuel Capacity (gal) | 684 | — |
| Flat Rating | — | ISA + 17 |
| Thrust (lbs) | — | 6722 |
| Dimensions | ||
| Length (ft) | 63.4 | 80.2 |
| Overall Height (ft) | 16.3 | 26.1 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | 1695 |
| Wingspan (ft) | — | 86.3 |
| Cabin Width (ft) | — | 7.7 |
| Cabin Height (ft) | — | 6.2 |
| Cabin Length (ft) | — | 42.7 |
| Cabin Width - Floor (ft) | — | 6.3 |
| Cabin Length - Seating (ft) | — | 29.2 |
| Baggage Volume Int. (cu. ft) | — | 140 |