Airbus Helicopters H225 vs Dassault Falcon 8x vs Embraer Legacy 650 E vs Enstrom 480b
The Airbus H225 and Enstrom 480B are helicopters, while the Dassault Falcon 8X and Embraer Legacy 650E are long‑range business jets, so their categories and performance priorities differ sharply. The H225 is a heavy twin‑engine helicopter optimized for offshore and utility transport; it typically carries around 19 passengers in high‑density seating (fewer in VIP layouts) and has a practical range on the order of roughly 500–600 nautical miles depending on mission profile. The Enstrom 480B is a light piston helicopter, generally configured for about 4–5 occupants including the pilot, with a range typically around 200–300 nautical miles. The Falcon 8X is an ultra‑long‑range trijet business jet, usually seating about 12–16 passengers, with intercontinental range around 6,400 nautical miles. The Legacy 650E is a large‑cabin long‑range business jet, commonly configured for about 13 passengers, with range roughly 3,900 nautical miles. In short, the jets dominate range and comfort for point‑to‑point travel, while the helicopters trade speed and range for vertical access and mission flexibility.
| 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 |