Dassault Falcon 8x vs Leonardo Aw189
The Dassault Falcon 8X and the Agusta/Leonardo AW189 serve very different missions. The Falcon 8X is a long‑range, three‑engine business jet designed for high‑speed, high‑altitude intercity and intercontinental travel from conventional runways, emphasizing cabin comfort and efficiency over long distances. The AW189 is a twin‑engine medium helicopter built for vertical lift operations, such as offshore transport, search and rescue, and access to remote or confined sites where runways are unavailable. In range terms, the Falcon 8X typically offers intercontinental capability at roughly 6,000+ nautical miles depending on conditions and payload, enabling nonstop flights such as North America to Europe. The AW189’s range is much shorter, commonly in the few‑hundred‑nautical‑mile class (often around 450–500 nautical miles with reserves, depending on configuration), optimized for regional legs rather than long-haul travel. Passenger capacity also differs: the Falcon 8X is usually configured for about 12 to 16 passengers in an executive layout, while the AW189 can carry more people in a high‑density transport setup, commonly up to around 16 to 19 passengers depending on layout and mission equipment.
| Spec | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 7.66 | $ 15.57 |
| Min Crew | 2 | 1 |
| Total Seats | 17 | 21 |
| Manufacturer | Dassault Falcon | Leonardo |
| Aircraft Name | 8X | AW189 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 651 |
| DOC / nm / Seat | $ 0.64 | $ 0.74 |
| Max Cabin Seats | 16 | 19 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | — |
| Standard Cabin Seats | 14 | 19 |
| Direct Operating Cost | $ 3,805 | $ 2,413 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | EFIS |
| Max Cruise Speed (ktas) | 516 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $2,413,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 3 | 2 |
| Lavatory | 2 Enclosed Flushing | — |
| Min Crew | 2 | 1 |
| Crew Rest | No | — |
| Jump Seat | Yes | — |
| Total Seats | 17 | 21 |
| Galley Location | FWD | — |
| Max Cabin Seats | 16 | 19 |
| Lavatory Location | FWD / AFT | — |
| Cabin Pressure (psi) | 10.2 | — |
| Galley / Refreshment | Galley | — |
| Standard Cabin Seats | 14 | 19 |
| SL Cabin Altitude (ft) | 29200 | — |
| Max Cabin Altitude (ft) | 3900 | — |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PW307D | CT7-2E1 |
| TBO (hrs) | On-Condition | 4000 |
| Flat Rating | ISA + 17 | — |
| Thrust (lbs) | 6722 | — |
| No. of Engines | 3 | 2 |
| Fuel Type | — | JetFuel |
| Horsepower | — | 1983 |
| Dimensions | ||
| Length (ft) | 80.2 | 57.8 |
| Wingspan (ft) | 86.3 | — |
| Cabin Width (ft) | 7.7 | — |
| Cabin Height (ft) | 6.2 | — |
| Cabin Length (ft) | 42.7 | — |
| Overall Height (ft) | 26.1 | 16.6 |
| Cabin Volume (cu. ft) | 1695 | 395 |
| Cabin Width - Floor (ft) | 6.3 | — |
| Cabin Length - Seating (ft) | 29.2 | — |
| Baggage Volume Int. (cu. ft) | 140 | — |
| Rotor Diameter (ft) | — | 48 |
| Baggage Volume Ext. (cu. ft) | — | 85 |