Dassault Falcon 8x vs Leonardo Aw189 vs Piaggio Avanti Evo
The Dassault Falcon 8X is a long‑range, large‑cabin business jet designed primarily for intercontinental travel. It typically carries about 12–16 passengers in executive layouts and offers roughly 6,400 nautical miles of range, making it suited to nonstop missions such as North America to Europe or deep transoceanic repositioning. The Leonardo (Agusta) AW189 is a super‑medium twin‑engine helicopter built for offshore transport, utility, and VIP roles where vertical lift and access to remote sites matter more than cruise efficiency. Passenger capacity varies by configuration, commonly around 16–19 seats, with a practical range on the order of 450–500 nautical miles (mission dependent), favoring regional legs and point-to-platform or point-to-site operations. The Piaggio Avanti EVO is a high‑speed turboprop business aircraft positioned between light jets and midsize turboprops. It generally seats about 7–9 passengers and delivers approximately 1,400–1,800 nautical miles of range, optimized for fast regional trips with good short‑field flexibility and lower operating costs than many jets.
| Spec | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | $ 15.57 | — |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 17 | 21 | 8 |
| Manufacturer | Dassault Falcon | Leonardo | Piaggio |
| Aircraft Name | 8X | AW189 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 651 | 1530 |
| DOC / nm / Seat | $ 0.64 | $ 0.74 | — |
| Max Cabin Seats | 16 | 19 | 7 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 36900 | — | 3775 |
| Standard Cabin Seats | 14 | 19 | 6 |
| Direct Operating Cost | $ 3,805 | $ 2,413 | — |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 516 | 155 | 400 |
| Base Aircraft Price (USD) | $ 62,500,000 | $2,413,000 | $ 7,695,000 |
| Flight Rules | — | IFR | IFR |
| Cabin | |||
| Cockpit | 3 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | — | No |
| Min Crew | 2 | 1 | 1 |
| Crew Rest | No | — | — |
| Jump Seat | Yes | — | — |
| Total Seats | 17 | 21 | 8 |
| Galley Location | FWD | — | — |
| Max Cabin Seats | 16 | 19 | 7 |
| Lavatory Location | FWD / AFT | — | — |
| Cabin Pressure (psi) | 10.2 | — | 9 |
| Galley / Refreshment | Galley | — | No |
| Standard Cabin Seats | 14 | 19 | 6 |
| SL Cabin Altitude (ft) | 29200 | — | 24000 |
| Max Cabin Altitude (ft) | 3900 | — | 6600 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PW307D | CT7-2E1 | PT6A–66B |
| TBO (hrs) | On-Condition | 4000 | 3600 |
| Flat Rating | ISA + 17 | — | ISA + 28 |
| Thrust (lbs) | 6722 | — | — |
| No. of Engines | 3 | 2 | 2 |
| Fuel Type | — | JetFuel | — |
| Horsepower | — | 1983 | 850 |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 80.2 | 57.8 | 47.3 |
| Wingspan (ft) | 86.3 | — | 47.1 |
| Cabin Width (ft) | 7.7 | — | 6.1 |
| Cabin Height (ft) | 6.2 | — | 5.8 |
| Cabin Length (ft) | 42.7 | — | 14.9 |
| Overall Height (ft) | 26.1 | 16.6 | 13.1 |
| Cabin Volume (cu. ft) | 1695 | 395 | — |
| Cabin Width - Floor (ft) | 6.3 | — | 3.5 |
| Cabin Length - Seating (ft) | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | 140 | — | 35.2 |
| Rotor Diameter (ft) | — | 48 | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — |