Dassault Falcon 8x vs Embraer Legacy 650 E vs Leonardo Aw189 vs Piaggio Avanti Evo
The Dassault Falcon 8X and Embraer Legacy 650E are long-range business jets, while the Piaggio Avanti EVO is a fast turboprop business aircraft and the Agusta/Leonardo AW189 is a long-range, super‑medium helicopter oriented to offshore and utility/VIP missions. In range, the Falcon 8X leads by a wide margin at roughly 6,450 nm, enabling true intercontinental city pairs. The Legacy 650E follows at about 3,900 nm, suited to transcontinental missions with more routing flexibility than most midsize jets. The Avanti EVO typically offers around 1,700–1,800 nm, optimized for shorter regional legs with jet-like cruise speeds for a turboprop. The AW189’s range is mission-dependent but is commonly on the order of ~450–500 nm, trading distance for vertical lift and access to remote sites. For passenger capacity, the Falcon 8X and Legacy 650E usually seat about 12–14 passengers in executive layouts. The Avanti EVO typically carries around 7–9 passengers. The AW189 can be configured for VIP seating, but in transport roles it can carry up to about 16–19 passengers.
| 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 | — |