Dassault Falcon 8x vs Enstrom 480b vs Leonardo Aw189 vs Piaggio Avanti Evo
The Dassault Falcon 8X is a long‑range, large‑cabin business jet designed for intercontinental missions. It typically carries 12–16 passengers in executive layouts (up to about 19) and offers roughly 6,000+ nautical miles of range, making it the clear leader for nonstop, high‑speed travel between distant city pairs. The Piaggio Avanti EVO is a turboprop business aircraft in the light‑to‑midsize executive category. It commonly seats about 6–8 passengers and provides around 1,500–1,800 nautical miles of range, favoring efficient regional and medium‑haul trips with good speed for a turboprop. The Agusta/Leonardo AW189 is a super‑medium twin helicopter primarily aimed at offshore transport, SAR, and utility/VIP roles. Passenger capacity is typically in the mid‑teens depending on configuration, and practical range is on the order of 400–500+ nautical miles, trading speed and range for vertical access and mission flexibility. The Enstrom 480B is a small single‑engine piston helicopter, usually seating up to 5 occupants, with a relatively short range in the few‑hundred‑nautical‑mile class, suited to training, patrol, and short‑hop utility missions.
| 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 | — |