Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Embraer Legacy 650 E vs Piaggio Avanti Evo
The Beechcraft King Air 360ER is a twin‑turboprop positioned as a rugged, short‑runway business/utility aircraft. It typically carries about 6–9 passengers and offers long turboprop legs, roughly around 1,800–2,000 nautical miles depending on load and conditions. The Piaggio Avanti EVO is also a twin‑turboprop, but optimized for speed and efficiency in a business role; it commonly seats about 6–8 passengers with a typical range around 1,500–1,800 nautical miles. The Embraer Legacy 650E is a large‑cabin business jet designed for comfort and baggage capacity, usually configured for about 12–14 passengers, with transcontinental range of roughly 3,900 nautical miles. The Dassault Falcon 8X is an ultra‑long‑range, large‑cabin tri‑jet focused on intercontinental missions; it typically seats about 12–16 passengers and reaches roughly 6,450 nautical miles, enabling nonstop city pairs that the others generally cannot.
| Spec | Dassault Falcon 8X | Piaggio Avanti EVO |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 7.66 | — |
| Min Crew | 2 | 1 |
| Total Seats | 17 | 8 |
| Manufacturer | Dassault Falcon | Piaggio |
| Aircraft Name | 8X | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 1530 |
| DOC / nm / Seat | $ 0.64 | — |
| Max Cabin Seats | 16 | 7 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | 3775 |
| Standard Cabin Seats | 14 | 6 |
| Direct Operating Cost | $ 3,805 | — |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 516 | 400 |
| Base Aircraft Price (USD) | $ 62,500,000 | $ 7,695,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 3 | 2 |
| Lavatory | 2 Enclosed Flushing | No |
| Min Crew | 2 | 1 |
| Crew Rest | No | — |
| Jump Seat | Yes | — |
| Total Seats | 17 | 8 |
| Galley Location | FWD | — |
| Max Cabin Seats | 16 | 7 |
| Lavatory Location | FWD / AFT | — |
| Cabin Pressure (psi) | 10.2 | 9 |
| Galley / Refreshment | Galley | No |
| Standard Cabin Seats | 14 | 6 |
| SL Cabin Altitude (ft) | 29200 | 24000 |
| Max Cabin Altitude (ft) | 3900 | 6600 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PW307D | PT6A–66B |
| TBO (hrs) | On-Condition | 3600 |
| Flat Rating | ISA + 17 | ISA + 28 |
| Thrust (lbs) | 6722 | — |
| No. of Engines | 3 | 2 |
| Horsepower | — | 850 |
| Fuel Burn (gph) | — | 100 |
| Dimensions | ||
| Length (ft) | 80.2 | 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 | 13.1 |
| Cabin Volume (cu. ft) | 1695 | — |
| Cabin Width - Floor (ft) | 6.3 | 3.5 |
| Cabin Length - Seating (ft) | 29.2 | — |
| Baggage Volume Int. (cu. ft) | 140 | 35.2 |