Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Enstrom 480b vs Piaggio Avanti Evo
By category, the Beechcraft King Air 360ER and Piaggio Avanti EVO are twin‑engine turboprops, with the King Air positioned as a utility/corporate turboprop and the Avanti as a high‑speed executive turboprop, while the Dassault Falcon 8X is a long‑range tri‑jet business jet. The Enstrom 480B is a single‑engine piston helicopter, suited to short‑haul utility, training, and light corporate missions rather than airline‑style transport. On range, the Falcon 8X is in a different class, offering intercontinental capability (roughly 6,000+ nautical miles). The King Air 360ER provides long turboprop reach for its segment (about 1,500–1,800 nautical miles depending on mission and reserves). The Avanti EVO is typically similar to or somewhat higher than many turboprops in practical cruise missions (around 1,400–1,700 nautical miles). The Enstrom 480B is far shorter‑range, generally a few hundred nautical miles. For passenger capacity, the Falcon 8X commonly seats around 12–16 in executive layouts, the King Air 360ER about 8–9, the Avanti EVO typically 7–9, and the Enstrom 480B usually carries 4–5 including the pilot.
| 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 |