Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Piaggio Avanti Evo vs Robinson R66
The Beechcraft King Air 360ER is a pressurized twin‑turboprop business aircraft suited to regional and remote operations, offering long endurance for its class (roughly up to 3,000 nautical miles with auxiliary fuel and favorable conditions) and typically seating about 6 to 9 passengers in executive layouts. The Dassault Falcon 8X is a long‑range tri‑jet in the large‑cabin category, designed for intercontinental missions at about 6,400 nautical miles and commonly configured for around 12 to 16 passengers. The Piaggio Avanti EVO is a high‑speed twin‑turboprop in the light business aircraft segment, generally offering about 1,500 to 1,800 nautical miles of range and usually seating 6 to 7 passengers. The Robinson R66 is a light single‑engine turbine helicopter, optimized for short‑range point‑to‑point and vertical access, with typical range around 300 to 350 nautical miles and seating for a pilot plus up to 4 passengers. Overall, the Falcon 8X leads by range and cabin capacity, the King Air 360ER emphasizes versatility and runway flexibility, the Avanti EVO focuses on speed and efficiency in turboprops, and the R66 trades range for VTOL access.
| 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 |