Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Leonardo Aw189 vs Piaggio Avanti Evo
The Beechcraft King Air 360ER is a pressurized twin‑turboprop business aircraft optimized for regional missions and short or unimproved runways, offering roughly 1,800–2,000 nm of range and typically seating about 6–9 passengers in executive layouts. The Dassault Falcon 8X is a long‑range tri‑jet in the large‑cabin category, built for intercontinental flying, with about 6,400–6,450 nm of range and common configurations around 12–16 passengers (with higher-density layouts possible). The Agusta/Leonardo AW189 is a medium twin helicopter aimed at offshore, SAR, and VIP transport; its range is generally around 450–500 nm depending on payload and reserves, and it typically carries about 12–16 passengers (higher in utility seating). The Piaggio Avanti EVO is a high‑speed twin‑turboprop business aircraft bridging turboprop efficiency with near light‑jet cruise speeds, with roughly 1,700–1,900 nm of range and typically 6–9 passengers. Overall, the Falcon 8X leads decisively on range and cabin size, the King Air and Avanti emphasize efficient short-to-mid range access, and the AW189 trades speed and range for vertical-lift capability.
| 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 | — |