Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Piaggio Avanti Evo vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop business aircraft best suited to regional missions and shorter runways, typically carrying about 6–9 passengers, with long endurance for its class at roughly 1,500–1,800 nautical miles depending on load and reserves. The Dassault Falcon 8X is a long‑range trijet business jet designed for intercontinental travel, usually configured for about 12–16 passengers, with a headline range around 6,450 nautical miles. The Piaggio Avanti EVO is a high‑speed twin‑turboprop positioned between traditional turboprops and light jets, generally seating 6–9 passengers, with typical range around 1,500–1,800 nautical miles. The Sikorsky S‑92 is a medium twin helicopter used for offshore, government, and VIP transport; passenger capacity varies widely by interior, commonly around 12–19 passengers, while range is much shorter than fixed‑wing options, roughly 400–550 nautical miles depending on configuration. Overall, the Falcon 8X leads on range and cabin scale, the King Air 360ER and Avanti EVO balance efficiency with regional reach, and the S‑92 prioritizes vertical lift and access over distance.
| Spec | Dassault Falcon 8X | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | — | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 17 | 8 | 21 |
| Manufacturer | Dassault Falcon | Piaggio | Sikorsky |
| Aircraft Name | 8X | Avanti EVO | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 1530 | 439 |
| DOC / nm / Seat | $ 0.64 | — | $ 0.94 |
| Max Cabin Seats | 16 | 7 | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 36900 | 3775 | 7417 |
| Standard Cabin Seats | 14 | 6 | 19 |
| Direct Operating Cost | $ 3,805 | — | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 516 | 400 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $ 7,695,000 | $30,650,000 |
| Flight Rules | — | IFR | IFR |
| Cabin | |||
| Cockpit | 3 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | No | — |
| Min Crew | 2 | 1 | 2 |
| Crew Rest | No | — | — |
| Jump Seat | Yes | — | — |
| Total Seats | 17 | 8 | 21 |
| Galley Location | FWD | — | — |
| Max Cabin Seats | 16 | 7 | 19 |
| Lavatory Location | FWD / AFT | — | — |
| Cabin Pressure (psi) | 10.2 | 9 | — |
| Galley / Refreshment | Galley | No | — |
| Standard Cabin Seats | 14 | 6 | 19 |
| SL Cabin Altitude (ft) | 29200 | 24000 | — |
| Max Cabin Altitude (ft) | 3900 | 6600 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PW307D | PT6A–66B | CT7-8A |
| TBO (hrs) | On-Condition | 3600 | 4000 |
| Flat Rating | ISA + 17 | ISA + 28 | — |
| Thrust (lbs) | 6722 | — | — |
| No. of Engines | 3 | 2 | 1 |
| Horsepower | — | 850 | 2520 |
| Fuel Burn (gph) | — | 100 | — |
| Fuel Type | — | — | JetFuel |
| Fuel Capacity (gal) | — | — | 760 |
| 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 | 17.8 |
| Cabin Volume (cu. ft) | 1695 | — | 775 |
| Cabin Width - Floor (ft) | 6.3 | 3.5 | — |
| Cabin Length - Seating (ft) | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | 140 | 35.2 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |