Dassault Falcon 8x vs Piaggio Avanti Evo vs Sikorsky S 92
The Dassault Falcon 8X and Piaggio Avanti EVO are fixed‑wing business aircraft, while the Sikorsky S‑92 is a medium twin‑engine helicopter typically used for offshore, executive, and utility missions. In range, the Falcon 8X is the clear long‑haul option, offering intercontinental capability of roughly 6,450 nautical miles, suitable for nonstop transoceanic trips. The Avanti EVO is a shorter‑range turboprop business aircraft at about 1,770 nautical miles, best for regional missions with efficient cruise at lower operating costs than many jets. The S‑92 has the shortest range in this comparison, generally around 540 nautical miles depending on payload and reserves, reflecting helicopter mission profiles rather than point‑to‑point long distance travel. For passenger capacity, the Falcon 8X typically carries around 12–16 passengers in a VIP layout, the Avanti EVO commonly seats about 7–9 passengers, and the S‑92 can be configured for about 19 passengers in a high‑density transport role or fewer in executive layouts.
| 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 |