Dassault Falcon 8x vs Embraer Legacy 650 E vs Piaggio Avanti Evo vs Sikorsky S 92
The Dassault Falcon 8X is a long‑range ultra‑long‑haul business jet, typically carrying about 12–16 passengers with intercontinental range of roughly 6,400 nautical miles. The Embraer Legacy 650E is a large‑cabin long‑range business jet, usually configured for around 13 passengers, with a range of about 3,900–4,000 nautical miles, making it well suited to transcontinental missions but shorter than the 8X. The Piaggio Avanti EVO is a high‑speed twin‑turboprop business aircraft, generally seating 6–8 passengers, with a range around 1,700–1,800 nautical miles, optimized for efficient regional flying and access to shorter runways. The Sikorsky S‑92 is a large twin‑engine helicopter used for offshore, VIP, and utility missions; passenger capacity commonly falls around 12–19 depending on configuration, with typical range roughly 500–600 nautical miles. Overall, the Falcon 8X leads on range, the Legacy 650E balances cabin size and reach, the Avanti EVO emphasizes efficiency on shorter routes, and the S‑92 trades speed and range for vertical lift and operational flexibility.
| 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 |