Dassault Falcon 8x vs Embraer Legacy 650 E vs Piper M600 Sls vs Sikorsky S 92
The Dassault Falcon 8X and Embraer Legacy 650E are long-range business jets, while the Piper M600 SLS is a single‑engine turboprop personal aircraft and the Sikorsky S‑92 is a medium/heavy twin‑engine helicopter used for executive transport and offshore missions. In range, the Falcon 8X leads with roughly 6,450 nm, enabling true intercontinental city pairs. The Legacy 650E follows with about 3,900 nm, suitable for transcontinental and many transoceanic routes with fewer payload constraints. The M600 SLS typically offers around 1,400–1,500 nm, optimized for regional trips and access to shorter runways rather than nonstop long-haul. The S‑92’s range is much shorter at roughly 500–600 nm, but it trades that for vertical lift and point‑to‑point access without runways. For passenger capacity, the Falcon 8X and Legacy 650E are commonly configured for about 12–14 passengers, with the Falcon usually offering more cabin flexibility and space. The M600 SLS generally seats up to six, and the S‑92 typically carries around 12–19 depending on configuration.
| Spec | Dassault Falcon 8X | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | $ 2.19 | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 17 | 6 | 21 |
| Manufacturer | Dassault Falcon | Piper | Sikorsky |
| Aircraft Name | 8X | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 1406 | 439 |
| DOC / nm / Seat | $ 0.64 | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 16 | — | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | 2200 | 7417 |
| Standard Cabin Seats | 14 | 4 | 19 |
| Direct Operating Cost | $ 3,805 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 516 | 274 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $3,081,400 | $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 | 5 | 21 |
| Galley Location | FWD | MID | — |
| Max Cabin Seats | 16 | — | 19 |
| Lavatory Location | FWD / AFT | — | — |
| Cabin Pressure (psi) | 10.2 | 5.6 | — |
| Galley / Refreshment | Galley | Refreshment Centre | — |
| Standard Cabin Seats | 14 | 4 | 19 |
| SL Cabin Altitude (ft) | 29200 | 12600 | — |
| Max Cabin Altitude (ft) | 3900 | 8644 | — |
| Engine | |||
| FADEC | Yes | No | Yes |
| Model | PW307D | PT6A-42A | CT7-8A |
| TBO (hrs) | On-Condition | 3600 | 4000 |
| Flat Rating | ISA + 17 | ISA + 55 | — |
| Thrust (lbs) | 6722 | — | — |
| No. of Engines | 3 | 1 | 1 |
| Horsepower | — | 600 | 2520 |
| Fuel Capacity (gal) | — | 260 | 760 |
| Fuel Type | — | — | JetFuel |
| Dimensions | |||
| Length (ft) | 80.2 | 29.7 | — |
| Wingspan (ft) | 86.3 | 43.2 | — |
| Cabin Width (ft) | 7.7 | 4.1 | — |
| Cabin Height (ft) | 6.2 | 4 | — |
| Cabin Length (ft) | 42.7 | 12.3 | — |
| Overall Height (ft) | 26.1 | 11.3 | 17.8 |
| Cabin Volume (cu. ft) | 1695 | 165 | 775 |
| Cabin Width - Floor (ft) | 6.3 | — | — |
| Cabin Length - Seating (ft) | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | 140 | 20 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |