Dassault Falcon 8x vs Embraer Legacy 650 E vs Enstrom 480b vs Sikorsky S 92
The Dassault Falcon 8X and Embraer Legacy 650E are long-range business jets, while the Enstrom 480B and Sikorsky S-92 are helicopters aimed at very different missions. The Falcon 8X is an ultra-long-range tri-jet designed for intercontinental travel, with roughly 6,450 nm range and typically seating about 12–16 passengers. The Legacy 650E is a large-cabin, long-range twin-jet with around 3,900 nm range and usually carries about 13 passengers, prioritizing cabin comfort on transcontinental routes rather than true global legs. The Enstrom 480B is a light single-engine piston helicopter used for training, utility, and short hops; its range is on the order of a few hundred nautical miles (roughly 200–300 nm) and it generally seats up to 5. The Sikorsky S-92 is a heavy twin-engine helicopter for offshore transport and SAR, offering several hundred nautical miles of range (about 500+ nm depending on fit) and commonly carries around 19 passengers.
| Spec | Dassault Falcon 8X | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 7.66 | $ 19.79 |
| Min Crew | 2 | 2 |
| Total Seats | 17 | 21 |
| Manufacturer | Dassault Falcon | Sikorsky |
| Aircraft Name | 8X | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 439 |
| DOC / nm / Seat | $ 0.64 | $ 0.94 |
| Max Cabin Seats | 16 | 19 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | 7417 |
| Standard Cabin Seats | 14 | 19 |
| Direct Operating Cost | $ 3,805 | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | EFIS |
| Max Cruise Speed (ktas) | 516 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $30,650,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 3 | 2 |
| Lavatory | 2 Enclosed Flushing | — |
| Min Crew | 2 | 2 |
| Crew Rest | No | — |
| Jump Seat | Yes | — |
| Total Seats | 17 | 21 |
| Galley Location | FWD | — |
| Max Cabin Seats | 16 | 19 |
| Lavatory Location | FWD / AFT | — |
| Cabin Pressure (psi) | 10.2 | — |
| Galley / Refreshment | Galley | — |
| Standard Cabin Seats | 14 | 19 |
| SL Cabin Altitude (ft) | 29200 | — |
| Max Cabin Altitude (ft) | 3900 | — |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PW307D | CT7-8A |
| TBO (hrs) | On-Condition | 4000 |
| Flat Rating | ISA + 17 | — |
| Thrust (lbs) | 6722 | — |
| No. of Engines | 3 | 1 |
| Fuel Type | — | JetFuel |
| Horsepower | — | 2520 |
| Fuel Capacity (gal) | — | 760 |
| Dimensions | ||
| Length (ft) | 80.2 | — |
| Wingspan (ft) | 86.3 | — |
| Cabin Width (ft) | 7.7 | — |
| Cabin Height (ft) | 6.2 | — |
| Cabin Length (ft) | 42.7 | — |
| Overall Height (ft) | 26.1 | 17.8 |
| Cabin Volume (cu. ft) | 1695 | 775 |
| Cabin Width - Floor (ft) | 6.3 | — |
| Cabin Length - Seating (ft) | 29.2 | — |
| Baggage Volume Int. (cu. ft) | 140 | — |
| Baggage Volume Ext. (cu. ft) | — | 140 |