Dassault Falcon 8x vs Gulfstream G700 vs Pilatus Pc 24 vs Sikorsky S 92
The Dassault Falcon 8X and Gulfstream G700 are ultra‑long‑range business jets designed for intercontinental travel. The Falcon 8X typically offers about 6,450 nm of range and usually seats around 12–16 passengers in executive layouts, emphasizing efficiency and flexible cabin zoning. The Gulfstream G700 is in the same category but generally larger, with roughly 7,500 nm range and commonly accommodates about 13–19 passengers, prioritizing maximum cabin volume and long nonstop missions. The Pilatus PC‑24 is a light/medium “super versatile” business jet aimed at shorter regional missions and access to shorter or less‑improved runways. Its range is about 2,000 nm (mission dependent) and seating is typically around 6–10 passengers, sometimes more in high‑density configurations. The Sikorsky S‑92 is a medium helicopter used for offshore, SAR, and VIP transport. Its range is roughly 500–600 nm (configuration dependent) and it commonly carries about 12–19 passengers, trading speed and range for vertical‑lift access and point‑to‑point flexibility.
| Spec | Dassault Falcon 8X | Gulfstream G700 | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| DOC / nm | $ 7.66 | — | $ 3.71 | $ 19.79 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 17 | 16 | 6 | 21 |
| Manufacturer | Dassault Falcon | Gulfstream | Pilatus | Sikorsky |
| Aircraft Name | 8X | G700 | PC-24 | S-92 |
| Certification | FAA / EASA | In Development | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 7500 | 2076 | 439 |
| DOC / nm / Seat | $ 0.64 | — | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 16 | 19 | 10 | 19 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | — | 6680 | 7417 |
| Standard Cabin Seats | 14 | 12 | 6 | 19 |
| Direct Operating Cost | $ 3,805 | — | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 516 | 516 | 440 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $78,000,000 | $11,800,000 | $30,650,000 |
| Flight Rules | — | — | — | IFR |
| Cabin | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | — | 1 Enclosed Flushing | — |
| Min Crew | 2 | 4 | 1 | 2 |
| Crew Rest | No | Optional | No | — |
| Jump Seat | Yes | Yes | No | — |
| Total Seats | 17 | 16 | 6 | 21 |
| Galley Location | FWD | FWD | FWD | — |
| Max Cabin Seats | 16 | 19 | 10 | 19 |
| Lavatory Location | FWD / AFT | FWD / AFT | FWD | — |
| Cabin Pressure (psi) | 10.2 | — | 9.3 | — |
| Galley / Refreshment | Galley | — | Optional Refreshment Center | — |
| Standard Cabin Seats | 14 | 12 | 6 | 19 |
| SL Cabin Altitude (ft) | 29200 | — | 23500 | — |
| Max Cabin Altitude (ft) | 3900 | — | — | — |
| Cargo Door | — | — | Yes | — |
| Engine | ||||
| FADEC | Yes | — | Yes | Yes |
| Model | PW307D | Pearl 700 | FJ44-4A-QPM | CT7-8A |
| TBO (hrs) | On-Condition | On Condition | 5000 | 4000 |
| Flat Rating | ISA + 17 | — | ISA + 23 | — |
| Thrust (lbs) | 6722 | 18250 | 3435 | — |
| No. of Engines | 3 | 2 | 2 | 1 |
| Fuel Type | — | — | — | JetFuel |
| Horsepower | — | — | — | 2520 |
| Fuel Capacity (gal) | — | — | — | 760 |
| Dimensions | ||||
| Length (ft) | 80.2 | 109.9 | 52.2 | — |
| Wingspan (ft) | 86.3 | 103 | 55.8 | — |
| Cabin Width (ft) | 7.7 | 8.2 | 5.6 | — |
| Cabin Height (ft) | 6.2 | 6.25 | 5.1 | — |
| Cabin Length (ft) | 42.7 | 56.9 | 23 | — |
| Overall Height (ft) | 26.1 | 25.4 | 17.4 | 17.8 |
| Cabin Volume (cu. ft) | 1695 | — | — | 775 |
| Cabin Width - Floor (ft) | 6.3 | — | 3.8 | — |
| Cabin Length - Seating (ft) | 29.2 | — | 17 | — |
| Baggage Volume Int. (cu. ft) | 140 | 195 | 90 | — |
| Aisle Step (ft) | — | Flat Floor | Flat Floor | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |