Dassault Falcon 8x vs Gulfstream G700 vs Piper M600 Sls vs Sikorsky S 92
The Dassault Falcon 8X and Gulfstream G700 are long-range, large-cabin 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 offshore, VIP, and utility missions. In range, the G700 is generally the longest-legged, capable of roughly about 7,500 nautical miles, with the Falcon 8X close behind at about 6,450 nautical miles, both intended for intercontinental travel. The M600 SLS is in a different class, offering roughly around 1,500 nautical miles, optimized for regional trips and lower operating costs. The S‑92 has the shortest range, typically on the order of a few hundred nautical miles (around 500 nm depending on configuration and reserves), trading speed and distance for vertical lift and access to helipads and remote sites. Passenger capacity also separates them: the G700 and Falcon 8X commonly seat around 12–16 in executive layouts, the M600 SLS typically carries 1 pilot plus up to 5 passengers, and the S‑92 can seat a larger cabin load, often around 12–19 depending on mission fit.
| Spec | Dassault Falcon 8X | Gulfstream G700 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| DOC / nm | $ 7.66 | — | $ 2.19 | $ 19.79 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 17 | 16 | 6 | 21 |
| Manufacturer | Dassault Falcon | Gulfstream | Piper | Sikorsky |
| Aircraft Name | 8X | G700 | M600 | S-92 |
| Certification | FAA / EASA | In Development | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 7500 | 1406 | 439 |
| DOC / nm / Seat | $ 0.64 | — | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 16 | 19 | — | 19 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | — | 2200 | 7417 |
| Standard Cabin Seats | 14 | 12 | 4 | 19 |
| Direct Operating Cost | $ 3,805 | — | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 516 | 516 | 274 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $78,000,000 | $3,081,400 | $30,650,000 |
| Flight Rules | — | — | IFR | IFR |
| Cabin | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | — | No | — |
| Min Crew | 2 | 4 | 1 | 2 |
| Crew Rest | No | Optional | — | — |
| Jump Seat | Yes | Yes | — | — |
| Total Seats | 17 | 16 | 5 | 21 |
| Galley Location | FWD | FWD | MID | — |
| Max Cabin Seats | 16 | 19 | — | 19 |
| Lavatory Location | FWD / AFT | FWD / AFT | — | — |
| Cabin Pressure (psi) | 10.2 | — | 5.6 | — |
| Galley / Refreshment | Galley | — | Refreshment Centre | — |
| Standard Cabin Seats | 14 | 12 | 4 | 19 |
| SL Cabin Altitude (ft) | 29200 | — | 12600 | — |
| Max Cabin Altitude (ft) | 3900 | — | 8644 | — |
| Engine | ||||
| FADEC | Yes | — | No | Yes |
| Model | PW307D | Pearl 700 | PT6A-42A | CT7-8A |
| TBO (hrs) | On-Condition | On Condition | 3600 | 4000 |
| Flat Rating | ISA + 17 | — | ISA + 55 | — |
| Thrust (lbs) | 6722 | 18250 | — | — |
| No. of Engines | 3 | 2 | 1 | 1 |
| Horsepower | — | — | 600 | 2520 |
| Fuel Capacity (gal) | — | — | 260 | 760 |
| Fuel Type | — | — | — | JetFuel |
| Dimensions | ||||
| Length (ft) | 80.2 | 109.9 | 29.7 | — |
| Wingspan (ft) | 86.3 | 103 | 43.2 | — |
| Cabin Width (ft) | 7.7 | 8.2 | 4.1 | — |
| Cabin Height (ft) | 6.2 | 6.25 | 4 | — |
| Cabin Length (ft) | 42.7 | 56.9 | 12.3 | — |
| Overall Height (ft) | 26.1 | 25.4 | 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 | 195 | 20 | — |
| Aisle Step (ft) | — | Flat Floor | — | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |