Dassault Falcon 8x vs Piper M600 Sls vs Sikorsky S 92
The Dassault Falcon 8X is a long-range, large-cabin business jet designed for intercontinental travel. It typically carries about 8 to 14 passengers depending on cabin configuration, and its range is roughly 6,400 nautical miles, enabling nonstop missions such as North America to Europe or deep transoceanic legs. The Piper M600 SLS is a single-engine turboprop aimed at owner-operators and shorter regional trips. It generally seats one pilot plus up to five passengers (about 6 total seats), and its range is about 1,400 nautical miles, favoring flexible access to smaller airports at lower operating cost than jets. The Sikorsky S-92 is a medium-lift twin-engine helicopter used for offshore transport, search-and-rescue, and executive/VIP missions. Passenger capacity is commonly around 19 in a typical transport layout (fewer in VIP configurations), while practical range is roughly 500 nautical miles, trading speed and distance for vertical lift, hover capability, and point-to-point access without runways.
| 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 |