Dassault Falcon 8x vs Piper M600 Sls vs Robinson R66 vs Sikorsky S 92
The Dassault Falcon 8X is a long‑range, large‑cabin business jet designed for intercontinental travel, offering roughly 3,500–4,000+ nautical miles of range and typically carrying about 12–16 passengers in executive seating. The Piper M600 SLS is a single‑engine turboprop aimed at owner‑pilots and shorter regional trips, with about 1,200–1,500 nautical miles of range and usually seating up to 5–6 people. The Robinson R66 is a light turbine helicopter suited to local and short cross‑country missions, with roughly 300–350 nautical miles of range and a typical capacity of 4–5 people including the pilot. The Sikorsky S‑92 is a medium/heavy twin‑engine helicopter built for offshore transport, SAR, and utility work, offering about 500–600 nautical miles of range and commonly configured for around 12–19 passengers depending on mission and interior. Overall, the 8X leads on range and cabin comfort, the M600 balances speed and simplicity, the R66 prioritizes low‑capacity rotorcraft flexibility, and the S‑92 maximizes helicopter payload and mission capability.
| 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 |