Dassault Falcon 8x vs Piaggio Avanti Evo vs Piper M600 Sls vs Sikorsky S 92
The Dassault Falcon 8X is a long-range large-cabin business jet, typically configured for about 12–16 passengers, and is designed for intercontinental missions with a range around 6,450 nautical miles. The Piaggio Avanti EVO is a high-speed twin‑turboprop business aircraft in the light/midsize cabin class, commonly seating about 6–9 passengers, with a range roughly in the 1,700–1,900 nautical mile class depending on payload and reserves. The Piper M600 SLS is a single‑engine turboprop personal/business aircraft, usually carrying about 4–6 passengers plus a pilot, and is optimized for regional trips with a range around 1,400 nautical miles. The Sikorsky S‑92 is a medium twin‑engine helicopter primarily used for offshore transport and utility/VIP roles; it commonly carries about 12–19 passengers in transport layouts (VIP configurations vary) and has a helicopter-typical range generally around 500–600 nautical miles. Overall, the Falcon 8X leads on range and cabin volume, the Avanti EVO balances speed and efficiency for midrange travel, the M600 SLS targets owner-flown regional capability, and the S‑92 trades range for vertical-lift access and mission flexibility.
| Spec | Dassault Falcon 8X | Piaggio Avanti EVO | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | — | $ 2.19 | $ 19.79 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 17 | 8 | 6 | 21 |
| Manufacturer | Dassault Falcon | Piaggio | Piper | Sikorsky |
| Aircraft Name | 8X | Avanti EVO | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 1530 | 1406 | 439 |
| DOC / nm / Seat | $ 0.64 | — | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 16 | 7 | — | 19 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | 3775 | 2200 | 7417 |
| Standard Cabin Seats | 14 | 6 | 4 | 19 |
| Direct Operating Cost | $ 3,805 | — | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 516 | 400 | 274 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $ 7,695,000 | $3,081,400 | $30,650,000 |
| Flight Rules | — | IFR | IFR | IFR |
| Cabin | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | No | No | — |
| Min Crew | 2 | 1 | 1 | 2 |
| Crew Rest | No | — | — | — |
| Jump Seat | Yes | — | — | — |
| Total Seats | 17 | 8 | 5 | 21 |
| Galley Location | FWD | — | MID | — |
| Max Cabin Seats | 16 | 7 | — | 19 |
| Lavatory Location | FWD / AFT | — | — | — |
| Cabin Pressure (psi) | 10.2 | 9 | 5.6 | — |
| Galley / Refreshment | Galley | No | Refreshment Centre | — |
| Standard Cabin Seats | 14 | 6 | 4 | 19 |
| SL Cabin Altitude (ft) | 29200 | 24000 | 12600 | — |
| Max Cabin Altitude (ft) | 3900 | 6600 | 8644 | — |
| Engine | ||||
| FADEC | Yes | Yes | No | Yes |
| Model | PW307D | PT6A–66B | PT6A-42A | CT7-8A |
| TBO (hrs) | On-Condition | 3600 | 3600 | 4000 |
| Flat Rating | ISA + 17 | ISA + 28 | ISA + 55 | — |
| Thrust (lbs) | 6722 | — | — | — |
| No. of Engines | 3 | 2 | 1 | 1 |
| Horsepower | — | 850 | 600 | 2520 |
| Fuel Burn (gph) | — | 100 | — | — |
| Fuel Capacity (gal) | — | — | 260 | 760 |
| Fuel Type | — | — | — | JetFuel |
| Dimensions | ||||
| Length (ft) | 80.2 | 47.3 | 29.7 | — |
| Wingspan (ft) | 86.3 | 47.1 | 43.2 | — |
| Cabin Width (ft) | 7.7 | 6.1 | 4.1 | — |
| Cabin Height (ft) | 6.2 | 5.8 | 4 | — |
| Cabin Length (ft) | 42.7 | 14.9 | 12.3 | — |
| Overall Height (ft) | 26.1 | 13.1 | 11.3 | 17.8 |
| Cabin Volume (cu. ft) | 1695 | — | 165 | 775 |
| Cabin Width - Floor (ft) | 6.3 | 3.5 | — | — |
| Cabin Length - Seating (ft) | 29.2 | — | — | — |
| Baggage Volume Int. (cu. ft) | 140 | 35.2 | 20 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |