Dassault Falcon 8x vs Piaggio Avanti Evo vs Piper M600 Sls vs Robinson R66
The Dassault Falcon 8X is a long‑range, large‑cabin business jet designed for intercontinental travel, offering roughly 6,450 nautical miles of range and typically seating about 12–16 passengers depending on cabin layout. The Piaggio Avanti EVO is a high‑speed twin‑turboprop business aircraft positioned for efficient regional and mid‑range trips, with about 1,700–1,800 nautical miles of range and usually 6–7 passengers in an executive configuration. The Piper M600 SLS is a single‑engine turboprop aimed at owner‑operators and shorter business hops, with around 1,000–1,500 nautical miles of range (mission dependent) and seating commonly 4–6 passengers. The Robinson R66 is a light single‑engine turbine helicopter optimized for short‑range point‑to‑point access and vertical operations, with roughly 300 nautical miles of range and seating for about 4 passengers plus a pilot. Overall, the 8X leads in range and cabin capacity, the Avanti EVO balances speed and efficiency for regional missions, the M600 SLS prioritizes simplicity and operating economy, and the R66 trades range and speed for landing flexibility.
| Spec | Dassault Falcon 8X | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | — | $ 2.19 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 17 | 8 | 6 |
| Manufacturer | Dassault Falcon | Piaggio | Piper |
| Aircraft Name | 8X | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 1530 | 1406 |
| DOC / nm / Seat | $ 0.64 | — | $ 0.55 |
| Max Cabin Seats | 16 | 7 | — |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 36900 | 3775 | 2200 |
| Standard Cabin Seats | 14 | 6 | 4 |
| Direct Operating Cost | $ 3,805 | — | $ 603 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 516 | 400 | 274 |
| Base Aircraft Price (USD) | $ 62,500,000 | $ 7,695,000 | $3,081,400 |
| Flight Rules | — | IFR | IFR |
| Cabin | |||
| Cockpit | 3 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | No | No |
| Min Crew | 2 | 1 | 1 |
| Crew Rest | No | — | — |
| Jump Seat | Yes | — | — |
| Total Seats | 17 | 8 | 5 |
| Galley Location | FWD | — | MID |
| Max Cabin Seats | 16 | 7 | — |
| Lavatory Location | FWD / AFT | — | — |
| Cabin Pressure (psi) | 10.2 | 9 | 5.6 |
| Galley / Refreshment | Galley | No | Refreshment Centre |
| Standard Cabin Seats | 14 | 6 | 4 |
| SL Cabin Altitude (ft) | 29200 | 24000 | 12600 |
| Max Cabin Altitude (ft) | 3900 | 6600 | 8644 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | PW307D | PT6A–66B | PT6A-42A |
| TBO (hrs) | On-Condition | 3600 | 3600 |
| Flat Rating | ISA + 17 | ISA + 28 | ISA + 55 |
| Thrust (lbs) | 6722 | — | — |
| No. of Engines | 3 | 2 | 1 |
| Horsepower | — | 850 | 600 |
| Fuel Burn (gph) | — | 100 | — |
| Fuel Capacity (gal) | — | — | 260 |
| 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 |
| Cabin Volume (cu. ft) | 1695 | — | 165 |
| Cabin Width - Floor (ft) | 6.3 | 3.5 | — |
| Cabin Length - Seating (ft) | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | 140 | 35.2 | 20 |