Dassault Falcon 8x vs Embraer Legacy 650 E vs Leonardo Aw189 vs Piper M600 Sls
The Dassault Falcon 8X and Embraer Legacy 650E are large-cabin business jets, while the Agusta/Leonardo AW189 is a medium twin‑engine helicopter and the Piper M600 SLS is a single‑engine turboprop. In range, the Falcon 8X leads with roughly 6,450 nautical miles, enabling true intercontinental missions. The Legacy 650E follows at about 3,900 nautical miles, well suited to transcontinental flying. The M600 SLS typically offers around 1,400–1,600 nautical miles, aimed at regional to mid-range trips with lower operating complexity. The AW189’s practical range is much shorter, generally a few hundred nautical miles depending on load and reserves, optimized for point-to-point access and offshore or utility roles rather than long-haul travel. For passenger capacity, the Falcon 8X commonly seats about 12–14, and the Legacy 650E about 13 (often up to 14) in executive layouts. The AW189 can carry more in high-density configurations (up to around 16–19), though VIP layouts reduce that. The M600 SLS is the smallest, typically 5–6 passengers.
| Spec | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | $ 15.57 | $ 2.19 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 17 | 21 | 6 |
| Manufacturer | Dassault Falcon | Leonardo | Piper |
| Aircraft Name | 8X | AW189 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 651 | 1406 |
| DOC / nm / Seat | $ 0.64 | $ 0.74 | $ 0.55 |
| Max Cabin Seats | 16 | 19 | — |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 36900 | — | 2200 |
| Standard Cabin Seats | 14 | 19 | 4 |
| Direct Operating Cost | $ 3,805 | $ 2,413 | $ 603 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 516 | 155 | 274 |
| Base Aircraft Price (USD) | $ 62,500,000 | $2,413,000 | $3,081,400 |
| Flight Rules | — | IFR | IFR |
| Cabin | |||
| Cockpit | 3 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | — | No |
| Min Crew | 2 | 1 | 1 |
| Crew Rest | No | — | — |
| Jump Seat | Yes | — | — |
| Total Seats | 17 | 21 | 5 |
| 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 | 19 | 4 |
| SL Cabin Altitude (ft) | 29200 | — | 12600 |
| Max Cabin Altitude (ft) | 3900 | — | 8644 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | PW307D | CT7-2E1 | PT6A-42A |
| TBO (hrs) | On-Condition | 4000 | 3600 |
| Flat Rating | ISA + 17 | — | ISA + 55 |
| Thrust (lbs) | 6722 | — | — |
| No. of Engines | 3 | 2 | 1 |
| Fuel Type | — | JetFuel | — |
| Horsepower | — | 1983 | 600 |
| Fuel Capacity (gal) | — | — | 260 |
| Dimensions | |||
| Length (ft) | 80.2 | 57.8 | 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 | 16.6 | 11.3 |
| Cabin Volume (cu. ft) | 1695 | 395 | 165 |
| Cabin Width - Floor (ft) | 6.3 | — | — |
| Cabin Length - Seating (ft) | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | 140 | — | 20 |
| Rotor Diameter (ft) | — | 48 | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — |