Dassault Falcon 8x vs Leonardo Aw189 vs Piper M600 Sls
The Dassault Falcon 8X is a long‑range, large‑cabin business jet designed for intercontinental travel. It typically carries about 12–16 passengers in executive layouts and can fly roughly 6,450 nautical miles, making it suited to nonstop city pairs across oceans with high cruise speed and jet comfort. The Agusta/Leonardo AW189 is a medium twin‑engine helicopter optimized for offshore, SAR, and utility/passenger transport where vertical lift and access to remote sites matter more than cruise efficiency. Depending on configuration it commonly carries around 16–19 passengers, but its range is much shorter than the Falcon 8X—on the order of a few hundred nautical miles (roughly 450–500 nm typical), varying with payload and reserves. The Piper M600 SLS is a single‑engine turboprop aimed at owner‑pilots and short‑to‑medium business trips. It seats up to 6, with a practical range around 1,000–1,400 nautical miles depending on speed/power settings. In summary: Falcon 8X leads decisively in range and speed; AW189 leads in vertical access and mission flexibility; M600 SLS offers efficient, smaller‑capacity point‑to‑point travel.
| 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 | — |