Dassault Falcon 8x vs Enstrom 480b 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 (with higher-density layouts possible) and offers roughly 6,400 nm of range, making it the clear leader for nonstop global missions. The Piper M600 SLS is a single‑engine turboprop personal/business aircraft in a much lighter category; it usually seats 5–6 passengers and has about 1,400–1,600 nm of range, optimized for efficient regional trips rather than transoceanic legs. The Leonardo (Agusta) AW189 is a medium twin‑engine helicopter aimed at offshore, SAR, and utility/VIP roles; passenger capacity is commonly around 16–19, with practical range generally in the ~400–500 nm class depending on configuration and reserves, trading speed and distance for vertical lift capability. The Enstrom 480B is a light single‑engine helicopter focused on training, patrol, and local utility; it typically seats 4–5 and has a shorter range, roughly ~300–400 nm, best suited to short‑haul missions where landing flexibility matters more than distance.
| 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 | — |