Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Leonardo Aw189 vs Piper M600 Sls
The Beechcraft King Air 360ER is a pressurized twin‑turboprop business aircraft optimized for regional missions and short or unimproved runways. Its typical range is about 1,500–1,800 nautical miles (depending on payload and reserves), and it generally carries 6–9 passengers in executive layouts. The Dassault Falcon 8X is a long‑range tri‑jet business jet in a higher category, designed for intercontinental travel; it offers roughly 6,400–6,500 nautical miles of range and commonly seats 12–16 passengers, with a significantly larger, quieter cabin and higher cruise speeds. The Agusta/Leonardo AW189 is a medium twin‑engine helicopter, best suited to point‑to‑point access where runways are unavailable (offshore, remote sites, EMS/VIP). Its range is typically around 450–500 nautical miles, and it can carry about 16–19 passengers in high‑density seating (fewer in VIP). The Piper M600 SLS is a single‑engine turboprop personal/business aircraft, smaller and simpler to operate, with around 1,200–1,500 nautical miles of range and seating for up to 6 occupants (typically 4–5 passengers plus pilot).
| 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 | — |