Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Piaggio Avanti Evo vs Piper M600 Sls
The Beechcraft King Air 360ER is a twin‑turboprop in the high‑end utility/business category, optimized for short and unimproved runways and flexible regional missions. It offers roughly 1,500–1,800 nm of range depending on payload and reserves, and typically carries 6–9 passengers in a club layout (with higher-density seating possible). The Dassault Falcon 8X is an ultra‑long‑range tri‑jet business jet aimed at intercontinental travel. It provides about 6,450 nm of range and usually accommodates 12–16 passengers (with maximum certified layouts higher), prioritizing cabin comfort and nonstop city‑pair capability. The Piaggio Avanti EVO is a fast twin‑turboprop business aircraft positioned between turboprops and light jets for speed and efficiency. Range is roughly 1,500–1,800 nm, and typical seating is 6–8 passengers. The Piper M600 SLS is a single‑engine turboprop in the owner‑pilot/entry business segment. Range is about 1,400–1,700 nm, and it generally seats 4–6 passengers (up to 6 including the pilot), emphasizing simplicity and lower operating complexity.
| 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 |