Beechcraft King Air 360 Er vs Dassault Falcon 8x vs Pilatus Pc 24 vs Piper M600 Sls
The Beechcraft King Air 360ER is a twin‑turboprop in the utility/business turboprop category, optimized for regional missions and shorter-field flexibility, with a typical range around 1,500–1,800 nm and usually seating about 6–9 passengers depending on layout. The Dassault Falcon 8X is a long‑range, large‑cabin tri‑jet business aircraft aimed at intercontinental travel, offering roughly 6,000+ nm range and commonly configured for about 12–16 passengers. The Pilatus PC‑24 is a light jet with strong short/rough‑field capability and a versatile cabin, generally providing about 2,000 nm range and typically carrying around 6–10 passengers. The Piper M600 SLS is a single‑engine turboprop positioned as a high‑performance personal/owner‑pilot aircraft, with a typical range near 1,400–1,600 nm and seating commonly 4–6 passengers (up to 6 total seats). Overall, the Falcon 8X leads on range and cabin size, the PC‑24 balances jet speed with operational flexibility, the King Air emphasizes turboprop efficiency and access, and the M600 focuses on simpler, lower‑capacity personal travel.
| Spec | Dassault Falcon 8X | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | $ 3.71 | $ 2.19 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 17 | 6 | 6 |
| Manufacturer | Dassault Falcon | Pilatus | Piper |
| Aircraft Name | 8X | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 2076 | 1406 |
| DOC / nm / Seat | $ 0.64 | $ 0.62 | $ 0.55 |
| Max Cabin Seats | 16 | 10 | — |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 36900 | 6680 | 2200 |
| Standard Cabin Seats | 14 | 6 | 4 |
| Direct Operating Cost | $ 3,805 | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 516 | 440 | 274 |
| Base Aircraft Price (USD) | $ 62,500,000 | $11,800,000 | $3,081,400 |
| Flight Rules | — | — | IFR |
| Cabin | |||
| Cockpit | 3 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | 1 Enclosed Flushing | No |
| Min Crew | 2 | 1 | 1 |
| Crew Rest | No | No | — |
| Jump Seat | Yes | No | — |
| Total Seats | 17 | 6 | 5 |
| Galley Location | FWD | FWD | MID |
| Max Cabin Seats | 16 | 10 | — |
| Lavatory Location | FWD / AFT | FWD | — |
| Cabin Pressure (psi) | 10.2 | 9.3 | 5.6 |
| Galley / Refreshment | Galley | Optional Refreshment Center | Refreshment Centre |
| Standard Cabin Seats | 14 | 6 | 4 |
| SL Cabin Altitude (ft) | 29200 | 23500 | 12600 |
| Max Cabin Altitude (ft) | 3900 | — | 8644 |
| Cargo Door | — | Yes | — |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | PW307D | FJ44-4A-QPM | PT6A-42A |
| TBO (hrs) | On-Condition | 5000 | 3600 |
| Flat Rating | ISA + 17 | ISA + 23 | ISA + 55 |
| Thrust (lbs) | 6722 | 3435 | — |
| No. of Engines | 3 | 2 | 1 |
| Horsepower | — | — | 600 |
| Fuel Capacity (gal) | — | — | 260 |
| Dimensions | |||
| Length (ft) | 80.2 | 52.2 | 29.7 |
| Wingspan (ft) | 86.3 | 55.8 | 43.2 |
| Cabin Width (ft) | 7.7 | 5.6 | 4.1 |
| Cabin Height (ft) | 6.2 | 5.1 | 4 |
| Cabin Length (ft) | 42.7 | 23 | 12.3 |
| Overall Height (ft) | 26.1 | 17.4 | 11.3 |
| Cabin Volume (cu. ft) | 1695 | — | 165 |
| Cabin Width - Floor (ft) | 6.3 | 3.8 | — |
| Cabin Length - Seating (ft) | 29.2 | 17 | — |
| Baggage Volume Int. (cu. ft) | 140 | 90 | 20 |
| Aisle Step (ft) | — | Flat Floor | — |