Dassault Falcon 8x vs Enstrom 480b vs Pilatus Pc 24 vs Piper M600 Sls
The Dassault Falcon 8X is a long-range large-cabin business jet, designed for intercontinental missions; it typically carries about 12–16 passengers and offers roughly 6,000–6,450 nm of range, depending on configuration and reserves. The Pilatus PC-24 is a light “super versatile” business jet aimed at shorter runways and mixed-use operations; it generally seats about 6–10 passengers and reaches around 2,000 nm range. The Piper M600 SLS is a single-engine turboprop personal/business aircraft, optimized for owner-operators; it commonly carries 4–6 passengers (up to 6 seats total) with about 1,400 nm range. The Enstrom 480B is a single-engine turbine helicopter used for utility, training, and short-range transport; it typically carries 4–5 occupants including the pilot and has a range on the order of roughly 300–400 nm. Overall, the Falcon 8X leads on range and cabin size, the PC-24 balances jet speed with operational flexibility, the M600 SLS offers efficient turboprop travel for smaller groups, and the 480B prioritizes vertical-lift access over distance.
| 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 | — |