Dassault Falcon 8x vs Piaggio Avanti Evo vs Pilatus Pc 24 vs Piper M600 Sls
The Dassault Falcon 8X is a long‑range, large‑cabin tri‑jet business jet, typically carrying about 12–16 passengers and optimized for intercontinental missions with roughly 6,400–6,500 nautical miles of range. The Piaggio Avanti EVO is a high‑speed, pressurized twin‑turboprop in the light business category, usually configured for about 6–7 passengers, with transcontinental capability around 1,700–1,800 nautical miles. The Pilatus PC‑24 is a versatile light jet designed for short and unimproved runways, commonly seating about 6–10 passengers depending on layout, with mid‑range performance around 2,000 nautical miles. The Piper M600 SLS is a single‑engine, pressurized turboprop positioned as an owner‑flown personal/business aircraft, typically carrying about 4–6 passengers, with range on the order of 1,400–1,500 nautical miles. Overall, the 8X leads on cabin size and range, the PC‑24 balances jet speed with runway flexibility, the Avanti EVO emphasizes efficient turboprop cruise, and the M600 SLS focuses on simpler single‑engine operation.
| Spec | Dassault Falcon 8X | Piaggio Avanti EVO | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | — | $ 3.71 | $ 2.19 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 17 | 8 | 6 | 6 |
| Manufacturer | Dassault Falcon | Piaggio | Pilatus | Piper |
| Aircraft Name | 8X | Avanti EVO | PC-24 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 1530 | 2076 | 1406 |
| DOC / nm / Seat | $ 0.64 | — | $ 0.62 | $ 0.55 |
| Max Cabin Seats | 16 | 7 | 10 | — |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 36900 | 3775 | 6680 | 2200 |
| Standard Cabin Seats | 14 | 6 | 6 | 4 |
| Direct Operating Cost | $ 3,805 | — | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 516 | 400 | 440 | 274 |
| Base Aircraft Price (USD) | $ 62,500,000 | $ 7,695,000 | $11,800,000 | $3,081,400 |
| Flight Rules | — | IFR | — | IFR |
| Cabin | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | No | 1 Enclosed Flushing | No |
| Min Crew | 2 | 1 | 1 | 1 |
| Crew Rest | No | — | No | — |
| Jump Seat | Yes | — | No | — |
| Total Seats | 17 | 8 | 6 | 5 |
| Galley Location | FWD | — | FWD | MID |
| Max Cabin Seats | 16 | 7 | 10 | — |
| Lavatory Location | FWD / AFT | — | FWD | — |
| Cabin Pressure (psi) | 10.2 | 9 | 9.3 | 5.6 |
| Galley / Refreshment | Galley | No | Optional Refreshment Center | Refreshment Centre |
| Standard Cabin Seats | 14 | 6 | 6 | 4 |
| SL Cabin Altitude (ft) | 29200 | 24000 | 23500 | 12600 |
| Max Cabin Altitude (ft) | 3900 | 6600 | — | 8644 |
| Cargo Door | — | — | Yes | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | PW307D | PT6A–66B | FJ44-4A-QPM | PT6A-42A |
| TBO (hrs) | On-Condition | 3600 | 5000 | 3600 |
| Flat Rating | ISA + 17 | ISA + 28 | ISA + 23 | ISA + 55 |
| Thrust (lbs) | 6722 | — | 3435 | — |
| No. of Engines | 3 | 2 | 2 | 1 |
| Horsepower | — | 850 | — | 600 |
| Fuel Burn (gph) | — | 100 | — | — |
| Fuel Capacity (gal) | — | — | — | 260 |
| Dimensions | ||||
| Length (ft) | 80.2 | 47.3 | 52.2 | 29.7 |
| Wingspan (ft) | 86.3 | 47.1 | 55.8 | 43.2 |
| Cabin Width (ft) | 7.7 | 6.1 | 5.6 | 4.1 |
| Cabin Height (ft) | 6.2 | 5.8 | 5.1 | 4 |
| Cabin Length (ft) | 42.7 | 14.9 | 23 | 12.3 |
| Overall Height (ft) | 26.1 | 13.1 | 17.4 | 11.3 |
| Cabin Volume (cu. ft) | 1695 | — | — | 165 |
| Cabin Width - Floor (ft) | 6.3 | 3.5 | 3.8 | — |
| Cabin Length - Seating (ft) | 29.2 | — | 17 | — |
| Baggage Volume Int. (cu. ft) | 140 | 35.2 | 90 | 20 |
| Aisle Step (ft) | — | — | Flat Floor | — |