Dassault Falcon 8x vs Piaggio Avanti Evo vs Pilatus Pc 24 vs Sikorsky S 92
The Dassault Falcon 8X is a long‑range, large‑cabin business jet designed for intercontinental missions, typically carrying about 12–16 passengers (with higher maximum configurations possible) and offering roughly 6,450 nautical miles of range. The Piaggio Avanti EVO is a high‑speed, pressurized twin‑turboprop best suited to regional to medium trips; it generally seats about 6–9 passengers and has a range around 1,700–1,900 nautical miles depending on conditions and configuration. The Pilatus PC‑24 is a light jet optimized for versatile operations, including shorter and rougher runways than most business jets; it commonly carries about 6–10 passengers and delivers roughly 2,000 nautical miles of range. The Sikorsky S‑92 is a heavy twin‑engine helicopter aimed at offshore, search‑and‑rescue, and VIP transport; it typically carries about 12–19 passengers and has a range on the order of 500–600 nautical miles, varying notably with payload and reserves. Overall, the 8X prioritizes maximum range and cabin comfort, the Avanti EVO and PC‑24 balance speed and flexibility for shorter missions, and the S‑92 trades range for vertical‑lift capability.
| Spec | Dassault Falcon 8X | Piaggio Avanti EVO | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | — | $ 3.71 | $ 19.79 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 17 | 8 | 6 | 21 |
| Manufacturer | Dassault Falcon | Piaggio | Pilatus | Sikorsky |
| Aircraft Name | 8X | Avanti EVO | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 1530 | 2076 | 439 |
| DOC / nm / Seat | $ 0.64 | — | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 16 | 7 | 10 | 19 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | 3775 | 6680 | 7417 |
| Standard Cabin Seats | 14 | 6 | 6 | 19 |
| Direct Operating Cost | $ 3,805 | — | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 516 | 400 | 440 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $ 7,695,000 | $11,800,000 | $30,650,000 |
| Flight Rules | — | IFR | — | IFR |
| Cabin | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | No | 1 Enclosed Flushing | — |
| Min Crew | 2 | 1 | 1 | 2 |
| Crew Rest | No | — | No | — |
| Jump Seat | Yes | — | No | — |
| Total Seats | 17 | 8 | 6 | 21 |
| Galley Location | FWD | — | FWD | — |
| Max Cabin Seats | 16 | 7 | 10 | 19 |
| Lavatory Location | FWD / AFT | — | FWD | — |
| Cabin Pressure (psi) | 10.2 | 9 | 9.3 | — |
| Galley / Refreshment | Galley | No | Optional Refreshment Center | — |
| Standard Cabin Seats | 14 | 6 | 6 | 19 |
| SL Cabin Altitude (ft) | 29200 | 24000 | 23500 | — |
| Max Cabin Altitude (ft) | 3900 | 6600 | — | — |
| Cargo Door | — | — | Yes | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PW307D | PT6A–66B | FJ44-4A-QPM | CT7-8A |
| TBO (hrs) | On-Condition | 3600 | 5000 | 4000 |
| Flat Rating | ISA + 17 | ISA + 28 | ISA + 23 | — |
| Thrust (lbs) | 6722 | — | 3435 | — |
| No. of Engines | 3 | 2 | 2 | 1 |
| Horsepower | — | 850 | — | 2520 |
| Fuel Burn (gph) | — | 100 | — | — |
| Fuel Type | — | — | — | JetFuel |
| Fuel Capacity (gal) | — | — | — | 760 |
| Dimensions | ||||
| Length (ft) | 80.2 | 47.3 | 52.2 | — |
| Wingspan (ft) | 86.3 | 47.1 | 55.8 | — |
| Cabin Width (ft) | 7.7 | 6.1 | 5.6 | — |
| Cabin Height (ft) | 6.2 | 5.8 | 5.1 | — |
| Cabin Length (ft) | 42.7 | 14.9 | 23 | — |
| Overall Height (ft) | 26.1 | 13.1 | 17.4 | 17.8 |
| Cabin Volume (cu. ft) | 1695 | — | — | 775 |
| 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 | — |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |