Dassault Falcon 8x vs Leonardo Aw189 vs Pilatus Pc 24 vs Sikorsky S 92
The Dassault Falcon 8X and Pilatus PC-24 are fixed‑wing business jets, while the Leonardo AW189 and Sikorsky S‑92 are twin‑engine helicopters aimed at offshore, SAR, and utility/VIP missions. In range, the Falcon 8X is the clear leader, typically around 6,450 nautical miles, enabling true intercontinental nonstop flights. The PC‑24 is a “super versatile jet” with a much shorter but still long business‑aviation range, roughly about 2,000 nautical miles depending on payload and conditions. Helicopter ranges are lower: the AW189 is generally in the ~450–500 nautical mile class, and the larger S‑92 is often around ~500 nautical miles (mission equipment and reserves can materially change both). Passenger capacity also separates them: the Falcon 8X commonly seats about 12–14 in executive layout, while the PC‑24 typically carries about 6–10 in a standard business configuration (it can be arranged for more in commuter/medevac roles). The AW189 is usually configured for about 16–19 passengers, and the S‑92 for roughly 19 passengers, with higher-density seating possible for utility missions.
| Spec | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | $ 15.57 | $ 3.71 | $ 19.79 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 17 | 21 | 6 | 21 |
| Manufacturer | Dassault Falcon | Leonardo | Pilatus | Sikorsky |
| Aircraft Name | 8X | AW189 | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 651 | 2076 | 439 |
| DOC / nm / Seat | $ 0.64 | $ 0.74 | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 16 | 19 | 10 | 19 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | — | 6680 | 7417 |
| Standard Cabin Seats | 14 | 19 | 6 | 19 |
| Direct Operating Cost | $ 3,805 | $ 2,413 | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | EFIS | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 516 | 155 | 440 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $2,413,000 | $11,800,000 | $30,650,000 |
| Flight Rules | — | IFR | — | IFR |
| Cabin | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | — | 1 Enclosed Flushing | — |
| Min Crew | 2 | 1 | 1 | 2 |
| Crew Rest | No | — | No | — |
| Jump Seat | Yes | — | No | — |
| Total Seats | 17 | 21 | 6 | 21 |
| Galley Location | FWD | — | FWD | — |
| Max Cabin Seats | 16 | 19 | 10 | 19 |
| Lavatory Location | FWD / AFT | — | FWD | — |
| Cabin Pressure (psi) | 10.2 | — | 9.3 | — |
| Galley / Refreshment | Galley | — | Optional Refreshment Center | — |
| Standard Cabin Seats | 14 | 19 | 6 | 19 |
| SL Cabin Altitude (ft) | 29200 | — | 23500 | — |
| Max Cabin Altitude (ft) | 3900 | — | — | — |
| Cargo Door | — | — | Yes | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PW307D | CT7-2E1 | FJ44-4A-QPM | CT7-8A |
| TBO (hrs) | On-Condition | 4000 | 5000 | 4000 |
| Flat Rating | ISA + 17 | — | ISA + 23 | — |
| Thrust (lbs) | 6722 | — | 3435 | — |
| No. of Engines | 3 | 2 | 2 | 1 |
| Fuel Type | — | JetFuel | — | JetFuel |
| Horsepower | — | 1983 | — | 2520 |
| Fuel Capacity (gal) | — | — | — | 760 |
| Dimensions | ||||
| Length (ft) | 80.2 | 57.8 | 52.2 | — |
| Wingspan (ft) | 86.3 | — | 55.8 | — |
| Cabin Width (ft) | 7.7 | — | 5.6 | — |
| Cabin Height (ft) | 6.2 | — | 5.1 | — |
| Cabin Length (ft) | 42.7 | — | 23 | — |
| Overall Height (ft) | 26.1 | 16.6 | 17.4 | 17.8 |
| Cabin Volume (cu. ft) | 1695 | 395 | — | 775 |
| Cabin Width - Floor (ft) | 6.3 | — | 3.8 | — |
| Cabin Length - Seating (ft) | 29.2 | — | 17 | — |
| Baggage Volume Int. (cu. ft) | 140 | — | 90 | — |
| Rotor Diameter (ft) | — | 48 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — | 140 |
| Aisle Step (ft) | — | — | Flat Floor | — |