Dassault Falcon 8x vs Leonardo Aw189 vs Piaggio Avanti Evo vs Pilatus Pc 24
The Dassault Falcon 8X is a long‑range, large‑cabin tri‑jet business aircraft suited to intercontinental missions. It typically carries about 12–16 passengers and offers roughly 5,900–6,400 nm of range depending on configuration, emphasizing comfort, speed, and nonstop global city pairs. The Leonardo (Agusta) AW189 is a twin‑engine medium helicopter designed for offshore, SAR, and utility/VIP roles rather than high‑altitude cruise. Passenger capacity is commonly around 16–19 in transport layouts, but range is much shorter than fixed‑wing options, roughly 400–500 nm (mission‑dependent), with the advantage of vertical access. The Piaggio Avanti EVO is a high‑speed turboprop business aircraft positioned for efficient regional flying. It generally seats about 6–9 passengers with a range around 1,500–1,800 nm, offering jet‑like cruise for shorter sectors. The Pilatus PC‑24 is a light jet optimized for versatility, including operation from shorter or semi‑prepared runways. It typically carries about 6–10 passengers and flies roughly 2,000–2,300 nm, bridging regional flexibility with true jet performance.
| Spec | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | $ 15.57 | — | $ 3.71 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 17 | 21 | 8 | 6 |
| Manufacturer | Dassault Falcon | Leonardo | Piaggio | Pilatus |
| Aircraft Name | 8X | AW189 | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 651 | 1530 | 2076 |
| DOC / nm / Seat | $ 0.64 | $ 0.74 | — | $ 0.62 |
| Max Cabin Seats | 16 | 19 | 7 | 10 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 36900 | — | 3775 | 6680 |
| Standard Cabin Seats | 14 | 19 | 6 | 6 |
| Direct Operating Cost | $ 3,805 | $ 2,413 | — | $ 1,619 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 516 | 155 | 400 | 440 |
| Base Aircraft Price (USD) | $ 62,500,000 | $2,413,000 | $ 7,695,000 | $11,800,000 |
| Flight Rules | — | IFR | IFR | — |
| Cabin | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | — | No | 1 Enclosed Flushing |
| Min Crew | 2 | 1 | 1 | 1 |
| Crew Rest | No | — | — | No |
| Jump Seat | Yes | — | — | No |
| Total Seats | 17 | 21 | 8 | 6 |
| Galley Location | FWD | — | — | FWD |
| Max Cabin Seats | 16 | 19 | 7 | 10 |
| Lavatory Location | FWD / AFT | — | — | FWD |
| Cabin Pressure (psi) | 10.2 | — | 9 | 9.3 |
| Galley / Refreshment | Galley | — | No | Optional Refreshment Center |
| Standard Cabin Seats | 14 | 19 | 6 | 6 |
| SL Cabin Altitude (ft) | 29200 | — | 24000 | 23500 |
| Max Cabin Altitude (ft) | 3900 | — | 6600 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PW307D | CT7-2E1 | PT6A–66B | FJ44-4A-QPM |
| TBO (hrs) | On-Condition | 4000 | 3600 | 5000 |
| Flat Rating | ISA + 17 | — | ISA + 28 | ISA + 23 |
| Thrust (lbs) | 6722 | — | — | 3435 |
| No. of Engines | 3 | 2 | 2 | 2 |
| Fuel Type | — | JetFuel | — | — |
| Horsepower | — | 1983 | 850 | — |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 80.2 | 57.8 | 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 | 16.6 | 13.1 | 17.4 |
| Cabin Volume (cu. ft) | 1695 | 395 | — | — |
| 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 |
| Rotor Diameter (ft) | — | 48 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — | — |
| Aisle Step (ft) | — | — | — | Flat Floor |