Airbus Helicopters H225 vs Dassault Falcon 8x vs Leonardo Aw189 vs Pilatus Pc 24
The Airbus H225 and Leonardo AW189 are twin‑engine helicopters suited to offshore, utility, and SAR-style missions, trading speed for vertical access. The H225 is the larger, typically carrying about 16–19 passengers with a practical range around 500–600 nautical miles depending on fit and reserves. The AW189 is slightly smaller, commonly configured for roughly 16–18 passengers with a broadly similar practical range in the 450–550 nautical mile class. The Dassault Falcon 8X and Pilatus PC‑24 are fixed‑wing business jets optimized for fast point‑to‑point travel. The Falcon 8X is a long‑range, large‑cabin trijet, typically seating 12–16 passengers and capable of intercontinental range of roughly 6,000+ nautical miles. The PC‑24 is a “super versatile jet” designed for shorter runways and mixed mission flexibility; it typically seats 6–10 passengers (up to about 11 in high‑density layouts) with range around 2,000 nautical miles. Overall, the 8X leads in range and cabin size, the PC‑24 emphasizes access, and the helicopters excel where landing pads replace runways.
| Spec | AIRBUS H225 | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 | $ 15.57 | $ 3.71 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 17 | 21 | 6 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Leonardo | Pilatus |
| Aircraft Name | H225 | 8X | AW189 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 | 651 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | $ 0.74 | $ 0.62 |
| Max Cabin Seats | 28 | 16 | 19 | 10 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 36900 | — | 6680 |
| Standard Cabin Seats | 19 | 14 | 19 | 6 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | $ 2,413 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | EFIS | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 516 | 155 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $2,413,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 17 | 21 | 6 |
| Max Cabin Seats | 28 | 16 | 19 | 10 |
| Standard Cabin Seats | 19 | 14 | 19 | 6 |
| Lavatory | — | 2 Enclosed Flushing | — | 1 Enclosed Flushing |
| Crew Rest | — | No | — | No |
| Jump Seat | — | Yes | — | No |
| Galley Location | — | FWD | — | FWD |
| Lavatory Location | — | FWD / AFT | — | FWD |
| Cabin Pressure (psi) | — | 10.2 | — | 9.3 |
| Galley / Refreshment | — | Galley | — | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 29200 | — | 23500 |
| Max Cabin Altitude (ft) | — | 3900 | — | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PW307D | CT7-2E1 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | JetFuel | — |
| TBO (hrs) | 3500 | On-Condition | 4000 | 5000 |
| Horsepower | 2100 | — | 1983 | — |
| No. of Engines | 2 | 3 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 17 | — | ISA + 23 |
| Thrust (lbs) | — | 6722 | — | 3435 |
| Dimensions | ||||
| Length (ft) | 63.4 | 80.2 | 57.8 | 52.2 |
| Overall Height (ft) | 16.3 | 26.1 | 16.6 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | 48 | — |
| Cabin Volume (cu. ft) | 547 | 1695 | 395 | — |
| 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 |
| Cabin Width - Floor (ft) | — | 6.3 | — | 3.8 |
| Cabin Length - Seating (ft) | — | 29.2 | — | 17 |
| Baggage Volume Int. (cu. ft) | — | 140 | — | 90 |
| Baggage Volume Ext. (cu. ft) | — | — | 85 | — |
| Aisle Step (ft) | — | — | — | Flat Floor |