Airbus Helicopters H225 vs Dassault Falcon 8x vs Piaggio Avanti Evo vs Pilatus Pc 24
The Airbus H225 is a long‑range twin‑engine helicopter, best suited to vertical‑lift missions such as offshore transport, search and rescue, and utility work. Its range is typically on the order of about 500–650 nautical miles depending on configuration and reserves, and it generally carries around 16–19 passengers (with higher-density seating possible for specific roles). The Dassault Falcon 8X is an ultra‑long‑range large‑cabin business jet designed for intercontinental travel. It offers roughly 6,400 nautical miles of range and commonly accommodates about 12–16 passengers in executive layouts. The Piaggio Avanti EVO is a high‑speed turboprop business aircraft, positioned between light jets and traditional turboprops. It typically provides around 1,700–1,900 nautical miles of range and usually seats 6–9 passengers. The Pilatus PC‑24 is a “super versatile jet” optimized for short and rough-field capability compared with most business jets. It delivers roughly 2,000 nautical miles of range and typically carries 6–10 passengers, with flexible cabin arrangements for mixed passenger/cargo or medevac use.
| Spec | AIRBUS H225 | Dassault Falcon 8X | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 | — | $ 3.71 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 17 | 8 | 6 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Piaggio | Pilatus |
| Aircraft Name | H225 | 8X | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 | 1530 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | — | $ 0.62 |
| Max Cabin Seats | 28 | 16 | 7 | 10 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 36900 | 3775 | 6680 |
| Standard Cabin Seats | 19 | 14 | 6 | 6 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 516 | 400 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $ 7,695,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 17 | 8 | 6 |
| Max Cabin Seats | 28 | 16 | 7 | 10 |
| Standard Cabin Seats | 19 | 14 | 6 | 6 |
| Lavatory | — | 2 Enclosed Flushing | No | 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 | 9.3 |
| Galley / Refreshment | — | Galley | No | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 29200 | 24000 | 23500 |
| Max Cabin Altitude (ft) | — | 3900 | 6600 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PW307D | PT6A–66B | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 3600 | 5000 |
| Horsepower | 2100 | — | 850 | — |
| No. of Engines | 2 | 3 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 17 | ISA + 28 | ISA + 23 |
| Thrust (lbs) | — | 6722 | — | 3435 |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 80.2 | 47.3 | 52.2 |
| Overall Height (ft) | 16.3 | 26.1 | 13.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 1695 | — | — |
| 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 |
| 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 |