Airbus Helicopters H225 vs Dassault Falcon 8x vs Enstrom 480b vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter, optimized for vertical lift missions rather than point‑to‑point cruise. Its range is roughly 450–500 nautical miles depending on fit and reserves, and it typically carries around 16–19 passengers (with high‑density layouts possible for offshore roles). The Dassault Falcon 8X is a long‑range business jet built for intercontinental travel, offering about 6,400–6,450 nautical miles of range and usually seating 12–16 passengers in executive configurations. The Enstrom 480B is a light single‑engine piston helicopter aimed at utility, training, and short‑haul transport; practical range is around 200–250 nautical miles, with seating for up to five people including the pilot. The Piaggio Avanti EVO is a fast twin‑turboprop business aircraft that sits between light jets and turboprops in mission profile, typically offering roughly 1,500–1,800 nautical miles of range and seating commonly 7–9 passengers (up to about 9–11 depending on layout).
| Spec | AIRBUS H225 | Dassault Falcon 8X | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 | — |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 17 | 8 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Piaggio |
| Aircraft Name | H225 | 8X | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | — |
| Max Cabin Seats | 28 | 16 | 7 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 36900 | 3775 |
| Standard Cabin Seats | 19 | 14 | 6 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | — |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 516 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $ 7,695,000 |
| Cabin | |||
| Cockpit | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 17 | 8 |
| Max Cabin Seats | 28 | 16 | 7 |
| Standard Cabin Seats | 19 | 14 | 6 |
| Lavatory | — | 2 Enclosed Flushing | No |
| Crew Rest | — | No | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | FWD / AFT | — |
| Cabin Pressure (psi) | — | 10.2 | 9 |
| Galley / Refreshment | — | Galley | No |
| SL Cabin Altitude (ft) | — | 29200 | 24000 |
| Max Cabin Altitude (ft) | — | 3900 | 6600 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | PW307D | PT6A–66B |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | 3600 |
| Horsepower | 2100 | — | 850 |
| No. of Engines | 2 | 3 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 17 | ISA + 28 |
| Thrust (lbs) | — | 6722 | — |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 63.4 | 80.2 | 47.3 |
| Overall Height (ft) | 16.3 | 26.1 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 1695 | — |
| Wingspan (ft) | — | 86.3 | 47.1 |
| Cabin Width (ft) | — | 7.7 | 6.1 |
| Cabin Height (ft) | — | 6.2 | 5.8 |
| Cabin Length (ft) | — | 42.7 | 14.9 |
| Cabin Width - Floor (ft) | — | 6.3 | 3.5 |
| Cabin Length - Seating (ft) | — | 29.2 | — |
| Baggage Volume Int. (cu. ft) | — | 140 | 35.2 |