Airbus Helicopters H225 vs Dassault Falcon 8x vs Piaggio Avanti Evo vs Robinson R66
The Airbus H225 and Robinson R66 are helicopters, while the Dassault Falcon 8X and Piaggio Avanti EVO are fixed‑wing business aircraft. The H225 is a large, long‑range twin‑engine helicopter typically used for offshore transport, search and rescue, and utility missions; it can carry roughly 16–24 passengers depending on cabin layout and offers about 450–550 nautical miles of range. The Robinson R66 is a light turbine helicopter aimed at private and light utility use; it generally seats 4–5 occupants and has a range around 300–350 nautical miles. Among the airplanes, the Falcon 8X is an ultra‑long‑range business jet built for intercontinental travel; it typically carries about 12–16 passengers and can fly roughly 6,400 nautical miles. The Piaggio Avanti EVO is a high‑speed turboprop positioned between light jets and traditional turboprops; it usually seats 6–9 passengers and offers about 1,400–1,800 nautical miles of range.
| 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 |