Airbus Helicopters H225 vs Dassault Falcon 8x vs Embraer Legacy 650 E vs Piaggio Avanti Evo
The Airbus H225 is a twin‑engine heavy helicopter rather than a fixed‑wing business aircraft. It’s optimized for short to medium missions, typically a few hundred nautical miles without refueling depending on payload and reserves, and it can carry roughly 16–19 passengers in offshore/utility seating (fewer in VIP layouts). The Dassault Falcon 8X is an ultra‑long‑range business jet, designed for intercontinental flying at about 6,450 nm, generally seating around 12–16 passengers in typical executive configurations. The Embraer Legacy 650E is a large‑cabin long‑range business jet with transcontinental capability of about 3,900 nm and typically accommodates about 13 passengers, with a generous cabin volume for its class. The Piaggio Avanti EVO is a twin‑turboprop business aircraft positioned for efficient regional travel; it offers roughly 1,700–1,800 nm range and usually seats 6–8 passengers. Overall, the Falcon 8X leads on range, the Legacy 650E emphasizes cabin comfort and solid long‑range performance, the Avanti EVO prioritizes efficiency on shorter routes, and the H225 stands apart for vertical lift and access to remote sites.
| 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 |