Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Dassault Falcon 8x vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter, best suited to offshore, SAR, and utility missions where vertical lift matters more than speed; it typically carries around 19 passengers and has a mission range on the order of roughly 500–600 nautical miles, depending on load and reserves. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility airplane optimized for short/rough strips and cargo or regional hops; it commonly seats 9–14 passengers and typically ranges about 800–900 nautical miles. The Dassault Falcon 8X is a long‑range tri‑jet business aircraft aimed at intercontinental travel; it usually carries about 12–16 passengers in executive layouts and offers roughly 6,000+ nautical miles of range. The Piaggio Avanti EVO is a high‑speed twin‑turboprop business aircraft positioned between utility turboprops and jets; it generally seats about 6–9 passengers and typically ranges around 1,700–1,900 nautical miles. Overall, the Falcon 8X leads in range and speed, the H225 leads in lift/VTOL capability, the Caravan leads in rugged versatility and simplicity, and the Avanti EVO balances efficiency with near‑light‑jet cruise performance.
| 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 |