Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Piaggio Avanti Evo vs Robinson R66
The Airbus H225 and Robinson R66 are helicopters, while the Cessna 208B Grand Caravan EX and Piaggio Avanti EVO are fixed‑wing turboprops, so their strengths differ immediately: helicopters trade speed and efficiency for vertical lift and access to confined sites. The H225 is a large, long‑range twin‑engine rotorcraft used for offshore, SAR, and utility missions, typically carrying roughly 19 passengers (high‑density layouts can be more) and offering on the order of 450–500+ nm range depending on fuel and payload. The R66 is a light single‑engine helicopter, usually 4–5 seats, with a much shorter typical range around 300 nm. The Grand Caravan EX is a rugged single‑engine utility turboprop, commonly 9–14 passengers, with about 900–1,000 nm range. The Piaggio Avanti EVO is a fast, pressurized twin‑turboprop business aircraft, typically 7–9 passengers, with roughly 1,500–1,800 nm range, emphasizing speed and comfort over rough‑field hauling.
| Spec | AIRBUS H225 | Piaggio Avanti EVO |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | — |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 8 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Piaggio |
| Aircraft Name | H225 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1530 |
| DOC / nm / Seat | $ 0.99 | — |
| Max Cabin Seats | 28 | 7 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 3775 |
| Standard Cabin Seats | 19 | 6 |
| Direct Operating Cost | $ 2,963 | — |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 7,695,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 8 |
| Max Cabin Seats | 28 | 7 |
| Standard Cabin Seats | 19 | 6 |
| Lavatory | — | No |
| Cabin Pressure (psi) | — | 9 |
| Galley / Refreshment | — | No |
| SL Cabin Altitude (ft) | — | 24000 |
| Max Cabin Altitude (ft) | — | 6600 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 2A1 | PT6A–66B |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | 3600 |
| Horsepower | 2100 | 850 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | — |
| Flat Rating | — | ISA + 28 |
| Fuel Burn (gph) | — | 100 |
| Dimensions | ||
| Length (ft) | 63.4 | 47.3 |
| Overall Height (ft) | 16.3 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | — |
| Wingspan (ft) | — | 47.1 |
| Cabin Width (ft) | — | 6.1 |
| Cabin Height (ft) | — | 5.8 |
| Cabin Length (ft) | — | 14.9 |
| Cabin Width - Floor (ft) | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | 35.2 |