Airbus Helicopters H225 vs Piaggio Avanti Evo vs Robinson R66
The Airbus H225 is a large, twin‑engine helicopter typically used for offshore transport, search and rescue, and heavy utility missions. It offers the highest passenger capacity of the three, commonly seating around 16–19 passengers depending on configuration, and it also provides substantial range for a helicopter, roughly in the 400–500+ nautical mile class with reserves depending on payload and conditions. The Piaggio Avanti EVO is a twin‑turboprop fixed‑wing aircraft optimized for fast business travel. It generally carries about 6–7 passengers (often plus one or two pilots) and, as a fixed‑wing design, usually delivers the longest range of this group, commonly around 1,200–1,500 nautical miles depending on mission profile. The Robinson R66 is a light, single‑engine helicopter aimed at private, training, and light utility roles. It has the smallest capacity, typically 4 passengers plus a pilot, and the shortest range, roughly around 300 nautical miles, varying with fuel, load, and operating conditions.
| 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 |