Airbus Helicopters H175 vs Airbus Helicopters H225 vs Piaggio Avanti Evo
The Airbus Helicopters H175 and H225 are medium and heavy twin‑engine helicopters designed primarily for offshore transport, search and rescue, and utility missions, while the Piaggio Avanti EVO is a twin‑turboprop fixed‑wing business aircraft optimized for fast point‑to‑point travel from runways. In range, the H175 typically offers roughly 600–700 nm depending on configuration and reserves, whereas the larger H225 is generally in a similar ballpark (often around 600–700+ nm) but can vary more with payload, role equipment, and fuel fit. The Avanti EVO usually delivers longer fixed‑wing legs, commonly around 1,400–1,700 nm, reflecting better cruise efficiency and speed than rotorcraft, but it cannot hover or operate vertically. For passenger capacity, the H175 is commonly arranged for about 12–16 passengers in typical transport layouts, the H225 for about 16–19 in standard offshore seating (and can be higher in high‑density configurations), while the Avanti EVO typically seats about 7–9 passengers in executive cabin layouts.
| Spec | AIRBUS H175 | AIRBUS H225 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 13.53 | $ 20.87 | — |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 21 | 8 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Piaggio |
| Aircraft Name | H175 | H225 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 573 | 454 | 1530 |
| DOC / nm / Seat | $ 0.75 | $ 0.99 | — |
| Max Cabin Seats | 18 | 28 | 7 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6797 | 11929 | 3775 |
| Standard Cabin Seats | 16 | 19 | 6 |
| Direct Operating Cost | $ 2,016 | $ 2,963 | — |
| Flight Deck (Base Spec) | EFIS | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 149 | 142 | 400 |
| Base Aircraft Price (USD) | $17,900,000 | $ 29,500,000 | $ 7,695,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 21 | 8 |
| Max Cabin Seats | 18 | 28 | 7 |
| Standard Cabin Seats | 16 | 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 | Yes |
| Model | PT6A-67E | Makila 2A1 | PT6A–66B |
| Fuel Type | JetFuel | JetFuel | — |
| TBO (hrs) | 3500 | 3500 | 3600 |
| Horsepower | 1775 | 2100 | 850 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | — | 684 | — |
| Flat Rating | — | — | ISA + 28 |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 59.2 | 63.4 | 47.3 |
| Overall Height (ft) | 17.5 | 16.3 | 13.1 |
| Rotor Diameter (ft) | 48.5 | 53.2 | — |
| Cabin Volume (cu. ft) | 423.8 | 547 | — |
| Baggage Volume Ext. (cu. ft) | 81.9 | — | — |
| 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 |