Airbus Helicopters H225 vs Embraer Legacy 650 E vs Leonardo Aw189 vs Piaggio Avanti Evo
The Airbus H225 and Leonardo AW189 are large twin‑engine helicopters, typically chosen for offshore, search-and-rescue, or utility missions where vertical lift matters more than speed. Both generally seat around 16–19 passengers in high‑density layouts (often fewer in VIP), with typical operational ranges roughly in the 450–550 nautical mile class depending on payload and reserves; the H225 is usually the larger, heavier‑lift option, while the AW189 sits slightly below it. The Embraer Legacy 650E and Piaggio Avanti EVO are fixed‑wing business aircraft optimized for fast point‑to‑point travel. The Legacy 650E is a long‑range large‑cabin jet, usually configured for about 13 passengers (up to around 14), with an intercontinental‑style range near 3,900 nautical miles. The Avanti EVO is a high‑speed turboprop with a smaller cabin, typically 6–8 passengers, and a range around 1,700–1,800 nautical miles, trading some range and cabin size for efficiency and lower operating costs.
| Spec | AIRBUS H225 | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.57 | — |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 21 | 8 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Leonardo | Piaggio |
| Aircraft Name | H225 | AW189 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 651 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.74 | — |
| Max Cabin Seats | 28 | 19 | 7 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — | 3775 |
| Standard Cabin Seats | 19 | 19 | 6 |
| Direct Operating Cost | $ 2,963 | $ 2,413 | — |
| Flight Deck (Base Spec) | EFIS | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 155 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $2,413,000 | $ 7,695,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 21 | 8 |
| Max Cabin Seats | 28 | 19 | 7 |
| Standard Cabin Seats | 19 | 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 | Makila 2A1 | CT7-2E1 | PT6A–66B |
| Fuel Type | JetFuel | JetFuel | — |
| TBO (hrs) | 3500 | 4000 | 3600 |
| Horsepower | 2100 | 1983 | 850 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | — | ISA + 28 |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 63.4 | 57.8 | 47.3 |
| Overall Height (ft) | 16.3 | 16.6 | 13.1 |
| Rotor Diameter (ft) | 53.2 | 48 | — |
| Cabin Volume (cu. ft) | 547 | 395 | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — |
| 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 |