Leonardo Aw139 vs Piaggio Avanti Evo
The Leonardo AW139 and Piaggio Avanti EVO serve different missions and fall into different categories. The AW139 is a twin‑engine, medium helicopter designed for vertical lift operations such as offshore transport, search and rescue, emergency medical services, and utility work, with the key advantage of landing in confined areas without runways. The Piaggio Avanti EVO is a twin‑engine turboprop business aircraft optimized for fast point‑to‑point travel from airports, emphasizing cabin comfort and efficiency. In range, the Avanti EVO typically offers longer nonstop capability than an AW139 because it is a fixed‑wing aircraft cruising efficiently at altitude, while the AW139’s range is generally shorter and more sensitive to payload and hover/loiter demands typical of helicopter missions. For passenger capacity, an AW139 is commonly configured for roughly 8 to 15 passengers depending on layout and mission equipment, whereas the Avanti EVO is usually arranged for about 6 to 9 passengers in a business cabin configuration. Overall, choose the AW139 for access and mission flexibility, and the Avanti EVO for speed and longer airport‑to‑airport trips.
| Spec | AGUSTA / LEONARDO AW139 | Piaggio Avanti EVO |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 11.69 | — |
| Min Crew | 2 | 1 |
| Total Seats | 17 | 8 |
| Flight Rules | IFR | IFR |
| Manufacturer | Leonardo | Piaggio |
| Aircraft Name | AW139 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 573 | 1530 |
| DOC / nm / Seat | $ 0.69 | — |
| Max Cabin Seats | 15 | 7 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4701 | 3775 |
| Standard Cabin Seats | 15 | 6 |
| Direct Operating Cost | $ 1,929 | — |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 165 | 400 |
| Base Aircraft Price (USD) | $15,900,000 | $ 7,695,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 17 | 8 |
| Max Cabin Seats | 15 | 7 |
| Standard Cabin Seats | 15 | 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 | PT6C-67C | PT6A–66B |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 5000 | 3600 |
| Horsepower | 1679 | 850 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 414 | — |
| Flat Rating | — | ISA + 28 |
| Fuel Burn (gph) | — | 100 |
| Dimensions | ||
| Length (ft) | 54.7 | 47.3 |
| Overall Height (ft) | 16.4 | 13.1 |
| Rotor Diameter (ft) | 54.7 | — |
| Cabin Volume (cu. ft) | 282 | — |
| Baggage Volume Ext. (cu. ft) | 120 | — |
| 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 |