Airbus Acj320 Neo vs Piaggio Avanti Evo
The Airbus ACJ320neo and the Piaggio Avanti EVO sit in very different aircraft categories. The ACJ320neo is an airliner-derived VIP “bizliner,” built around a large-cabin commercial jet platform intended for head-of-state or corporate shuttle missions with extensive cabin customization. The Avanti EVO is a twin‑turboprop business aircraft, optimized for efficient short- to mid-range trips, typically operating from smaller airports with lower operating costs. In range, the ACJ320neo generally offers intercontinental capability, typically around 6,000 nautical miles depending on configuration, allowing nonstop long-haul sectors with fewer refueling stops. The Avanti EVO is a medium-range aircraft, typically around 1,700 to 1,800 nautical miles, better suited to regional flying rather than true long-range missions. Passenger capacity also differs sharply. An ACJ320neo can be configured for high-density shuttle seating well over 100 passengers, but in VIP layouts it commonly carries a few dozen with lounges, bedrooms, and conference areas. The Avanti EVO is usually configured for about 6 to 9 passengers in an executive cabin.
| Spec | Airbus ACJ320 Neo | Piaggio Avanti EVO |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 14.74 | — |
| Min Crew | 4 | 1 |
| Total Seats | 12 | 8 |
| Manufacturer | Airbus | Piaggio |
| Aircraft Name | ACJ320 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6750 | 1530 |
| DOC / nm / Seat | $ 1.84 | — |
| Max Cabin Seats | 35 | 7 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 32500 | 3775 |
| Standard Cabin Seats | 8 | 6 |
| Direct Operating Cost | $ 6,926 | — |
| Flight Deck (Base Spec) | Thales | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 470 | 400 |
| Base Aircraft Price (USD) | $96,000,000 | $ 7,695,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 4 | 1 |
| Total Seats | 10 | 8 |
| Configuration | Green Interior | — |
| Max Cabin Seats | 35 | 7 |
| Standard Cabin Seats | 8 | 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 | CFM LEAP-1A27 | PT6A–66B |
| TBO (hrs) | On-Condition | 3600 |
| Thrust (lbs) | 27000 | — |
| No. of Engines | 2 | 2 |
| Horsepower | — | 850 |
| Flat Rating | — | ISA + 28 |
| Fuel Burn (gph) | — | 100 |
| Dimensions | ||
| Length (ft) | 111 | 47.3 |
| Wingspan (ft) | 117.5 | 47.1 |
| Cabin Width (ft) | 12.1 | 6.1 |
| Cabin Height (ft) | 7.4 | 5.8 |
| Cabin Length (ft) | 78.8 | 14.9 |
| Overall Height (ft) | 38.58 | 13.1 |
| Cabin Volume (cu. ft) | 6710 | — |
| Baggage Volume Ext. (cu. ft) | 943 | — |
| Cabin Width - Floor (ft) | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | 35.2 |