Compare Airbus ACJ330 Neo vs Airbus ACJ320 Neo vs Piaggio Avanti EVO
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| Manufacturer | Airbus | Airbus | Piaggio |
| Aircraft Type | ACJ330 Neo | ACJ320 | Avanti EVO |
| Base Aircraft Price (USD) | $101,500,000 | $96,000,000 | $ 7,695,000 |
| Direct Operating Cost | $ 7,965 | $ 6,926 | - |
| DOC / nm | $ 16.95 | $ 14.74 | - |
| DOC / nm / Seat | $ 2.12 | $ 1.84 | - |
| Max Cruise Speed (ktas) | 470 | 470 | 400 |
| Max Range (nm) | 6000 | 6750 | 1530 |
| Useful Load (lbs) | 28800 | 32500 | 3775 |
| Total Seats | 10 | 10 | 8 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 8 | 6 |
| Max Cabin Seats | 35 | 35 | 7 |
| Min Crew | 4 | 4 | 1 |
| Flight Deck (Base Spec) | Thales | Thales | Rockwell Collins Pro Line 21 |
| Flight Rules | - | - | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Weights | |||
| MRAMP (lbs) | - | - | 12150 |
| MTOW (lbs) | 174100 | 172400 | 12100 |
| MLW (lbs) | 148600 | 140850 | 11500 |
| MZFW (lbs) | 141700 | 116850 | 9800 |
| BOW (lbs) | 106500 | 102000 | 8375 |
| BEW (lbs) | - | - | 8325 |
| Useful Load (lbs) | 28800 | 32500 | 3775 |
| Max Payload (lbs) | - | - | 1425 |
| Fuel Capacity (lbs) | 60620 | 66000 | 2802 |
| Payload Max Fuel (lbs) | - | - | 973 |
| Max Baggage Weight (lbs) | - | - | 350 |
| Dimensions | |||
| Wingspan (ft) | 117.5 | 117.5 | 47.1 |
| Overall Height (ft) | 38.58 | 38.58 | 13.1 |
| Length (ft) | 123.3 | 111 | 47.3 |
| Cabin Height (ft) | 7.4 | 7.4 | 5.8 |
| Cabin Width (ft) | 12.1 | 12.1 | 6.1 |
| Cabin Width - Floor (ft) | - | - | 3.5 |
| Cabin Length (ft) | 91 | 78.8 | 14.9 |
| Cabin Volume (cu. ft) | 7700 | 6710 | - |
| Baggage Volume Int. (cu. ft) | - | - | 35.2 |
| Baggage Volume Ext. (cu. ft) | 1324 | 943 | - |
| Engine | |||
| No. of Engines | 2 | 2 | 2 |
| Manufacturer | Airbus | Airbus | Piaggio |
| Model | CFM LEAP-1A27 | CFM LEAP-1A27 | PT6A–66B |
| Horsepower | - | - | 850 |
| Thrust (lbs) | 29000 | 27000 | - |
| Flat Rating | - | - | ISA + 28 |
| FADEC | Yes | Yes | Yes |
| TBO (hrs) | On-Condition | On-Condition | 3600 |
| Fuel Burn (gph) | - | - | 100 |
| Avionics | |||
| Flight Deck | Thales | Thales | Rockwell Collins Pro Line 21 |
| Flight Rules | - | - | IFR |
| FMS | 3 | 3 | - |
| Autopilot | 2 | 2 | - |
| PFD | 2 | 2 | - |
| MFD | 2 | 2 | - |
| GPS | 3 | 3 | - |
| AHRS | 1 | 1 | - |
| Transponder | 2 | 2 | - |
| VHF Com | 3 | 3 | - |
| VHF NAV | 3 | 3 | - |
| Cabin | |||
| Total Seats | 10 | 10 | 8 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 8 | 6 |
| Max Cabin Seats | 35 | 35 | 7 |
| Min Crew | 4 | 4 | 1 |
| Configuration | Green Interior | Green Interior | - |
| Lavatory | - | - | No |
| Galley / Refreshment | - | - | No |
| Max Cabin Altitude (ft) | - | - | 6600 |
| SL Cabin Altitude (ft) | - | - | 24000 |
| Cabin Pressure (psi) | - | - | 9 |
| Other | |||
| Prop Manufacturer | - | - | Hartzell |
| Prop Description | - | - | Scimitar |
| Gear Type | - | - | Retractable |
| Warranty | |||
| Airframe (Yrs) | 3 | 3 | - |
| Airframe (Hrs) | 1000 | 1000 | - |
| Engine (Yrs) | 2 | 2 | - |
| Engine (Hrs) | 1000 | 1000 | - |
| APU (Hrs) | 2000 | 2000 | - |
| Performance | |||
| Max Cruise Speed (Mach) | 0.82 | 0.82 | 0.7 |
| Max Cruise Speed (ktas) | 470 | 470 | 400 |
| Long Range Cruise (Mach) | 0.78 | 0.78 | - |
| Long Range Cruise (ktas) | 447 | 447 | 318 |
| Max Range (nm) | 6000 | 6750 | 1530 |
| Max Range Crew + 4 (nm) | 6000 | 6750 | - |
| Max Range Crew + 6 (nm) | 6000 | 6750 | - |
| Max Range Crew + 8 (nm) | 6000 | 6750 | - |
| Take-off FL (ft) | 5020 | 5400 | - |
| Take-off Roll (ft) | - | - | 3262 |
| Take-Off (5000 / ISA + 10) | - | - | 4700 |
| Landing Roll (ft) | 2850 | 2680 | - |
| Landing >50ft Obst. (ft) | - | - | 3282 |
| Max Climb Rate (fpm) | - | - | 2770 |
| Service Ceiling (ft) | 41000 | 41000 | 41000 |