Compare Airbus ACJ330 Neo vs Dassault Falcon 10X vs Piaggio Avanti EVO
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| Manufacturer | Airbus | Dassault Falcon | Piaggio |
| Aircraft Type | ACJ330 Neo | 10X | Avanti EVO |
| Base Aircraft Price (USD) | $101,500,000 | $ 75,000,000 | $ 7,695,000 |
| Direct Operating Cost | $ 7,965 | $2,770 | - |
| DOC / nm | $ 16.95 | - | - |
| DOC / nm / Seat | $ 2.12 | - | - |
| Max Cruise Speed (ktas) | 470 | 516 | 400 |
| Max Range (nm) | 6000 | 7505 | 1530 |
| Useful Load (lbs) | 28800 | 36900 | 3775 |
| Total Seats | 10 | 17 | 8 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 14 | 6 |
| Max Cabin Seats | 35 | 16 | 7 |
| Min Crew | 4 | 2 | 1 |
| Flight Deck (Base Spec) | Thales | Digital Flight Control System | 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 | - | 12100 |
| MLW (lbs) | 148600 | - | 11500 |
| MZFW (lbs) | 141700 | - | 9800 |
| BOW (lbs) | 106500 | - | 8375 |
| BEW (lbs) | - | - | 8325 |
| Useful Load (lbs) | 28800 | 36900 | 3775 |
| Max Payload (lbs) | - | - | 1425 |
| Fuel Capacity (lbs) | 60620 | - | 2802 |
| Payload Max Fuel (lbs) | - | - | 973 |
| Max Baggage Weight (lbs) | - | - | 350 |
| Dimensions | |||
| Wingspan (ft) | 117.5 | - | 47.1 |
| Overall Height (ft) | 38.58 | - | 13.1 |
| Length (ft) | 123.3 | - | 47.3 |
| Cabin Height (ft) | 7.4 | - | 5.8 |
| Cabin Width (ft) | 12.1 | - | 6.1 |
| Cabin Width - Floor (ft) | - | - | 3.5 |
| Cabin Length (ft) | 91 | - | 14.9 |
| Cabin Volume (cu. ft) | 7700 | - | - |
| Baggage Volume Int. (cu. ft) | - | - | 35.2 |
| Baggage Volume Ext. (cu. ft) | 1324 | - | - |
| Engine | |||
| No. of Engines | 2 | - | 2 |
| Manufacturer | Airbus | Dassault Falcon | Piaggio |
| Model | CFM LEAP-1A27 | - | PT6A–66B |
| Horsepower | - | - | 850 |
| Thrust (lbs) | 29000 | - | - |
| Flat Rating | - | - | ISA + 28 |
| FADEC | Yes | - | Yes |
| TBO (hrs) | On-Condition | - | 3600 |
| Fuel Burn (gph) | - | - | 100 |
| Avionics | |||
| Flight Deck | Thales | NeXus | Rockwell Collins Pro Line 21 |
| Flight Rules | - | - | IFR |
| FMS | 3 | - | - |
| Autopilot | 2 | - | - |
| PFD | 2 | - | - |
| MFD | 2 | - | - |
| GPS | 3 | - | - |
| AHRS | 1 | - | - |
| Transponder | 2 | - | - |
| VHF Com | 3 | - | - |
| VHF NAV | 3 | - | - |
| Cabin | |||
| Total Seats | 10 | 17 | 8 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 14 | 6 |
| Max Cabin Seats | 35 | 16 | 7 |
| Min Crew | 4 | 2 | 1 |
| Configuration | 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 | - | - |
| Airframe (Hrs) | 1000 | - | - |
| Engine (Yrs) | 2 | - | - |
| Engine (Hrs) | 1000 | - | - |
| APU (Hrs) | 2000 | - | - |
| Performance | |||
| Max Cruise Speed (Mach) | 0.82 | .925 | 0.7 |
| Max Cruise Speed (ktas) | 470 | 516 | 400 |
| Long Range Cruise (Mach) | 0.78 | - | - |
| Long Range Cruise (ktas) | 447 | - | 318 |
| Max Range (nm) | 6000 | 7505 | 1530 |
| Max Range Crew + 4 (nm) | 6000 | - | - |
| Max Range Crew + 6 (nm) | 6000 | - | - |
| Max Range Crew + 8 (nm) | 6000 | - | - |
| Take-off FL (ft) | 5020 | - | - |
| Take-off Roll (ft) | - | - | 3262 |
| Take-Off (5000 / ISA + 10) | - | - | 4700 |
| Landing Roll (ft) | 2850 | - | - |
| Landing >50ft Obst. (ft) | - | - | 3282 |
| Max Climb Rate (fpm) | - | - | 2770 |
| Service Ceiling (ft) | 41000 | - | 41000 |