Compare Airbus ACJ330 Neo vs Airbus ACJ320 Neo vs Beechcraft King Air 360ER vs Piaggio Avanti EVO
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| Manufacturer | Airbus | Airbus | Beechcraft | Piaggio |
| Aircraft Type | ACJ330 Neo | ACJ320 | KingAir 350ER | Avanti EVO |
| Base Aircraft Price (USD) | $101,500,000 | $96,000,000 | $8,750,000 | $ 7,695,000 |
| Direct Operating Cost | $ 7,965 | $ 6,926 | $ 1,324 | - |
| DOC / nm | $ 16.95 | $ 14.74 | $ 4.37 | - |
| DOC / nm / Seat | $ 2.12 | $ 1.84 | $ 0.55 | - |
| Max Cruise Speed (ktas) | 470 | 470 | 303 | 400 |
| Max Range (nm) | 6000 | 6750 | 2338 | 1530 |
| Useful Load (lbs) | 28800 | 32500 | 6585 | 3775 |
| Total Seats | 10 | 10 | 10 | 8 |
| Cockpit | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 8 | 8 | 6 |
| Max Cabin Seats | 35 | 35 | 9 | 7 |
| Min Crew | 4 | 4 | 1 | 1 |
| Flight Deck (Base Spec) | Thales | Thales | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line 21 |
| Flight Rules | - | - | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Weights | ||||
| MRAMP (lbs) | - | - | 16600 | 12150 |
| MTOW (lbs) | 174100 | 172400 | 16500 | 12100 |
| MLW (lbs) | 148600 | 140850 | 15675 | 11500 |
| MZFW (lbs) | 141700 | 116850 | 13000 | 9800 |
| BOW (lbs) | 106500 | 102000 | 10215 | 8375 |
| BEW (lbs) | - | - | 9915 | 8325 |
| Useful Load (lbs) | 28800 | 32500 | 6585 | 3775 |
| Max Payload (lbs) | - | - | 2785 | 1425 |
| Fuel Capacity (lbs) | 60620 | 66000 | 5192 | 2802 |
| Payload Max Fuel (lbs) | - | - | 1193 | 973 |
| Max Baggage Weight (lbs) | - | - | 1150 | 350 |
| Dimensions | ||||
| Wingspan (ft) | 117.5 | 117.5 | 57.9 | 47.1 |
| Overall Height (ft) | 38.58 | 38.58 | 14.4 | 13.1 |
| Length (ft) | 123.3 | 111 | 46.7 | 47.3 |
| Cabin Height (ft) | 7.4 | 7.4 | 4.8 | 5.8 |
| Cabin Width (ft) | 12.1 | 12.1 | 4.5 | 6.1 |
| Cabin Width - Floor (ft) | - | - | 4.1 | 3.5 |
| Cabin Length (ft) | 91 | 78.8 | 19.5 | 14.9 |
| Cabin Length - Seating (ft) | - | - | 19.5 | - |
| Cabin Volume (cu. ft) | 7700 | 6710 | - | - |
| Baggage Volume Int. (cu. ft) | - | - | 71 | 35.2 |
| Baggage Volume Ext. (cu. ft) | 1324 | 943 | - | - |
| Engine | ||||
| No. of Engines | 2 | 2 | 1 | 2 |
| Manufacturer | Airbus | Airbus | Beechcraft | Piaggio |
| Model | CFM LEAP-1A27 | CFM LEAP-1A27 | PT6A-60A | PT6A–66B |
| Horsepower | - | - | 1050 | 850 |
| Thrust (lbs) | 29000 | 27000 | - | - |
| Flat Rating | - | - | ISA + 10 | ISA + 28 |
| FADEC | Yes | Yes | Yes | Yes |
| TBO (hrs) | On-Condition | On-Condition | 3600 | 3600 |
| Fuel Capacity (gal) | - | - | 775 | - |
| Fuel Burn (gph) | - | - | - | 100 |
| Avionics | ||||
| Flight Deck | Thales | Thales | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line 21 |
| Flight Rules | - | - | IFR | IFR |
| FMS | 3 | 3 | 2 | - |
| Autopilot | 2 | 2 | 1 | - |
| PFD | 2 | 2 | 2 | - |
| MFD | 2 | 2 | 1 | - |
| GPS | 3 | 3 | 1 | - |
| AHRS | 1 | 1 | 1 | - |
| Transponder | 2 | 2 | 1 | - |
| VHF Com | 3 | 3 | 2 | - |
| VHF NAV | 3 | 3 | 2 | - |
| Cabin | ||||
| Total Seats | 10 | 10 | 10 | 8 |
| Cockpit | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 8 | 8 | 6 |
| Max Cabin Seats | 35 | 35 | 9 | 7 |
| Min Crew | 4 | 4 | 1 | 1 |
| Configuration | Green Interior | Green Interior | - | - |
| Cargo Door | - | - | Optional | - |
| Lavatory | - | - | Yes (Belted Optional) | No |
| Lavatory Location | - | - | AFT | - |
| Galley / Refreshment | - | - | Refreshment Center | No |
| Galley Location | - | - | FWD | - |
| Max Cabin Altitude (ft) | - | - | - | 6600 |
| SL Cabin Altitude (ft) | - | - | - | 24000 |
| Cabin Pressure (psi) | - | - | 6.5 | 9 |
| Other | ||||
| Prop Manufacturer | - | - | Hartzell | Hartzell |
| Prop Description | - | - | 4-Blade Constant Feathering Reverse | Scimitar |
| Gear Type | - | - | Retractable | 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 | 0.58 | 0.7 |
| Max Cruise Speed (ktas) | 470 | 470 | 303 | 400 |
| Long Range Cruise (Mach) | 0.78 | 0.78 | - | - |
| Long Range Cruise (ktas) | 447 | 447 | 238 | 318 |
| Vref (kias) | - | - | 104 | - |
| Stall Speed - Clean (kias) | - | - | 82 | - |
| Max Range (nm) | 6000 | 6750 | 2338 | 1530 |
| Max Range Crew + 4 (nm) | 6000 | 6750 | 2271 | - |
| Max Range Crew + 6 (nm) | 6000 | 6750 | - | - |
| Max Range Crew + 8 (nm) | 6000 | 6750 | - | - |
| Take-off FL (ft) | 5020 | 5400 | 4057 | - |
| Take-off Roll (ft) | - | - | - | 3262 |
| Take-Off (5000 / ISA + 10) | - | - | 7675 | 4700 |
| Landing Roll (ft) | 2850 | 2680 | - | - |
| Landing >50ft Obst. (ft) | - | - | 2728 | 3282 |
| Max Climb Rate (fpm) | - | - | 2400 | 2770 |
| Service Ceiling (ft) | 41000 | 41000 | 35000 | 41000 |