Compare Airbus ACJ330 Neo vs Beechcraft King Air 360ER vs Embraer Lineage 1000E vs Embraer Praetor 600
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| Manufacturer | Airbus | Beechcraft | Embraer | Embraer |
| Aircraft Type | ACJ330 Neo | KingAir 350ER | Lineage 1000E | Praetor 600 |
| Base Aircraft Price (USD) | $101,500,000 | $8,750,000 | $51,250,000 | $20,995,000 |
| Direct Operating Cost | $ 7,965 | $ 1,324 | $ 5,827 | $ 3,141 |
| DOC / nm | $ 16.95 | $ 4.37 | $ 11.68 | $ 6.74 |
| DOC / nm / Seat | $ 2.12 | $ 0.55 | $ 0.97 | $ 0.84 |
| Max Cruise Speed (ktas) | 470 | 303 | 470 | 476 |
| Max Range (nm) | 6000 | 2338 | 4640 | 4018 |
| Useful Load (lbs) | 28800 | 6585 | 50043 | - |
| Total Seats | 10 | 10 | 14 | 10 |
| Cockpit | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 8 | 12 | 8 |
| Max Cabin Seats | 35 | 9 | 19 | 12 |
| Min Crew | 4 | 1 | 3 | 2 |
| Flight Deck (Base Spec) | Thales | Rockwell Collins Pro Line Fusion | Honeywell Primus Epic | Rockwell Collins Pro Line Fusion |
| Flight Rules | - | IFR | - | - |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Weights | ||||
| MRAMP (lbs) | - | 16600 | 120591 | - |
| MTOW (lbs) | 174100 | 16500 | 120591 | - |
| MLW (lbs) | 148600 | 15675 | 100972 | - |
| MZFW (lbs) | 141700 | 13000 | 80469 | - |
| BOW (lbs) | 106500 | 10215 | 70548 | - |
| BEW (lbs) | - | 9915 | 70548 | - |
| Useful Load (lbs) | 28800 | 6585 | 50043 | - |
| Max Payload (lbs) | - | 2785 | 9921 | 4001 |
| Fuel Capacity (lbs) | 60620 | 5192 | 48217 | - |
| Payload Max Fuel (lbs) | - | 1193 | 1826 | - |
| Max Baggage Weight (lbs) | - | 1150 | 2998 | - |
| Dimensions | ||||
| Wingspan (ft) | 117.5 | 57.9 | 94.2 | 70.5 |
| Overall Height (ft) | 38.58 | 14.4 | 34.7 | 21 |
| Length (ft) | 123.3 | 46.7 | 119 | 68.1 |
| Cabin Height (ft) | 7.4 | 4.8 | 6.6 | 6 |
| Aisle Step (ft) | - | - | Flat Floor | Flat Floor |
| Cabin Width (ft) | 12.1 | 4.5 | 8.8 | 6.8 |
| Cabin Width - Floor (ft) | - | 4.1 | 8 | 4.7 |
| Cabin Length (ft) | 91 | 19.5 | 76.6 | 24.1 |
| Cabin Length - Seating (ft) | - | 19.5 | 67.2 | 21.3 |
| Cabin Volume (cu. ft) | 7700 | - | - | - |
| Baggage Volume Int. (cu. ft) | - | 71 | 323 | 45 |
| Baggage Volume Ext. (cu. ft) | 1324 | - | 120 | 110 |
| Engine | ||||
| No. of Engines | 2 | 1 | 2 | 2 |
| Manufacturer | Airbus | Beechcraft | Embraer | Embraer |
| Model | CFM LEAP-1A27 | PT6A-60A | CF34-10 E7-B | HTF7500E |
| Horsepower | - | 1050 | - | - |
| Thrust (lbs) | 29000 | - | 18500 | 7528 |
| Flat Rating | - | ISA + 10 | ISA + 15 | ISA + 18 |
| FADEC | Yes | Yes | Yes | Yes |
| TBO (hrs) | On-Condition | 3600 | On-Condition | On-Condition |
| Fuel Capacity (gal) | - | 775 | - | 1963 |
| Fuel Burn (lbph) | - | - | 4184 | - |
| Avionics | ||||
| Flight Deck | Thales | Rockwell Collins Pro Line Fusion | Honeywell Primus Epic | Rockwell Collins Pro Line Fusion |
| Flight Rules | - | IFR | - | - |
| FMS | 3 | 2 | 2 | 2 |
| Autopilot | 2 | 1 | 1 | 2 |
| PFD | 2 | 2 | 2 | 2 |
| MFD | 2 | 1 | 2 | 2 |
| GPS | 3 | 1 | 1 | 2 |
| AHRS | 1 | 1 | 1 | 1 |
| Transponder | 2 | 1 | 1 | 2 |
| VHF Com | 3 | 2 | 1 | 2 |
| VHF NAV | 3 | 2 | 1 | 2 |
| Cabin | ||||
| Total Seats | 10 | 10 | 14 | 10 |
| Cockpit | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 8 | 12 | 8 |
| Max Cabin Seats | 35 | 9 | 19 | 12 |
| Min Crew | 4 | 1 | 3 | 2 |
| Configuration | Green Interior | - | - | - |
| Cargo Door | - | Optional | - | - |
| Connectivity | - | - | - | Gogo AVANCE L5 |
| Lavatory | - | Yes (Belted Optional) | 2 Enclosed Flushing | 1 Enclosed Belted Flushing |
| Lavatory Location | - | AFT | FWD / AFT | AFT |
| Galley / Refreshment | - | Refreshment Center | Galley | Galley |
| Galley Location | - | FWD | FWD | FWD |
| Crew Rest | - | - | Yes | No |
| Jump Seat | - | - | Yes | No |
| Max Cabin Altitude (ft) | - | - | - | 5800 |
| SL Cabin Altitude (ft) | - | - | 23190 | 27140 |
| Cabin Pressure (psi) | - | 6.5 | 8.8 | 9.7 |
| Other | ||||
| Prop Manufacturer | - | Hartzell | - | - |
| Prop Description | - | 4-Blade Constant Feathering Reverse | - | - |
| Gear Type | - | Retractable | - | - |
| Warranty | ||||
| Airframe (Yrs) | 3 | - | 3 | 3 |
| Airframe (Hrs) | 1000 | - | 1000 | 1000 |
| Engine (Yrs) | 2 | - | 2 | 2 |
| Engine (Hrs) | 1000 | - | 1000 | 1000 |
| APU (Hrs) | 2000 | - | 2000 | 2000 |
| Performance | ||||
| Max Cruise Speed (Mach) | 0.82 | 0.58 | 0.82 | 0.83 |
| Max Cruise Speed (ktas) | 470 | 303 | 470 | 476 |
| Long Range Cruise (Mach) | 0.78 | - | 0.78 | 0.77 |
| Long Range Cruise (ktas) | 447 | 238 | 447 | 440 |
| Vref (kias) | - | 104 | 110 | 102 |
| Stall Speed - Clean (kias) | - | 82 | - | - |
| Max Range (nm) | 6000 | 2338 | 4640 | 4018 |
| Max Range Crew + 4 (nm) | 6000 | 2271 | 4602 | 4018 |
| Max Range Crew + 6 (nm) | 6000 | - | - | - |
| Max Range Crew + 8 (nm) | 6000 | - | - | - |
| Take-off FL (ft) | 5020 | 4057 | 6076 | 4717 |
| Take-Off (5000 / ISA + 10) | - | 7675 | 9500 | - |
| Landing Roll (ft) | 2850 | - | 2450 | 2165 |
| Landing >50ft Obst. (ft) | - | 2728 | - | - |
| Max Climb Rate (fpm) | - | 2400 | 2464 | - |
| Service Ceiling (ft) | 41000 | 35000 | 41000 | 45000 |