Compare Airbus ACJ330 Neo vs Bombardier Challenger 3500 vs Embraer Praetor 600
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| Manufacturer | Airbus | Bombardier | Embraer |
| Aircraft Type | ACJ330 Neo | Challenger 3500 | Praetor 600 |
| Base Aircraft Price (USD) | $101,500,000 | $26,950,000 | $20,995,000 |
| Direct Operating Cost | $ 7,965 | $ 3,152 | $ 3,141 |
| DOC / nm | $ 16.95 | $ 6.71 | $ 6.74 |
| DOC / nm / Seat | $ 2.12 | $ 0.84 | $ 0.84 |
| Max Cruise Speed (ktas) | 470 | 533 | 476 |
| Max Range (nm) | 6000 | 3400 | 4018 |
| Useful Load (lbs) | 28800 | 15950 | - |
| Total Seats | 10 | 10 | 10 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 8 | 8 |
| Max Cabin Seats | 35 | 10 | 12 |
| Min Crew | 4 | 2 | 2 |
| Flight Deck (Base Spec) | Thales | Rockwell Collins Pro Line 21 Advanced | Rockwell Collins Pro Line Fusion |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Weights | |||
| MRAMP (lbs) | - | 40750 | - |
| MTOW (lbs) | 174100 | 40600 | - |
| MLW (lbs) | 148600 | 34150 | - |
| MZFW (lbs) | 141700 | 28200 | - |
| BOW (lbs) | 106500 | 24800 | - |
| BEW (lbs) | - | 24650 | - |
| Useful Load (lbs) | 28800 | 15950 | - |
| Max Payload (lbs) | - | 3400 | 4001 |
| Fuel Capacity (lbs) | 60620 | 14045 | - |
| Payload Max Fuel (lbs) | - | 1905 | - |
| Max Baggage Weight (lbs) | - | 750 | - |
| Dimensions | |||
| Wingspan (ft) | 117.5 | 69 | 70.5 |
| Overall Height (ft) | 38.58 | 20 | 21 |
| Length (ft) | 123.3 | 68.7 | 68.1 |
| Cabin Height (ft) | 7.4 | 6 | 6 |
| Aisle Step (ft) | - | Flat Floor | Flat Floor |
| Cabin Width (ft) | 12.1 | 7.2 | 6.8 |
| Cabin Width - Floor (ft) | - | 5.1 | 4.7 |
| Cabin Length (ft) | 91 | 25.2 | 24.1 |
| Cabin Length - Seating (ft) | - | 16.6 | 21.3 |
| Cabin Volume (cu. ft) | 7700 | - | - |
| Baggage Volume Int. (cu. ft) | - | 106 | 45 |
| Baggage Volume Ext. (cu. ft) | 1324 | - | 110 |
| Engine | |||
| No. of Engines | 2 | 2 | 2 |
| Manufacturer | Airbus | Bombardier | Embraer |
| Model | CFM LEAP-1A27 | HTF73500 | HTF7500E |
| Thrust (lbs) | 29000 | 7323 | 7528 |
| Flat Rating | - | ISA + 15 | ISA + 18 |
| FADEC | Yes | Yes | Yes |
| TBO (hrs) | On-Condition | On-Condition | On-Condition |
| Fuel Capacity (gal) | - | - | 1963 |
| Avionics | |||
| Flight Deck | Thales | Rockwell Collins Pro Line 21 Advanced | Rockwell Collins Pro Line Fusion |
| FMS | 3 | 2 | 2 |
| Autopilot | 2 | 2 | 2 |
| PFD | 2 | 2 | 2 |
| MFD | 2 | 2 | 2 |
| GPS | 3 | 2 | 2 |
| AHRS | 1 | 2 | 1 |
| Transponder | 2 | 1 | 2 |
| VHF Com | 3 | 2 | 2 |
| VHF NAV | 3 | 2 | 2 |
| Cabin | |||
| Total Seats | 10 | 10 | 10 |
| Cockpit | 2 | 2 | 2 |
| Standard Cabin Seats | 8 | 8 | 8 |
| Max Cabin Seats | 35 | 10 | 12 |
| Min Crew | 4 | 2 | 2 |
| Configuration | Green Interior | - | - |
| Connectivity | - | - | Gogo AVANCE L5 |
| Lavatory | - | 1 Enclosed Flushing | 1 Enclosed Belted Flushing |
| Lavatory Location | - | AFT | AFT |
| Galley / Refreshment | - | Galley | Galley |
| Galley Location | - | FWD | FWD |
| Crew Rest | - | No | No |
| Jump Seat | - | Yes | No |
| Max Cabin Altitude (ft) | - | - | 5800 |
| SL Cabin Altitude (ft) | - | 23338 | 27140 |
| Cabin Pressure (psi) | - | 8.8 | 9.7 |
| Other | |||
| APU Manufacturer | - | - | - |
| APU Model | - | - | - |
| APU TBO (hrs) | - | - | - |
| 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 | 0.82 | 0.83 |
| Max Cruise Speed (ktas) | 470 | 533 | 476 |
| Long Range Cruise (Mach) | 0.78 | 0.8 | 0.77 |
| Long Range Cruise (ktas) | 447 | 458 | 440 |
| Vref (kias) | - | 111 | 102 |
| Max Range (nm) | 6000 | 3400 | 4018 |
| Max Range Crew + 4 (nm) | 6000 | 3400 | 4018 |
| Max Range Crew + 6 (nm) | 6000 | 3400 | - |
| Max Range Crew + 8 (nm) | 6000 | 3250 | - |
| Take-off FL (ft) | 5020 | 4835 | 4717 |
| Landing Roll (ft) | 2850 | 2364 | 2165 |
| Max Climb Rate (fpm) | - | 5000 | - |
| Service Ceiling (ft) | 41000 | 45000 | 45000 |