Compare Airbus ACJ320 Neo vs Dassault Falcon 8X vs Dassault Falcon 900LX
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| Manufacturer | Airbus | Dassault Falcon | Dassault Falcon |
| Aircraft Type | ACJ320 | 8X | 900LX |
| Base Aircraft Price (USD) | $96,000,000 | $ 62,500,000 | $44,000,000 |
| Direct Operating Cost | $ 6,926 | $ 3,805 | $ 3,588 |
| DOC / nm | $ 14.74 | $ 7.66 | $ 7.57 |
| DOC / nm / Seat | $ 1.84 | $ 0.64 | $ 0.63 |
| Max Cruise Speed (ktas) | 470 | 516 | 498 |
| Max Range (nm) | 6750 | 6450 | 4750 |
| Useful Load (lbs) | 32500 | 36900 | 22450 |
| Total Seats | 10 | 17 | 16 |
| Cockpit | 2 | 3 | 2 |
| Standard Cabin Seats | 8 | 14 | 14 |
| Max Cabin Seats | 35 | 16 | 14 |
| Min Crew | 4 | 2 | 2 |
| Flight Deck (Base Spec) | Thales | Honeywell Primus EASy II | Honeywell Primus EASy II |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Weights | |||
| MRAMP (lbs) | - | 73200 | 49200 |
| MTOW (lbs) | 172400 | 73000 | 49000 |
| MLW (lbs) | 140850 | 62400 | 44500 |
| MZFW (lbs) | 116850 | 41000 | 30864 |
| BOW (lbs) | 102000 | 36100 | 26750 |
| BEW (lbs) | - | 36100 | 26550 |
| Useful Load (lbs) | 32500 | 36900 | 22450 |
| Max Payload (lbs) | - | 4560 | 4114 |
| Fuel Capacity (lbs) | 66000 | 35141 | 21000 |
| Payload Max Fuel (lbs) | - | 1759 | 1545 |
| Max Baggage Weight (lbs) | - | 2004 | 2866 |
| Dimensions | |||
| Wingspan (ft) | 117.5 | 86.3 | 70.2 |
| Overall Height (ft) | 38.58 | 26.1 | 24.8 |
| Length (ft) | 111 | 80.2 | 66.4 |
| Cabin Height (ft) | 7.4 | 6.2 | 6.2 |
| Cabin Width (ft) | 12.1 | 7.7 | 7.7 |
| Cabin Width - Floor (ft) | - | 6.3 | 6.3 |
| Cabin Length (ft) | 78.8 | 42.7 | 33.2 |
| Cabin Length - Seating (ft) | - | 29.2 | 23.5 |
| Cabin Volume (cu. ft) | 6710 | 1695 | 1264 |
| Baggage Volume Int. (cu. ft) | - | 140 | 127 |
| Baggage Volume Ext. (cu. ft) | 943 | - | - |
| Engine | |||
| No. of Engines | 2 | 3 | 3 |
| Manufacturer | Airbus | Dassault Falcon | Dassault Falcon |
| Model | CFM LEAP-1A27 | PW307D | TFE731-60 |
| Thrust (lbs) | 27000 | 6722 | 5000 |
| Flat Rating | - | ISA + 17 | ISA + 17 |
| FADEC | Yes | Yes | Yes |
| TBO (hrs) | On-Condition | On-Condition | 5000 |
| Avionics | |||
| Flight Deck | Thales | Honeywell Primus EASy II | Honeywell Primus EASy II |
| FMS | 3 | 3 | 3 |
| Autopilot | 2 | 2 | 2 |
| PFD | 2 | 2 | 2 |
| MFD | 2 | 2 | 2 |
| GPS | 3 | 3 | 3 |
| AHRS | 1 | 1 | 1 |
| Transponder | 2 | 2 | 2 |
| VHF Com | 3 | 3 | 3 |
| VHF NAV | 3 | 3 | 3 |
| Cabin | |||
| Total Seats | 10 | 17 | 16 |
| Cockpit | 2 | 3 | 2 |
| Standard Cabin Seats | 8 | 14 | 14 |
| Max Cabin Seats | 35 | 16 | 14 |
| Min Crew | 4 | 2 | 2 |
| Configuration | Green Interior | - | - |
| Lavatory | - | 2 Enclosed Flushing | 1 Enclosed Flushing |
| Lavatory Location | - | FWD / AFT | AFT |
| Galley / Refreshment | - | Galley | Galley |
| Galley Location | - | FWD | FWD |
| Crew Rest | - | No | No |
| Jump Seat | - | Yes | No |
| Max Cabin Altitude (ft) | - | 3900 | - |
| SL Cabin Altitude (ft) | - | 29200 | 25300 |
| Cabin Pressure (psi) | - | 10.2 | 9.6 |
| 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 | 0.9 | 0.87 |
| Max Cruise Speed (ktas) | 470 | 516 | 498 |
| Long Range Cruise (Mach) | 0.78 | 0.85 | 0.8 |
| Long Range Cruise (ktas) | 447 | 487 | 458 |
| Vref (kias) | - | 106 | 111 |
| Max Range (nm) | 6750 | 6450 | 4750 |
| Max Range Crew + 4 (nm) | 6750 | 6450 | 4650 |
| Max Range Crew + 6 (nm) | 6750 | - | - |
| Max Range Crew + 8 (nm) | 6750 | - | - |
| Take-off FL (ft) | 5400 | 5910 | 5360 |
| Take-Off (5000 / ISA + 10) | - | 8245 | 6715 |
| Landing Roll (ft) | 2680 | 2240 | 2415 |
| Max Climb Rate (fpm) | - | 2055 | 2055 |
| Service Ceiling (ft) | 41000 | 51000 | 51000 |