Compare Airbus ACJ TwoTwenty vs Airbus ACJ320 Neo vs Dassault Falcon 7X
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| Manufacturer | Airbus | Airbus | Dassault Falcon |
| Aircraft Type | ACJ TwoTwenty | ACJ320 | 7X |
| Base Aircraft Price (USD) | $80,000,000 | $96,000,000 | $53,800,000 |
| Direct Operating Cost | - | $ 6,926 | $ 3,850 |
| DOC / nm | - | $ 14.74 | $ 7.75 |
| DOC / nm / Seat | - | $ 1.84 | $ 0.65 |
| Max Cruise Speed (ktas) | 470 | 470 | 516 |
| Max Range (nm) | 5650 | 6750 | 5950 |
| Useful Load (lbs) | - | 32500 | 33600 |
| Total Seats | 16 | 10 | 17 |
| Cockpit | 2 | 2 | 3 |
| Standard Cabin Seats | - | 8 | 14 |
| Max Cabin Seats | 18 | 35 | 16 |
| Min Crew | 2 | 4 | 2 |
| Flight Deck (Base Spec) | Thales | Thales | Honeywell Primus EASy II |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Weights | |||
| MRAMP (lbs) | - | - | 70200 |
| MTOW (lbs) | - | 172400 | 70000 |
| MLW (lbs) | - | 140850 | 62400 |
| MZFW (lbs) | - | 116850 | 41000 |
| BOW (lbs) | - | 102000 | 36600 |
| BEW (lbs) | - | - | 36400 |
| Useful Load (lbs) | - | 32500 | 33600 |
| Max Payload (lbs) | - | - | 4400 |
| Fuel Capacity (lbs) | - | 66000 | 31940 |
| Payload Max Fuel (lbs) | - | - | 1660 |
| Max Baggage Weight (lbs) | - | - | 2004 |
| Dimensions | |||
| Wingspan (ft) | - | 117.5 | 86 |
| Overall Height (ft) | - | 38.58 | 25.7 |
| Length (ft) | - | 111 | 76.7 |
| Cabin Height (ft) | - | 7.4 | 6.2 |
| Cabin Width (ft) | - | 12.1 | 7.7 |
| Cabin Width - Floor (ft) | - | - | 6.3 |
| Cabin Length (ft) | - | 78.8 | 39.1 |
| Cabin Length - Seating (ft) | - | - | 26.2 |
| Cabin Volume (cu. ft) | - | 6710 | 1552 |
| Baggage Volume Int. (cu. ft) | - | - | 140 |
| Baggage Volume Ext. (cu. ft) | - | 943 | - |
| Engine | |||
| No. of Engines | - | 2 | 3 |
| Manufacturer | Airbus | Airbus | Dassault Falcon |
| Model | - | CFM LEAP-1A27 | PW307A |
| Thrust (lbs) | - | 27000 | 6402 |
| Flat Rating | - | - | ISA + 17 |
| FADEC | - | Yes | Yes |
| TBO (hrs) | - | On-Condition | 7200 |
| Avionics | |||
| Flight Deck | Rockwell Collins ProLine Fusion | Thales | Honeywell Primus EASy II |
| FMS | - | 3 | 3 |
| Autopilot | - | 2 | 2 |
| PFD | - | 2 | 2 |
| MFD | - | 2 | 2 |
| GPS | - | 3 | 3 |
| AHRS | - | 1 | 1 |
| Transponder | - | 2 | 2 |
| VHF Com | - | 3 | 3 |
| VHF NAV | - | 3 | 3 |
| Cabin | |||
| Total Seats | 16 | 10 | 17 |
| Cockpit | 2 | 2 | 3 |
| Standard Cabin Seats | - | 8 | 14 |
| Max Cabin Seats | 18 | 35 | 16 |
| Min Crew | 2 | 4 | 2 |
| Configuration | - | Green Interior | - |
| Lavatory | - | - | 2 Enclosed Flushing |
| Lavatory Location | - | - | FWD / AFT |
| Galley / Refreshment | - | - | Galley |
| Galley Location | - | - | FWD |
| Crew Rest | - | - | No |
| Jump Seat | - | - | Yes |
| Max Cabin Altitude (ft) | - | - | 3900 |
| SL Cabin Altitude (ft) | - | - | 29200 |
| Cabin Pressure (psi) | - | - | 10.2 |
| Other | |||
| APU Manufacturer | - | - | - |
| APU Model | - | - | - |
| APU TBO (hrs) | - | - | - |
| 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 | 0.9 |
| Max Cruise Speed (ktas) | 470 | 470 | 516 |
| Long Range Cruise (Mach) | - | 0.78 | 0.8 |
| Long Range Cruise (ktas) | - | 447 | 458 |
| Vref (kias) | - | - | 106 |
| Max Range (nm) | 5650 | 6750 | 5950 |
| Max Range Crew + 4 (nm) | - | 6750 | 5950 |
| Max Range Crew + 6 (nm) | - | 6750 | 5950 |
| Max Range Crew + 8 (nm) | - | 6750 | 5950 |
| Take-off FL (ft) | - | 5400 | 5710 |
| Take-Off (5000 / ISA + 10) | - | - | 8045 |
| Landing Roll (ft) | - | 2680 | 2070 |
| Max Climb Rate (fpm) | - | - | 2055 |
| Service Ceiling (ft) | - | 41000 | 51000 |