Compare Airbus ACJ TwoTwenty vs Bombardier Global 5500 vs Bombardier Global 7500 vs Dassault Falcon 6X
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| Manufacturer | Airbus | Bombardier | Bombardier | Dassault Falcon |
| Aircraft Type | ACJ TwoTwenty | Global 5500 | Global 7500 | 6X |
| Base Aircraft Price (USD) | $80,000,000 | $46,000,000 | $75,000,000 | $49,500,000 |
| Direct Operating Cost | - | $ 4,895 | $ 4,900 | $ 3,845 |
| DOC / nm | - | $ 9.49 | $ 9.50 | $ 7.74 |
| DOC / nm / Seat | - | $ 0.79 | $ 0.79 | $ 0.64 |
| Max Cruise Speed (ktas) | 470 | 504 | 516 | 516 |
| Max Range (nm) | 5650 | 5700 | 7700 | 5500 |
| Total Seats | 16 | 14 | 14 | 17 |
| Cockpit | 2 | 2 | 2 | 3 |
| Standard Cabin Seats | - | 12 | 12 | 14 |
| Max Cabin Seats | 18 | 16 | 19 | 16 |
| Min Crew | 2 | 2 | 2 | 2 |
| Flight Deck (Base Spec) | Thales | Bombardier Vision (Pro Line Fusion) | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy III |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Weights | ||||
| MRAMP (lbs) | - | 92750 | - | 77260 |
| MTOW (lbs) | - | 92500 | - | 77460 |
| MLW (lbs) | - | 78600 | - | 66190 |
| MZFW (lbs) | - | 58000 | - | 45920 |
| BOW (lbs) | - | 50861 | - | - |
| Fuel Capacity (lbs) | - | 39250 | - | 33790 |
| Useful Load Max Fuel (lbs) | - | 7139 | - | - |
| Max Baggage Weight (lbs) | - | - | - | 2004 |
| Dimensions | ||||
| Wingspan (ft) | - | 94 | 104 | 85.1 |
| Overall Height (ft) | - | 25.5 | 27 | 24.5 |
| Length (ft) | - | 96 | 111 | 84.3 |
| Cabin Height (ft) | - | 6.2 | 6.2 | 6.5 |
| Cabin Width (ft) | - | 8 | 8 | 8.5 |
| Cabin Width - Floor (ft) | - | - | - | 6.3 |
| Cabin Length (ft) | - | 40.8 | 54.5 | 40.4 |
| Cabin Length - Seating (ft) | - | - | - | 27.5 |
| Cabin Volume (cu. ft) | - | - | - | 1843 |
| Baggage Volume Int. (cu. ft) | - | - | - | 140 |
| Engine | ||||
| No. of Engines | - | 2 | 2 | 2 |
| Manufacturer | Airbus | Bombardier | Bombardier | Dassault Falcon |
| Model | - | Pearl | Passport | PW812D |
| Thrust (lbs) | - | 15125 | 18920 | 14000 |
| Flat Rating | - | - | ISA + 15 | ISA + 17 |
| FADEC | - | Yes | Yes | Yes |
| TBO (hrs) | - | On-Condition | On-Condition | 5000 |
| Avionics | ||||
| Flight Deck | Rockwell Collins ProLine Fusion | Bombardier Vision (Pro Line Fusion) | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy III |
| FMS | - | 1 | 3 | 3 |
| Autopilot | - | 1 | 2 | 2 |
| PFD | - | 2 | 2 | 2 |
| MFD | - | 2 | 2 | 2 |
| GPS | - | 2 | 3 | 3 |
| AHRS | - | 2 | 2 | 1 |
| ADC | - | 2 | 2 | - |
| Transponder | - | 2 | 2 | 2 |
| VHF Com | - | 2 | 3 | 3 |
| VHF NAV | - | 2 | 3 | 3 |
| Cabin | ||||
| Total Seats | 16 | 14 | 14 | 17 |
| Cockpit | 2 | 2 | 2 | 3 |
| Standard Cabin Seats | - | 12 | 12 | 14 |
| Max Cabin Seats | 18 | 16 | 19 | 16 |
| Min Crew | 2 | 2 | 2 | 2 |
| Lavatory | - | 2 Enclosed Flushing | 2 Enclosed Flushing | 2 Enclosed Flushing |
| Lavatory Location | - | FWD / AFT | FWD / AFT | FWD / AFT |
| Galley / Refreshment | - | Galley | Galley | Galley |
| Galley Location | - | FWD | FWD | FWD |
| Crew Rest | - | No | Yes | No |
| Jump Seat | - | Yes | Yes | Yes |
| Max Cabin Altitude (ft) | - | - | 4500 | 3900 |
| SL Cabin Altitude (ft) | - | - | - | 29200 |
| Cabin Pressure (psi) | - | - | - | 10.2 |
| 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) | - | 0.88 | 0.9 | 0.9 |
| Max Cruise Speed (ktas) | 470 | 504 | 516 | 516 |
| Long Range Cruise (Mach) | - | 0.85 | 0.85 | 0.8 |
| Long Range Cruise (ktas) | - | 487 | 487 | 458 |
| Vref (kias) | - | - | - | 106 |
| Max Range (nm) | 5650 | 5700 | 7700 | 5500 |
| Max Range Crew + 4 (nm) | - | 5700 | 7700 | 5500 |
| Max Range Crew + 6 (nm) | - | 5700 | 7700 | - |
| Max Range Crew + 8 (nm) | - | 5700 | 7700 | - |
| Take-off FL (ft) | - | 5490 | 5800 | 5480 |
| Take-Off (5000 / ISA + 10) | - | - | - | 7815 |
| Landing Roll (ft) | - | 2207 | 2520 | 2480 |
| Service Ceiling (ft) | - | 51000 | 51000 | 51000 |