Compare Bombardier Global 5500 vs Dassault Falcon 10X vs Dassault Falcon 6X vs Gulfstream G800
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| Manufacturer | Bombardier | Dassault Falcon | Dassault Falcon | Gulfstream |
| Aircraft Type | Global 5500 | 10X | 6X | G750 |
| Base Aircraft Price (USD) | $46,000,000 | $ 75,000,000 | $49,500,000 | 71500000 |
| Direct Operating Cost | $ 4,895 | $2,770 | $ 3,845 | - |
| DOC / nm | $ 9.49 | - | $ 7.74 | - |
| DOC / nm / Seat | $ 0.79 | - | $ 0.64 | - |
| Max Cruise Speed (ktas) | 504 | 516 | 516 | 982 |
| Max Range (nm) | 5700 | 7505 | 5500 | 8000 |
| Useful Load (lbs) | - | 36900 | - | - |
| Total Seats | 14 | 17 | 17 | 12 |
| Cockpit | 2 | 2 | 3 | - |
| Standard Cabin Seats | 12 | 14 | 14 | - |
| Max Cabin Seats | 16 | 16 | 16 | - |
| Min Crew | 2 | 2 | 2 | - |
| Flight Deck (Base Spec) | Bombardier Vision (Pro Line Fusion) | Digital Flight Control System | Honeywell Primus EASy III | - |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | - |
| OEM Verification | 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 | - | 85.1 | - |
| Overall Height (ft) | 25.5 | - | 24.5 | - |
| Length (ft) | 96 | - | 84.3 | - |
| Cabin Height (ft) | 6.2 | - | 6.5 | - |
| Cabin Width (ft) | 8 | - | 8.5 | - |
| Cabin Width - Floor (ft) | - | - | 6.3 | - |
| Cabin Length (ft) | 40.8 | - | 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 | - |
| Manufacturer | Bombardier | Dassault Falcon | Dassault Falcon | Gulfstream |
| Model | Pearl | - | PW812D | - |
| Thrust (lbs) | 15125 | - | 14000 | - |
| Flat Rating | - | - | ISA + 17 | - |
| FADEC | Yes | - | Yes | - |
| TBO (hrs) | On-Condition | - | 5000 | - |
| Avionics | ||||
| Flight Deck | Bombardier Vision (Pro Line Fusion) | NeXus | Honeywell Primus EASy III | - |
| FMS | 1 | - | 3 | - |
| Autopilot | 1 | - | 2 | - |
| PFD | 2 | - | 2 | - |
| MFD | 2 | - | 2 | - |
| GPS | 2 | - | 3 | - |
| AHRS | 2 | - | 1 | - |
| ADC | 2 | - | - | - |
| Transponder | 2 | - | 2 | - |
| VHF Com | 2 | - | 3 | - |
| VHF NAV | 2 | - | 3 | - |
| Cabin | ||||
| Total Seats | 14 | 17 | 17 | 12 |
| Cockpit | 2 | 2 | 3 | - |
| Standard Cabin Seats | 12 | 14 | 14 | - |
| Max Cabin Seats | 16 | 16 | 16 | - |
| Min Crew | 2 | 2 | 2 | - |
| Lavatory | 2 Enclosed Flushing | - | 2 Enclosed Flushing | - |
| Lavatory Location | FWD / AFT | - | FWD / AFT | - |
| Galley / Refreshment | Galley | - | Galley | - |
| Galley Location | FWD | - | FWD | - |
| Crew Rest | No | - | No | - |
| Jump Seat | Yes | - | 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) | 0.88 | .925 | 0.9 | - |
| Max Cruise Speed (ktas) | 504 | 516 | 516 | 982 |
| Long Range Cruise (Mach) | 0.85 | - | 0.8 | - |
| Long Range Cruise (ktas) | 487 | - | 458 | - |
| Vref (kias) | - | - | 106 | - |
| Max Range (nm) | 5700 | 7505 | 5500 | 8000 |
| Max Range Crew + 4 (nm) | 5700 | - | 5500 | - |
| Max Range Crew + 6 (nm) | 5700 | - | - | - |
| Max Range Crew + 8 (nm) | 5700 | - | - | - |
| Take-off FL (ft) | 5490 | - | 5480 | - |
| Take-Off (5000 / ISA + 10) | - | - | 7815 | - |
| Landing Roll (ft) | 2207 | - | 2480 | - |
| Service Ceiling (ft) | 51000 | - | 51000 | - |