Compare Bombardier Global 8000 vs Dassault Falcon 8X vs Gulfstream G800
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| Manufacturer | Bombardier | Dassault Falcon | Gulfstream |
| Aircraft Type | Global 8000 | 8X | G750 |
| Base Aircraft Price (USD) | $78,000,000 | $ 62,500,000 | 71500000 |
| Direct Operating Cost | $ 4,900 | $ 3,805 | - |
| DOC / nm | $ 9.50 | $ 7.66 | - |
| DOC / nm / Seat | $ 0.79 | $ 0.64 | - |
| Max Cruise Speed (ktas) | 626 | 516 | 982 |
| Max Range (nm) | 8000 | 6450 | 8000 |
| Useful Load (lbs) | - | 36900 | - |
| Total Seats | 19 | 17 | 12 |
| Cockpit | 2 | 3 | - |
| Standard Cabin Seats | 12 | 14 | - |
| Max Cabin Seats | 19 | 16 | - |
| Min Crew | 4 | 2 | - |
| Flight Deck (Base Spec) | Enhanced and Synthetic Vision Systems | Honeywell Primus EASy II | - |
| Certification | FAA / EASA | FAA / EASA | - |
| OEM Verification | VERIFIED | VERIFIED | - |
| Max Passengers | 19 | - | - |
| Weights | |||
| MRAMP (lbs) | - | 73200 | - |
| MTOW (lbs) | - | 73000 | - |
| MLW (lbs) | - | 62400 | - |
| MZFW (lbs) | - | 41000 | - |
| BOW (lbs) | - | 36100 | - |
| BEW (lbs) | - | 36100 | - |
| Useful Load (lbs) | - | 36900 | - |
| Max Payload (lbs) | - | 4560 | - |
| Fuel Capacity (lbs) | - | 35141 | - |
| Payload Max Fuel (lbs) | - | 1759 | - |
| Max Baggage Weight (lbs) | - | 2004 | - |
| Dimensions | |||
| Wingspan (ft) | 104 | 86.3 | - |
| Overall Height (ft) | 27 | 26.1 | - |
| Length (ft) | 111 | 80.2 | - |
| Cabin Height (ft) | 6.2 | 6.2 | - |
| Cabin Width (ft) | 8 | 7.7 | - |
| Cabin Width - Floor (ft) | - | 6.3 | - |
| Cabin Length (ft) | 54.5 | 42.7 | - |
| Cabin Length - Seating (ft) | - | 29.2 | - |
| Cabin Volume (cu. ft) | - | 1695 | - |
| Baggage Volume Int. (cu. ft) | - | 140 | - |
| Engine | |||
| No. of Engines | 2 | 3 | - |
| Manufacturer | Bombardier | Dassault Falcon | Gulfstream |
| Model | Passport | PW307D | - |
| Thrust (lbs) | 18920 | 6722 | - |
| Flat Rating | ISA + 15 | ISA + 17 | - |
| FADEC | Yes | Yes | - |
| TBO (hrs) | On-Condition | On-Condition | - |
| Avionics | |||
| Flight Deck | Enhanced and Synthetic Vision Systems | Honeywell Primus EASy II | - |
| FMS | 3 | 3 | - |
| Autopilot | 2 | 2 | - |
| PFD | 2 | 2 | - |
| MFD | 2 | 2 | - |
| GPS | 3 | 3 | - |
| AHRS | 2 | 1 | - |
| ADC | 2 | - | - |
| Transponder | 2 | 2 | - |
| VHF Com | 3 | 3 | - |
| VHF NAV | 3 | 3 | - |
| Cabin | |||
| Total Seats | 19 | 17 | 12 |
| Cockpit | 2 | 3 | - |
| Standard Cabin Seats | 12 | 14 | - |
| Max Cabin Seats | 19 | 16 | - |
| Min Crew | 4 | 2 | - |
| Lavatory | 2 Enclosed Flushing | 2 Enclosed Flushing | - |
| Lavatory Location | FWD / AFT | FWD / AFT | - |
| Galley / Refreshment | Galley | Galley | - |
| Galley Location | FWD | FWD | - |
| Crew Rest | Yes | No | - |
| Jump Seat | Yes | Yes | - |
| Max Cabin Altitude (ft) | 2,900 | 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) | 0.94 | 0.9 | - |
| Max Cruise Speed (ktas) | 626 | 516 | 982 |
| Long Range Cruise (Mach) | - | 0.85 | - |
| Long Range Cruise (ktas) | - | 487 | - |
| Vref (kias) | - | 106 | - |
| Max Range (nm) | 8000 | 6450 | 8000 |
| Max Range Crew + 4 (nm) | 8000 | 6450 | - |
| Take-off FL (ft) | 5760 | 5910 | - |
| Take-Off (5000 / ISA + 10) | - | 8245 | - |
| Landing Roll (ft) | 2237 | 2240 | - |
| Max Climb Rate (fpm) | - | 2055 | - |
| Service Ceiling (ft) | 51000 | 51000 | - |