Compare Bombardier Global 5500 vs Dassault Falcon 900LX vs Gulfstream G400
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| Manufacturer | Bombardier | Dassault Falcon | Gulfstream |
| Aircraft Type | Global 5500 | 900LX | G400 |
| Base Aircraft Price (USD) | $46,000,000 | $44,000,000 | 34500000 |
| Direct Operating Cost | $ 4,895 | $ 3,588 | - |
| DOC / nm | $ 9.49 | $ 7.57 | - |
| DOC / nm / Seat | $ 0.79 | $ 0.63 | - |
| Max Cruise Speed (ktas) | 504 | 498 | 539 |
| Max Range (nm) | 5700 | 4750 | 4200 |
| Useful Load (lbs) | - | 22450 | 30650 |
| Total Seats | 14 | 16 | 12 |
| Cockpit | 2 | 2 | - |
| Standard Cabin Seats | 12 | 14 | - |
| Max Cabin Seats | 16 | 14 | 19 |
| Min Crew | 2 | 2 | 4 |
| Flight Deck (Base Spec) | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck |
| Certification | FAA / EASA | FAA / EASA | - |
| OEM Verification | VERIFIED | VERIFIED | - |
| Weights | |||
| MRAMP (lbs) | 92750 | 49200 | - |
| MTOW (lbs) | 92500 | 49000 | - |
| MLW (lbs) | 78600 | 44500 | - |
| MZFW (lbs) | 58000 | 30864 | - |
| BOW (lbs) | 50861 | 26750 | - |
| BEW (lbs) | - | 26550 | - |
| Useful Load (lbs) | - | 22450 | 30650 |
| Max Payload (lbs) | - | 4114 | - |
| Fuel Capacity (lbs) | 39250 | 21000 | - |
| Useful Load Max Fuel (lbs) | 7139 | - | - |
| Payload Max Fuel (lbs) | - | 1545 | - |
| Max Baggage Weight (lbs) | - | 2866 | - |
| Dimensions | |||
| Wingspan (ft) | 94 | 70.2 | - |
| Overall Height (ft) | 25.5 | 24.8 | - |
| Length (ft) | 96 | 66.4 | - |
| Cabin Height (ft) | 6.2 | 6.2 | - |
| Cabin Width (ft) | 8 | 7.7 | - |
| Cabin Width - Floor (ft) | - | 6.3 | - |
| Cabin Length (ft) | 40.8 | 33.2 | - |
| Cabin Length - Seating (ft) | - | 23.5 | - |
| Cabin Volume (cu. ft) | - | 1264 | - |
| Baggage Volume Int. (cu. ft) | - | 127 | - |
| Engine | |||
| No. of Engines | 2 | 3 | - |
| Manufacturer | Bombardier | Dassault Falcon | Gulfstream |
| Model | Pearl | TFE731-60 | - |
| Thrust (lbs) | 15125 | 5000 | - |
| Flat Rating | - | ISA + 17 | - |
| FADEC | Yes | Yes | - |
| TBO (hrs) | On-Condition | 5000 | - |
| Avionics | |||
| Flight Deck | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy II | - |
| 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 | 16 | 12 |
| Cockpit | 2 | 2 | - |
| Standard Cabin Seats | 12 | 14 | - |
| Max Cabin Seats | 16 | 14 | 19 |
| Min Crew | 2 | 2 | 4 |
| 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 | - |
| SL Cabin Altitude (ft) | - | 25300 | - |
| Cabin Pressure (psi) | - | 9.6 | - |
| 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 | 0.87 | - |
| Max Cruise Speed (ktas) | 504 | 498 | 539 |
| Long Range Cruise (Mach) | 0.85 | 0.8 | - |
| Long Range Cruise (ktas) | 487 | 458 | - |
| Vref (kias) | - | 111 | - |
| Max Range (nm) | 5700 | 4750 | 4200 |
| Max Range Crew + 4 (nm) | 5700 | 4650 | - |
| Max Range Crew + 6 (nm) | 5700 | - | - |
| Max Range Crew + 8 (nm) | 5700 | - | - |
| Take-off FL (ft) | 5490 | 5360 | - |
| Take-Off (5000 / ISA + 10) | - | 6715 | - |
| Landing Roll (ft) | 2207 | 2415 | - |
| Max Climb Rate (fpm) | - | 2055 | - |
| Service Ceiling (ft) | 51000 | 51000 | - |