Compare Bombardier Challenger 650 vs Bombardier Global 5500 vs Dassault Falcon 6X vs Gulfstream G400 vs Gulfstream G500
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| Manufacturer | Bombardier | Bombardier | Dassault Falcon | Gulfstream | Gulfstream |
| Aircraft Type | Challenger 650 | Global 5500 | 6X | G400 | G500 |
| Base Aircraft Price (USD) | $32,400,000 | $46,000,000 | $49,500,000 | 34500000 | $47,500,000 |
| Direct Operating Cost | $ 3,365 | $ 4,895 | $ 3,845 | - | $ 4,644 |
| DOC / nm | $ 7.16 | $ 9.49 | $ 7.74 | - | $ 9.00 |
| DOC / nm / Seat | $ 0.80 | $ 0.79 | $ 0.64 | - | $ 0.90 |
| Max Cruise Speed (ktas) | 470 | 504 | 516 | 539 | 516 |
| Max Range (nm) | 4085 | 5700 | 5500 | 4200 | 5200 |
| Useful Load (lbs) | 21050 | - | - | 30650 | 30650 |
| Total Seats | 11 | 14 | 17 | 12 | 12 |
| Cockpit | 2 | 2 | 3 | - | 2 |
| Standard Cabin Seats | 9 | 12 | 14 | - | 10 |
| Max Cabin Seats | 12 | 16 | 16 | 19 | 19 |
| Min Crew | 2 | 2 | 2 | 4 | 4 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 Advanced | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy III | Gulfstream Symmetry Flight Deck | Gulfstream Symmetry Flight Deck |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | - | In Development |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | - | Un-Verified |
| Weights | |||||
| MRAMP (lbs) | 48300 | 92750 | 77260 | - | 77250 |
| MTOW (lbs) | 48200 | 92500 | 77460 | - | 79600 |
| MLW (lbs) | 38000 | 78600 | 66190 | - | 64350 |
| MZFW (lbs) | 32000 | 58000 | 45920 | - | 52100 |
| BOW (lbs) | 27250 | 50861 | - | - | 46850 |
| BEW (lbs) | 27150 | - | - | - | - |
| Useful Load (lbs) | 21050 | - | - | 30650 | 30650 |
| Max Payload (lbs) | 3750 | - | - | - | 5500 |
| Fuel Capacity (lbs) | 19852 | 39250 | 33790 | - | 28850 |
| Useful Load Max Fuel (lbs) | - | 7139 | - | - | - |
| Payload Max Fuel (lbs) | 1198 | - | - | - | 1800 |
| Max Baggage Weight (lbs) | 900 | - | 2004 | - | 2250 |
| Dimensions | |||||
| Wingspan (ft) | 64.4 | 94 | 85.1 | - | 86.3 |
| Overall Height (ft) | 20.7 | 25.5 | 24.5 | - | 25.5 |
| Length (ft) | 68.4 | 96 | 84.3 | - | 91.2 |
| Cabin Height (ft) | 6 | 6.2 | 6.5 | - | 6.4 |
| Aisle Step (ft) | Flat Floor | - | - | - | Flat Floor |
| Cabin Width (ft) | 7.9 | 8 | 8.5 | - | 7.6 |
| Cabin Width - Floor (ft) | 6.9 | - | 6.3 | - | 6.1 |
| Cabin Length (ft) | 25.6 | 40.8 | 40.4 | - | 41.5 |
| Cabin Length - Seating (ft) | 15.4 | - | 27.5 | - | 26.3 |
| Cabin Volume (cu. ft) | - | - | 1843 | - | - |
| Baggage Volume Int. (cu. ft) | 112 | - | 140 | - | 230 |
| Engine | |||||
| No. of Engines | 2 | 2 | 2 | - | 2 |
| Manufacturer | Bombardier | Bombardier | Dassault Falcon | Gulfstream | Gulfstream |
| Model | CF34-3B MTO | Pearl | PW812D | - | PW814GA |
| Thrust (lbs) | 9220 | 15125 | 14000 | - | 15144 |
| Flat Rating | ISA + 15 | - | ISA + 17 | - | ISA + 15 |
| FADEC | Yes | Yes | Yes | - | Yes |
| TBO (hrs) | On-Condition | On-Condition | 5000 | - | 10000 |
| Avionics | |||||
| Flight Deck | Rockwell Collins Pro Line 21 Advanced | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy III | - | Gulfstream Symmetry Flight Deck |
| FMS | 2 | 1 | 3 | - | 3 |
| Autopilot | 1 | 1 | 2 | - | 2 |
| PFD | 2 | 2 | 2 | - | 2 |
| MFD | 2 | 2 | 2 | - | 2 |
| GPS | 2 | 2 | 3 | - | 3 |
| AHRS | 2 | 2 | 1 | - | 1 |
| ADC | 2 | 2 | - | - | - |
| Transponder | 2 | 2 | 2 | - | 2 |
| VHF Com | 2 | 2 | 3 | - | 3 |
| VHF NAV | 2 | 2 | 3 | - | 3 |
| Cabin | |||||
| Total Seats | 11 | 14 | 17 | 12 | 12 |
| Cockpit | 2 | 2 | 3 | - | 2 |
| Standard Cabin Seats | 9 | 12 | 14 | - | 10 |
| Max Cabin Seats | 12 | 16 | 16 | 19 | 19 |
| Min Crew | 2 | 2 | 2 | 4 | 4 |
| Lavatory | 2 Enclosed Flushing | 2 Enclosed Flushing | 2 Enclosed Flushing | - | 2 Enclosed Flushing |
| Lavatory Location | FWD / AFT | FWD / AFT | FWD / AFT | - | FWD / AFT |
| Galley / Refreshment | Galley | Galley | Galley | - | Galley |
| Galley Location | FWD | FWD | FWD | - | FWD |
| Crew Rest | Yes | No | No | - | No |
| Jump Seat | Yes | Yes | Yes | - | Yes |
| Max Cabin Altitude (ft) | - | - | 3900 | - | - |
| SL Cabin Altitude (ft) | 23000 | - | 29200 | - | 31900 |
| Cabin Pressure (psi) | 8.8 | - | 10.2 | - | 10.7 |
| Other | |||||
| APU Manufacturer | - | - | - | - | - |
| APU Model | - | - | - | - | - |
| APU TBO (hrs) | - | - | - | - | - |
| Warranty | |||||
| Airframe (Yrs) | 3 | 3 | 3 | - | 3 |
| Airframe (Hrs) | 1000 | 1000 | 1000 | - | 1000 |
| Engine (Yrs) | 2 | 2 | 2 | - | 2 |
| Engine (Hrs) | 1000 | 1000 | 1000 | - | 1000 |
| APU (Hrs) | 2000 | 2000 | 2000 | - | 2000 |
| Performance | |||||
| Max Cruise Speed (Mach) | 0.82 | 0.88 | 0.9 | - | 0.9 |
| Max Cruise Speed (ktas) | 470 | 504 | 516 | 539 | 516 |
| Long Range Cruise (Mach) | 0.8 | 0.85 | 0.8 | - | 0.85 |
| Long Range Cruise (ktas) | 458 | 487 | 458 | - | 487 |
| Vref (kias) | 117 | - | 106 | - | - |
| Max Range (nm) | 4085 | 5700 | 5500 | 4200 | 5200 |
| Max Range Crew + 4 (nm) | 4011 | 5700 | 5500 | - | 5200 |
| Max Range Crew + 6 (nm) | 4011 | 5700 | - | - | 5200 |
| Max Range Crew + 8 (nm) | - | 5700 | - | - | 5200 |
| Take-off FL (ft) | 5640 | 5490 | 5480 | - | 5200 |
| Take-Off (5000 / ISA + 10) | - | - | 7815 | - | - |
| Landing Roll (ft) | 2402 | 2207 | 2480 | - | 3100 |
| Max Climb Rate (fpm) | 4345 | - | - | - | - |
| Service Ceiling (ft) | 41000 | 51000 | 51000 | - | 51000 |