Bombardier Challenger 650 vs Dassault Falcon 2000lxs vs Gulfstream G400 vs Gulfstream G500
The Bombardier Challenger 650 and Dassault Falcon 2000LXS are typically positioned as large-cabin business jets, while the Gulfstream G400 and G500 sit in the long-range, large-cabin segment, with the G500 generally considered the more capable step up. In range, the Challenger 650 and Falcon 2000LXS are broadly similar, each offering roughly mid–3,000-nautical-mile capability, making them well suited to transcontinental U.S. missions and many North Atlantic routes with favorable winds and payload. The Gulfstream G400 extends that envelope into the low–4,000-nautical-mile class, and the Gulfstream G500 reaches farther still, around the mid–5,000-nautical-mile class, enabling more nonstop intercontinental city pairs. For passenger capacity, all four commonly seat about 8 to 12 passengers in typical executive layouts; the Falcon 2000LXS and Challenger 650 are often configured around 8 to 10, while the G400 and G500 frequently run 10 to 14 depending on cabin zones and options. Actual performance and seating vary by configuration, payload, and conditions.
| Spec | Bombardier Challenger 650 | Dassault Falcon 2000LXS | Gulfstream G400 | Gulfstream G500 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | — | 2 |
| DOC / nm | $ 7.16 | $ 6.38 | — | $ 9.00 |
| Min Crew | 2 | 2 | 4 | 4 |
| Total Seats | 11 | 12 | 12 | 12 |
| Manufacturer | Bombardier | Dassault Falcon | Gulfstream | Gulfstream |
| Aircraft Name | Challenger 650 | 2000LXS | G400 | G500 |
| Certification | FAA / EASA | FAA / EASA | — | In Development |
| Max Range (nm) | 4085 | 4155 | 4200 | 5200 |
| DOC / nm / Seat | $ 0.80 | $ 0.80 | — | $ 0.90 |
| Max Cabin Seats | 12 | 10 | 19 | 19 |
| OEM Verification | VERIFIED | VERIFIED | — | Un-Verified |
| Useful Load (lbs) | 21050 | 18250 | 30650 | 30650 |
| Standard Cabin Seats | 9 | 10 | — | 10 |
| Direct Operating Cost | $ 3,365 | $ 3,073 | — | $ 4,644 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 Advanced | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 470 | 490 | 539 | 516 |
| Base Aircraft Price (USD) | $32,400,000 | $35,100,000 | 34500000 | $47,500,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | — | 2 |
| Lavatory | 2 Enclosed Flushing | 1 Enclosed Flushing | — | 2 Enclosed Flushing |
| Min Crew | 2 | 2 | — | 4 |
| Crew Rest | Yes | No | — | No |
| Jump Seat | Yes | No | — | Yes |
| Total Seats | 11 | 12 | — | 12 |
| Galley Location | FWD | FWD | — | FWD |
| Max Cabin Seats | 12 | 10 | — | 19 |
| Lavatory Location | FWD / AFT | AFT | — | FWD / AFT |
| Cabin Pressure (psi) | 8.8 | 9.6 | — | 10.7 |
| Galley / Refreshment | Galley | Galley | — | Galley |
| Standard Cabin Seats | 9 | 10 | — | 10 |
| SL Cabin Altitude (ft) | 23000 | 25300 | — | 31900 |
| Engine | ||||
| FADEC | Yes | Yes | — | Yes |
| Model | CF34-3B MTO | PW308C | — | PW814GA |
| TBO (hrs) | On-Condition | 7000 | — | 10000 |
| Flat Rating | ISA + 15 | ISA + 15 | — | ISA + 15 |
| Thrust (lbs) | 9220 | 7000 | — | 15144 |
| No. of Engines | 2 | 2 | — | 2 |
| Dimensions | ||||
| Length (ft) | 68.4 | 66.4 | — | 91.2 |
| Wingspan (ft) | 64.4 | 70.2 | — | 86.3 |
| Aisle Step (ft) | Flat Floor | Flat Floor | — | Flat Floor |
| Cabin Width (ft) | 7.9 | 7.7 | — | 7.6 |
| Cabin Height (ft) | 6 | 6.2 | — | 6.4 |
| Cabin Length (ft) | 25.6 | 26.2 | — | 41.5 |
| Overall Height (ft) | 20.7 | 23.2 | — | 25.5 |
| Cabin Width - Floor (ft) | 6.9 | 6.3 | — | 6.1 |
| Cabin Length - Seating (ft) | 15.4 | 17.1 | — | 26.3 |
| Baggage Volume Int. (cu. ft) | 112 | 131 | — | 230 |
| Cabin Volume (cu. ft) | — | 1024 | — | — |