Bombardier Challenger 650 vs Dassault Falcon 2000lxs vs Gulfstream G400 vs Gulfstream G800 1
By category, the Bombardier Challenger 650 is typically considered a large-cabin business jet, while the Dassault Falcon 2000LXS sits in the super-midsize to large-cabin class with a strong short-field and runway-performance emphasis. The Gulfstream G400 is a large-cabin, long-range jet positioned above traditional large-cabin models but below Gulfstream’s flagship ultra-long-range offerings. The Gulfstream G800 is an ultra-long-range, large-cabin flagship designed for the longest nonstop city pairs. On range, the Challenger 650 is best suited to transcontinental missions and some North Atlantic capability depending on payload and winds, whereas the Falcon 2000LXS generally offers similar “large-midsize/entry-large” mission capability with excellent access to shorter runways. The G400 steps up to true long-range flying for more consistent intercontinental missions. The G800 goes further, targeting ultra-long-range nonstop routes that exceed the practical reach of the other three. On passenger capacity, the Challenger 650 and Falcon 2000LXS commonly seat around 8 to 10 in typical executive layouts. The G400 is often configured for roughly 10 to 12. The G800 usually accommodates about 12 to 16 depending on layout.
| Spec | Bombardier Challenger 650 | Dassault Falcon 2000LXS | Gulfstream G400 | Gulfstream G800 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | — | — |
| DOC / nm | $ 7.16 | $ 6.38 | — | — |
| Min Crew | 2 | 2 | 4 | — |
| Total Seats | 11 | 12 | 12 | 15 |
| Manufacturer | Bombardier | Dassault Falcon | Gulfstream | Gulfstream |
| Aircraft Name | Challenger 650 | 2000LXS | G400 | G750 |
| Certification | FAA / EASA | FAA / EASA | — | — |
| Max Range (nm) | 4085 | 4155 | 4200 | — |
| DOC / nm / Seat | $ 0.80 | $ 0.80 | — | — |
| Max Cabin Seats | 12 | 10 | 19 | — |
| OEM Verification | VERIFIED | VERIFIED | — | — |
| Useful Load (lbs) | 21050 | 18250 | 30650 | — |
| Standard Cabin Seats | 9 | 10 | — | — |
| Direct Operating Cost | $ 3,365 | $ 3,073 | — | — |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 Advanced | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck | — |
| Max Cruise Speed (ktas) | 470 | 490 | 539 | 982 |
| Base Aircraft Price (USD) | $32,400,000 | $35,100,000 | 34500000 | 71500000 |
| Cabin | ||||
| Cockpit | 2 | 2 | — | — |
| Lavatory | 2 Enclosed Flushing | 1 Enclosed Flushing | — | — |
| Min Crew | 2 | 2 | — | — |
| Crew Rest | Yes | No | — | — |
| Jump Seat | Yes | No | — | — |
| Total Seats | 11 | 12 | — | — |
| Galley Location | FWD | FWD | — | — |
| Max Cabin Seats | 12 | 10 | — | — |
| Lavatory Location | FWD / AFT | AFT | — | — |
| Cabin Pressure (psi) | 8.8 | 9.6 | — | — |
| Galley / Refreshment | Galley | Galley | — | — |
| Standard Cabin Seats | 9 | 10 | — | — |
| SL Cabin Altitude (ft) | 23000 | 25300 | — | — |
| Engine | ||||
| FADEC | Yes | Yes | — | — |
| Model | CF34-3B MTO | PW308C | — | — |
| TBO (hrs) | On-Condition | 7000 | — | — |
| Flat Rating | ISA + 15 | ISA + 15 | — | — |
| Thrust (lbs) | 9220 | 7000 | — | — |
| No. of Engines | 2 | 2 | — | — |
| Dimensions | ||||
| Length (ft) | 68.4 | 66.4 | — | — |
| Wingspan (ft) | 64.4 | 70.2 | — | — |
| Aisle Step (ft) | Flat Floor | Flat Floor | — | — |
| Cabin Width (ft) | 7.9 | 7.7 | — | — |
| Cabin Height (ft) | 6 | 6.2 | — | — |
| Cabin Length (ft) | 25.6 | 26.2 | — | — |
| Overall Height (ft) | 20.7 | 23.2 | — | — |
| Cabin Width - Floor (ft) | 6.9 | 6.3 | — | — |
| Cabin Length - Seating (ft) | 15.4 | 17.1 | — | — |
| Baggage Volume Int. (cu. ft) | 112 | 131 | — | — |
| Cabin Volume (cu. ft) | — | 1024 | — | — |