Bombardier Challenger 650 vs Dassault Falcon 2000s vs Dassault Falcon 900lx vs Gulfstream G280
In category, the Bombardier Challenger 650 is typically considered a super-midsize business jet with a wide, “large-cabin” cross-section feel, while the Gulfstream G280 is also in the super-midsize class but is generally positioned as a high-performance, long-range super-midsize. The Dassault Falcon 2000S is commonly grouped in the large-cabin/light-long-range category (a smaller large-cabin twinjet), whereas the Dassault Falcon 900LX is a true large-cabin, long-range trijet. On range, the Challenger 650 and Falcon 2000S sit in the mid-to-upper 3,000 nm class depending on mission and payload, while the G280 typically stretches further into the upper 3,000 to about 4,000 nm class. The Falcon 900LX leads this group, reaching into roughly the 4,000+ nm class, enabling more nonstop transoceanic or deep intercontinental segments. For passenger capacity, all can be configured for around 8 to 12 passengers in typical layouts, but the larger Falcons—especially the 900LX—more often support higher-density or multi-zone cabin configurations, while the Challenger 650 and G280 are most commonly optimized for 8–10 in comfort.
| Spec | Bombardier Challenger 650 | Dassault Falcon 2000S | Dassault Falcon 900LX | Gulfstream G280 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 7.16 | $ 6.63 | $ 7.57 | $ 6.57 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 11 | 12 | 16 | 10 |
| Manufacturer | Bombardier | Dassault Falcon | Dassault Falcon | Gulfstream |
| Aircraft Name | Challenger 650 | 2000S | 900LX | G280 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 4085 | 3540 | 4750 | 3600 |
| DOC / nm / Seat | $ 0.80 | $ 0.83 | $ 0.63 | $ 0.82 |
| Max Cabin Seats | 12 | 10 | 14 | 10 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 21050 | 18250 | 22450 | 15550 |
| Standard Cabin Seats | 9 | 10 | 14 | 8 |
| Direct Operating Cost | $ 3,365 | $ 3,150 | $ 3,588 | $ 3,168 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 Advanced | Honeywell Primus EASy II | Honeywell Primus EASy II | Gulfstream PlaneView (Pro Line Fusion) |
| Max Cruise Speed (ktas) | 470 | 490 | 498 | 481 |
| Base Aircraft Price (USD) | $32,400,000 | $ 26,000,000 | $44,000,000 | $24,900,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | 1 Enclosed Flushing | 1 Enclosed Flushing | 1 Enclosed Belted Flushing |
| Min Crew | 2 | 2 | 2 | 2 |
| Crew Rest | Yes | No | No | No |
| Jump Seat | Yes | No | No | No |
| Total Seats | 11 | 12 | 16 | 10 |
| Galley Location | FWD | FWD | FWD | FWD |
| Max Cabin Seats | 12 | 10 | 14 | 10 |
| Lavatory Location | FWD / AFT | AFT | AFT | AFT |
| Cabin Pressure (psi) | 8.8 | 9.6 | 9.6 | 9.2 |
| Galley / Refreshment | Galley | Galley | Galley | Galley |
| Standard Cabin Seats | 9 | 10 | 14 | 8 |
| SL Cabin Altitude (ft) | 23000 | 25300 | 25300 | 25000 |
| Max Cabin Altitude (ft) | — | — | — | 5800 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | CF34-3B MTO | PW308C | TFE731-60 | HTF7250G |
| TBO (hrs) | On-Condition | 7000 | 5000 | On-Condition |
| Flat Rating | ISA + 15 | ISA + 15 | ISA + 17 | ISA + 17 |
| Thrust (lbs) | 9220 | 7000 | 5000 | 7624 |
| No. of Engines | 2 | 2 | 3 | 2 |
| Dimensions | ||||
| Length (ft) | 68.4 | 66.4 | 66.4 | 66.9 |
| Wingspan (ft) | 64.4 | 70.2 | 70.2 | 63 |
| Aisle Step (ft) | Flat Floor | Flat Floor | — | 0.3 |
| Cabin Width (ft) | 7.9 | 7.7 | 7.7 | 6.9 |
| Cabin Height (ft) | 6 | 6.2 | 6.2 | 6.3 |
| Cabin Length (ft) | 25.6 | 26.2 | 33.2 | 25.9 |
| Overall Height (ft) | 20.7 | 23.2 | 24.8 | 21.4 |
| Cabin Width - Floor (ft) | 6.9 | 6.3 | 6.3 | 5.4 |
| Cabin Length - Seating (ft) | 15.4 | 17.1 | 23.5 | 17.7 |
| Baggage Volume Int. (cu. ft) | 112 | 134 | 127 | 154 |
| Cabin Volume (cu. ft) | — | 1024 | 1264 | — |