Bombardier Challenger 650 vs Dassault Falcon 6x vs Embraer Legacy 650e vs Gulfstream G400
The Bombardier Challenger 650 and Embraer Legacy 650E sit in the large-cabin, long-range business jet category, with broadly similar missions focused on comfortable transcontinental flying rather than ultra-long-haul. In range terms, both are typically cited around the 3,900–4,000 nautical mile class, making them well suited to North America coast-to-coast or many Atlantic city pairs with favorable winds. Passenger capacity is usually configured for about 9 to 12, with maximum certified layouts higher. The Dassault Falcon 6X is a newer-generation large-cabin, long-range jet that steps up in both capability and cabin volume versus the Challenger/Legacy class. Its published range is commonly cited around 5,500 nautical miles, enabling more nonstop intercontinental routes, and it is generally configured for roughly 12 to 16 passengers. The Gulfstream G400 is positioned as a large-cabin, long-range aircraft between traditional super-midsize and flagship ultra-long-range models. Its published range is around 4,200 nautical miles, offering more reach than Challenger/Legacy while typically seating about 10 to 12 in executive layouts, with higher-density options available.
| Spec | Bombardier Challenger 650 | Dassault Falcon 6X | Embraer Legacy 650E | Gulfstream G400 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | — |
| DOC / nm | $ 7.16 | $ 7.74 | $ 8.41 | — |
| Min Crew | 2 | 2 | 2 | 4 |
| Total Seats | 11 | 17 | 14 | 12 |
| Manufacturer | Bombardier | Dassault Falcon | Embraer | Gulfstream |
| Aircraft Name | Challenger 650 | 6X | Legacy 650E | G400 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | — |
| Max Range (nm) | 4085 | 5500 | 3980 | 4200 |
| DOC / nm / Seat | $ 0.80 | $ 0.64 | $ 0.70 | — |
| Max Cabin Seats | 12 | 16 | 19 | 19 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | — |
| Useful Load (lbs) | 21050 | — | 22510 | 30650 |
| Standard Cabin Seats | 9 | 14 | 12 | — |
| Direct Operating Cost | $ 3,365 | $ 3,845 | $ 3,860 | — |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 Advanced | Honeywell Primus EASy III | Honeywell Primus Elite | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 470 | 516 | 458 | 539 |
| Base Aircraft Price (USD) | $32,400,000 | $49,500,000 | $26,500,000 | 34500000 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | — |
| Lavatory | 2 Enclosed Flushing | 2 Enclosed Flushing | 1 Enclosed Belted Flushing | — |
| Min Crew | 2 | 2 | 2 | — |
| Crew Rest | Yes | No | No | — |
| Jump Seat | Yes | Yes | No | — |
| Total Seats | 11 | 17 | 14 | — |
| Galley Location | FWD | FWD | FWD | — |
| Max Cabin Seats | 12 | 16 | 19 | — |
| Lavatory Location | FWD / AFT | FWD / AFT | AFT | — |
| Cabin Pressure (psi) | 8.8 | 10.2 | 8.4 | — |
| Galley / Refreshment | Galley | Galley | Galley | — |
| Standard Cabin Seats | 9 | 14 | 12 | — |
| SL Cabin Altitude (ft) | 23000 | 29200 | 21650 | — |
| Max Cabin Altitude (ft) | — | 3900 | — | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | — |
| Model | CF34-3B MTO | PW812D | AE3007A2 | — |
| TBO (hrs) | On-Condition | 5000 | On-Condition | — |
| Flat Rating | ISA + 15 | ISA + 17 | ISA + 15 | — |
| Thrust (lbs) | 9220 | 14000 | 9020 | — |
| No. of Engines | 2 | 2 | 2 | — |
| Fuel Burn (lbph) | — | — | 1901 | — |
| Dimensions | ||||
| Length (ft) | 68.4 | 84.3 | 86.5 | — |
| Wingspan (ft) | 64.4 | 85.1 | 69.5 | — |
| Aisle Step (ft) | Flat Floor | — | Flat Floor | — |
| Cabin Width (ft) | 7.9 | 8.5 | 6.9 | — |
| Cabin Height (ft) | 6 | 6.5 | 6 | — |
| Cabin Length (ft) | 25.6 | 40.4 | 42.4 | — |
| Overall Height (ft) | 20.7 | 24.5 | 22.2 | — |
| Cabin Width - Floor (ft) | 6.9 | 6.3 | 5.2 | — |
| Cabin Length - Seating (ft) | 15.4 | 27.5 | 30.3 | — |
| Baggage Volume Int. (cu. ft) | 112 | 140 | 286 | — |
| Cabin Volume (cu. ft) | — | 1843 | — | — |