Bombardier Challenger 650 vs Dassault Falcon 2000s vs Embraer Praetor 600
All three are super-midsize business jets, but they differ in reach and cabin count. The Bombardier Challenger 650 is typically positioned as a super-midsize with a notably wide cabin and a common seating configuration around 10–12 passengers; its range is about 4,000 nautical miles, making it well suited for transcontinental U.S. flying and many North Atlantic city pairs with favorable conditions. The Dassault Falcon 2000S is often described as a large-cabin/super-midsize crossover, generally seating about 8–10 in typical executive layouts (with higher-density options), and offers roughly 3,350 nautical miles of range, emphasizing runway performance and operational flexibility over maximum distance. The Embraer Praetor 600 is a super-midsize jet usually configured for about 8–12 passengers and delivers the longest range of the three at roughly 4,018 nautical miles, pairing that reach with modern avionics and efficient cruise performance. Overall, for maximum range the Praetor 600 leads slightly, the Challenger 650 is close with a spacious cabin, and the Falcon 2000S trades some range for robust short-field capability and a larger-airframe feel.
| Spec | Bombardier Challenger 650 | Dassault Falcon 2000S | Embraer Praetor 600 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 7.16 | $ 6.63 | $ 6.74 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 11 | 12 | 10 |
| Manufacturer | Bombardier | Dassault Falcon | Embraer |
| Aircraft Name | Challenger 650 | 2000S | Praetor 600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 4085 | 3540 | 4018 |
| DOC / nm / Seat | $ 0.80 | $ 0.83 | $ 0.84 |
| Max Cabin Seats | 12 | 10 | 12 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 21050 | 18250 | — |
| Standard Cabin Seats | 9 | 10 | 8 |
| Direct Operating Cost | $ 3,365 | $ 3,150 | $ 3,141 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 Advanced | Honeywell Primus EASy II | Rockwell Collins Pro Line Fusion |
| Max Cruise Speed (ktas) | 470 | 490 | 542 |
| Base Aircraft Price (USD) | $32,400,000 | $ 26,000,000 | $20,995,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | 1 Enclosed Flushing | 1 Enclosed Belted Flushing |
| Min Crew | 2 | 2 | 2 |
| Crew Rest | Yes | No | No |
| Jump Seat | Yes | No | No |
| Total Seats | 11 | 12 | 10 |
| Galley Location | FWD | FWD | FWD |
| Max Cabin Seats | 12 | 10 | 12 |
| Lavatory Location | FWD / AFT | AFT | AFT |
| Cabin Pressure (psi) | 8.8 | 9.6 | 9.7 |
| Galley / Refreshment | Galley | Galley | Galley |
| Standard Cabin Seats | 9 | 10 | 8 |
| SL Cabin Altitude (ft) | 23000 | 25300 | 27140 |
| Connectivity | — | — | Gogo AVANCE L5 |
| Max Cabin Altitude (ft) | — | — | 5800 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | CF34-3B MTO | PW308C | HTF7500E |
| TBO (hrs) | On-Condition | 7000 | On-Condition |
| Flat Rating | ISA + 15 | ISA + 15 | ISA + 18 |
| Thrust (lbs) | 9220 | 7000 | 7528 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | — | — | 1963 |
| Dimensions | |||
| Length (ft) | 68.4 | 66.4 | 68.1 |
| Wingspan (ft) | 64.4 | 70.2 | 70.5 |
| Aisle Step (ft) | Flat Floor | Flat Floor | Flat Floor |
| Cabin Width (ft) | 7.9 | 7.7 | 6.8 |
| Cabin Height (ft) | 6 | 6.2 | 6 |
| Cabin Length (ft) | 25.6 | 26.2 | 24.1 |
| Overall Height (ft) | 20.7 | 23.2 | 21 |
| Cabin Width - Floor (ft) | 6.9 | 6.3 | 4.7 |
| Cabin Length - Seating (ft) | 15.4 | 17.1 | 21.3 |
| Baggage Volume Int. (cu. ft) | 112 | 134 | 45 |
| Cabin Volume (cu. ft) | — | 1024 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 110 |