Embraer Praetor 600 vs Gulfstream G400 vs Bombardier Challenger 650 vs Dassault Falcon 2000lxs
Aircraft are often compared by category, range, and passenger capacity, and each factor tends to trade off against the others. General aviation aircraft, such as single- and light twin‑engine planes, typically carry 1–6 passengers and are optimized for flexibility and short to medium trips, commonly a few hundred to roughly 1,500 nautical miles depending on speed, payload, and fuel. Regional aircraft, including turboprops and smaller regional jets, usually seat about 30–90 passengers and serve short to midrange routes, often around 500–2,000 nautical miles, balancing airport performance with efficient high‑frequency service. Narrow‑body mainline jets, widely used for domestic and shorter international flying, generally carry about 120–240 passengers and cover roughly 1,500–4,000 nautical miles, with variants tuned either for higher capacity or longer legs. Wide‑body jets are designed for long‑haul missions, typically seating around 250–450+ passengers and reaching approximately 4,000–8,000+ nautical miles, emphasizing payload, comfort, and fuel efficiency over very long distances. Cargo aircraft follow similar range classes but prioritize volume and maximum payload rather than seats.
| Spec | Bombardier Challenger 650 | Dassault Falcon 2000LXS | Embraer Praetor 600 | Gulfstream G400 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | — |
| DOC / nm | $ 7.16 | $ 6.38 | $ 6.74 | — |
| Min Crew | 2 | 2 | 2 | 4 |
| Total Seats | 11 | 12 | 10 | 12 |
| Manufacturer | Bombardier | Dassault Falcon | Embraer | Gulfstream |
| Aircraft Name | Challenger 650 | 2000LXS | Praetor 600 | G400 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | — |
| Max Range (nm) | 4085 | 4155 | 4018 | 4200 |
| DOC / nm / Seat | $ 0.80 | $ 0.80 | $ 0.84 | — |
| Max Cabin Seats | 12 | 10 | 12 | 19 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | — |
| Useful Load (lbs) | 21050 | 18250 | — | 30650 |
| Standard Cabin Seats | 9 | 10 | 8 | — |
| Direct Operating Cost | $ 3,365 | $ 3,073 | $ 3,141 | — |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 Advanced | Honeywell Primus EASy II | Rockwell Collins Pro Line Fusion | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 470 | 490 | 542 | 539 |
| Base Aircraft Price (USD) | $32,400,000 | $35,100,000 | $20,995,000 | 34500000 |
| 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 | 131 | 45 | — |
| Cabin Volume (cu. ft) | — | 1024 | — | — |
| Baggage Volume Ext. (cu. ft) | — | — | 110 | — |