Falcon 2000LXS
$35.0M
Challenger 601
$13.0M
Technical Specification Matrix
Performance Metrics
| Parameter | Falcon 2000LXS | Challenger 601 |
|---|---|---|
| Max Range (NBAA IFR) | 4,000 nmWinner | 3,370 nm |
| Max Cruise Speed | Mach 0.862Winner (Speed) | Mach 0.82 |
| Takeoff Distance (SL, ISA, MTOW) | 4,675 ftShort Field | 5,830 ft |
| Max Operating Altitude | 47,000 ft | 41,000 ft |
Cabin Environment
| Max Certified Seating | 10 pax | 12 pax |
| Cabin Width | 7.7 ft | 8.2 ftWider |
| Cabin Altitude @ FL410 | 7,000 ftLower Altitude | 8,000 ft |
Expert Insights
Range & Capability
The Falcon 2000LXS excels in sheer capability with a 4000nm range, making it preferred for extreme ultra-long-haul city pairs, whereas the Challenger 601 counters with 3370nm.
Cabin Architecture
While the Falcon 2000LXS focuses on its 2-zone configuration (7.7ft wide), the Challenger 601 provides 8.2ft of width, offering a distinctly different volumetric feel for passengers.
Technological Edge
The Dassault Falcon 2000LXS is a compelling choice in the large cabin segment because it combines cr... Both platforms represent the pinnacle of modern fly-by-wire avionics and systems redundancy in the large cabin class.
Operating Economics (Est.)
Variable Costs Per Hour
Economic Note
Estimates based on 450 hours annual utilization. The Falcon 2000LXS shows higher fuel efficiency resulting in lower direct variable costs per hour, while both airframes require similar fixed overheads for crew and hangarage.