Falcon 900
$21.0M
Global 6000
$62.0M
Technical Specification Matrix
Performance Metrics
| Parameter | Falcon 900 | Global 6000 |
|---|---|---|
| Max Range (NBAA IFR) | 3,800 nm | 6,000 nmWinner |
| Max Cruise Speed | Mach 0.87 | Mach 0.89Winner (Speed) |
| Takeoff Distance (SL, ISA, MTOW) | 5,235 ftShort Field | 6,476 ft |
| Max Operating Altitude | 51,000 ft | 51,000 ft |
Cabin Environment
| Max Certified Seating | 14 pax | 17 pax |
| Cabin Width | 7.7 ft | 7.9 ftWider |
| Cabin Altitude @ FL410 | 8,000 ft | 4,500 ftLower Altitude |
Expert Insights
Range & Capability
The Falcon 900 excels in sheer capability with a 3800nm range, making it preferred for extreme ultra-long-haul city pairs, whereas the Global 6000 counters with 6000nm.
Cabin Architecture
While the Falcon 900 focuses on its 3-zone configuration (7.7ft wide), the Global 6000 provides 7.9ft of width, offering a distinctly different volumetric feel for passengers.
Technological Edge
The Dassault Falcon 900 remains a meaningful Falcon model for operators, buyers, and aviation resear... Both platforms represent the pinnacle of modern fly-by-wire avionics and systems redundancy in the long range class.
Operating Economics (Est.)
Variable Costs Per Hour
Economic Note
Estimates based on 450 hours annual utilization. The Falcon 900 shows higher fuel efficiency resulting in lower direct variable costs per hour, while both airframes require similar fixed overheads for crew and hangarage.