Challenger 300
$24.0M
G280
$25.0M
Technical Specification Matrix
Performance Metrics
| Parameter | Challenger 300 | G280 |
|---|---|---|
| Max Range (NBAA IFR) | 3,100 nm | 3,600 nmWinner |
| Max Cruise Speed | Mach 0.83 | Mach 0.85Winner (Speed) |
| Takeoff Distance (SL, ISA, MTOW) | 4,810 ft | 4,750 ftShort Field |
| Max Operating Altitude | 45,000 ft | 45,000 ft |
Cabin Environment
| Max Certified Seating | 10 pax | 10 pax |
| Cabin Width | 7.2 ft | 7.2 ft |
| Cabin Altitude @ FL410 | 7,400 ft | 7,000 ftLower Altitude |
Expert Insights
Range & Capability
The Challenger 300 excels in sheer capability with a 3100nm range, making it preferred for extreme ultra-long-haul city pairs, whereas the G280 counters with 3600nm.
Cabin Architecture
While the Challenger 300 focuses on its 2-zone configuration (7.2ft wide), the G280 provides 7.2ft of width, offering a distinctly different volumetric feel for passengers.
Technological Edge
The Bombardier Challenger 300 remains useful to understand because it shaped Bombardier's position i... Both platforms represent the pinnacle of modern fly-by-wire avionics and systems redundancy in the super mid size class.
Operating Economics (Est.)
Variable Costs Per Hour
Economic Note
Estimates based on 450 hours annual utilization. The G280 shows higher fuel efficiency resulting in lower direct variable costs per hour, while both airframes require similar fixed overheads for crew and hangarage.