CL-600 Challenger vs Learjet 45
Overview
The CL-600 Challenger and the Learjet 45 are both Military Transport Aircraft, manufactured by Bombardier and Bombardier respectively.
Top speed is 882 km/h for the CL-600 Challenger vs 858 km/h for the Learjet 45. The CL-600 Challenger has an operational range of 7,400 km vs 3,167 km for the Learjet 45. The Learjet 45 operates at altitudes up to 15,545 m compared to 12,497 m for the CL-600 Challenger. At 19,550 kg MTOW, the CL-600 Challenger is 2.1x the Learjet 45's 9,163 kg.
The CL-600 Challenger has been produced in 1,066 units vs 642 for the Learjet 45. Unit cost is $14M for the CL-600 Challenger vs $3.2M for the Learjet 45. The CL-600 Challenger first flew 17 years before the Learjet 45 (1978 vs 1995).
| Canadian business jet, introduced in the 1980s, extensively deployed for VIP and corporate travel worldwide. | |
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| Origin country | 🇨🇦 Canada |
| Category | Military Transport Aircraft |
| Manufacturer | Bombardier |
| First flight | 8 November 1978 |
| Year introduced | 1980 |
| Number produced | 1066 units |
| Average unit price | $14 million |
| Canadian light business jet, prevalently used for private and business aviation, came into operation in the mid-1990s. | |
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| Origin country | 🇨🇦 Canada |
| Category | Military Transport Aircraft |
| Manufacturer | Bombardier |
| First flight | 7 October 1995 |
| Year introduced | 1998 |
| Number produced | 642 units |
| Average unit price | $3.2 million |
| Wing area | 48.3 m² ◉ |
| Wingspan | 19.6 m â—‰ |
| Height | 6.3 m â—‰ |
| Length | 20.9 m â—‰ |
| Maximum speed | 882 km/h â—‰ |
| Operational range | 7,400 km â—‰ |
| Service ceiling | 12,497 m â—‰ |
| Max. takeoff weight | 19,550 kg â—‰ |
| Empty weight | 9,292 kg â—‰ |
| Total thrust | 2 x 2,073 kgf â—‰ |
| Wing area | 29.0 m² ◉ |
| Wingspan | 14.6 m â—‰ |
| Height | 4.3 m â—‰ |
| Length | 17.6 m â—‰ |
| Maximum speed | 858 km/h â—‰ |
| Operational range | 3,167 km â—‰ |
| Service ceiling | 15,545 m â—‰ |
| Max. takeoff weight | 9,163 kg â—‰ |
| Empty weight | 5,829 kg â—‰ |
| Total thrust | 2 x 794 kgf â—‰ |
Performance Radar Chart
Detailed Comparison
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