208 Caravan vs CL-600 Challenger
Overview
The 208 Caravan and the CL-600 Challenger are both Military Transport Aircraft, manufactured by Cessna and Bombardier respectively.
The CL-600 Challenger reaches 882 km/h β 2.6x the 208 Caravan's 344 km/h. The 208 Caravan has an operational range of 1,980 km vs 7,400 km for the CL-600 Challenger. The CL-600 Challenger operates at altitudes up to 12,497 m compared to 7,600 m for the 208 Caravan. At 19,550 kg MTOW, the CL-600 Challenger is 4.9x the 208 Caravan's 3,970 kg.
The 208 Caravan has been produced in 3,000 units vs 1,066 for the CL-600 Challenger. Unit cost is $2.1M for the 208 Caravan vs $14M for the CL-600 Challenger. The CL-600 Challenger first flew 4 years before the 208 Caravan (1978 vs 1982).
| American utility aircraft, primarily deployed for passenger and cargo transportation, known for its operational history since the 1980s. | |
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| Origin country | πΊπΈ United States |
| Category | Military Transport Aircraft |
| Manufacturer | Cessna |
| First flight | 9 December 1982 |
| Year introduced | 1984 |
| Number produced | 3000 units |
| Average unit price | $2.1 million |
| Canadian business jet, introduced in the 1980s, extensively deployed for VIP and corporate travel worldwide. | |
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| Origin country | π¨π¦ Canada |
| Category | Military Transport Aircraft |
| Manufacturer | Bombardier |
| First flight | 8 November 1978 |
| Year introduced | 1980 |
| Number produced | 1066 units |
| Average unit price | $14 million |
| Wing area | 26.0 mΒ² β |
| Wingspan | 15.9 m β |
| Height | 4.3 m β |
| Length | 12.7 m β |
| Maximum speed | 344 km/h β |
| Operational range | 1,980 km β |
| Service ceiling | 7,600 m β |
| Max. takeoff weight | 3,970 kg β |
| Empty weight | 2,073 kg β |
| Total thrust | 1 x 505 kW β |
| Wing area | 48.3 mΒ² β |
| Wingspan | 19.6 m β |
| Height | 6.3 m β |
| Length | 20.9 m β |
| Maximum speed | 882 km/h β |
| Operational range | 7,400 km β |
| Service ceiling | 12,497 m β |
| Max. takeoff weight | 19,550 kg β |
| Empty weight | 9,292 kg β |
| Total thrust | 2 x 2,073 kgf β |
Performance Radar Chart
Detailed Comparison
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