An-2 Colt vs CL-415 Super Scooper
Overview
The An-2 Colt and the CL-415 Super Scooper are both Military Transport Aircraft, manufactured by Antonov and Viking Air respectively.
Top speed is 258 km/h for the An-2 Colt vs 359 km/h for the CL-415 Super Scooper. The An-2 Colt has an operational range of 845 km vs 2,427 km for the CL-415 Super Scooper. The An-2 Colt operates at altitudes up to 4,500 m compared to 4,481 m for the CL-415 Super Scooper. At 19,890 kg MTOW, the CL-415 Super Scooper is 3.7x the An-2 Colt's 5,440 kg.
The An-2 Colt has been produced in 18,000 units vs 95 for the CL-415 Super Scooper. Unit cost is $0.1M for the An-2 Colt vs $37M for the CL-415 Super Scooper. The An-2 Colt first flew 46 years before the CL-415 Super Scooper (1947 vs 1993).
| Soviet single-engine biplane aircraft, mass-produced since 1947, remaining in service for military and civilian operations. | |
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| Origin country | 🇨🇳 Ex-USSR |
| Category | Military Transport Aircraft |
| Manufacturer | Antonov |
| First flight | 31 August 1947 |
| Year introduced | 1947 |
| Number produced | 18000 units |
| Average unit price | $100K |
| Canadian amphibious aircraft, significant in firefighting operations globally, developed in the late 20th century. | |
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| Origin country | 🇨🇦 Canada |
| Category | Military Transport Aircraft |
| Manufacturer | Viking Air |
| First flight | 6 December 1993 |
| Year introduced | 1994 |
| Number produced | 95 units |
| Average unit price | $37 million |
| Wing area | 71.5 m² ◉ |
| Wingspan | 18.2 m â—‰ |
| Height | 4.1 m â—‰ |
| Length | 12.4 m â—‰ |
| Maximum speed | 258 km/h â—‰ |
| Operational range | 845 km â—‰ |
| Service ceiling | 4,500 m â—‰ |
| Max. takeoff weight | 5,440 kg â—‰ |
| Empty weight | 3,300 kg â—‰ |
| Total thrust | 1 x 750 kW â—‰ |
| Wing area | 100.0 m² ◉ |
| Wingspan | 28.4 m â—‰ |
| Height | 8.9 m â—‰ |
| Length | 20.0 m â—‰ |
| Maximum speed | 359 km/h â—‰ |
| Operational range | 2,427 km â—‰ |
| Service ceiling | 4,481 m â—‰ |
| Max. takeoff weight | 19,890 kg â—‰ |
| Empty weight | 12,882 kg â—‰ |
| Total thrust | 2 x 888 kW â—‰ |
Performance Radar Chart
Detailed Comparison
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