CL-415 Super Scooper vs CN-235
| Canadian amphibious aircraft, significant in firefighting operations globally, developed in the late 20th century. | |
|
|
| 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 |
| Spanish-Indonesian transport aircraft, widespread use in the civil sector, military services, and humanitarian aid, developed during the late 20th century. | |
|
|
| Origin country | 🇪🇸 Spain 🇮🇩 Indonesia |
| Category | Military Transport Aircraft |
| Manufacturer | CASA |
| First flight | 11 November 1983 |
| Year introduced | 1988 |
| Number produced | 354 units |
| Average unit price | $25 million |
| 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 | -- km |
| Service ceiling | 4,481 m â—‰ |
| Max. takeoff weight | 19,890 kg â—‰ |
| Empty weight | 12,882 kg â—‰ |
| Total thrust | 2 x 1,775 kW â—‰ |
| Wing area | 59.1 m² ◉ |
| Wingspan | 25.8 m â—‰ |
| Height | 8.2 m â—‰ |
| Length | 21.4 m â—‰ |
| Maximum speed | 450 km/h â—‰ |
| Operational range | 5,060 km |
| Service ceiling | 9,144 m â—‰ |
| Max. takeoff weight | 16,500 kg â—‰ |
| Empty weight | 8,800 kg â—‰ |
| Total thrust | 2 x 1,305 kW â—‰ |
Performance Radar Chart
Photo of CL-415 Super Scooper by Maarten Visser.