CN-235 vs C-160 Transall
| 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 of introduction | 1988 |
| Number produced | 354 units |
| Average unit price | $25 million |
| German-French transport plane, employed globally since the Cold War, essential for humanitarian aid, military logistical support, and troop transport. | |
|
|
| Origin country | 🇩🇪 Germany 🇫🇷 France |
| Category | Military Transport Aircraft |
| Manufacturer | Transall |
| First flight | 25 February 1963 |
| Year of introduction | 1967 |
| Number produced | 214 units |
| Average unit price | $12 million |
| 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 â—‰ |
| 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—‰ |
| Wing area | 160.0 m² ◉ |
| Wingspan | 40.0 m â—‰ |
| Height | 11.7 m â—‰ |
| Length | 32.4 m â—‰ |
| Maximum speed | 513 km/h â—‰ |
| Operational range | 1,850 km â—‰ |
| Service ceiling | 8,230 m â—‰ |
| Max. takeoff weight | 51,000 kg â—‰ |
| Empty weight | 29,000 kg â—‰ |
| Total thrust | 2 x 4,549 kW â—‰ |
|
|