DHC-6 Twin Otter vs Y-12
| Canadian utility aircraft, vital in civil and military operations worldwide since the 1960s, famous for its STOL capabilities. | |
|
|
| Origin country | 🇨🇦 Canada |
| Category | Military Transport Aircraft |
| Manufacturer | De Havilland Canada |
| First flight | 20 May 1965 |
| Year of introduction | 1966 |
| Number produced | 985 units |
| Average unit price | $7 million |
| Chinese twin-engine light utility aircraft, recognized from its 1980s development, frequently used for passenger and cargo transportation. | |
|
|
| Origin country | 🇨🇳 China |
| Category | Military Transport Aircraft |
| Manufacturer | Harbin |
| First flight | 14 July 1982 |
| Year of introduction | 1985 |
| Number produced | 71 units |
| Average unit price | $5 million |
| Wing area | 39.0 m² ◉ |
| Wingspan | 20.0 m â—‰ |
| Height | 6.0 m â—‰ |
| Length | 15.8 m â—‰ |
| Maximum speed | 315 km/h â—‰ |
| Operational range | -- km |
| Service ceiling | 7,620 m â—‰ |
| Max. takeoff weight | 5,670 kg â—‰ |
| Empty weight | 3,175 kg â—‰ |
| Total thrust | 2 x 410 kW â—‰ |
| Wing area | 34.3 m² ◉ |
| Wingspan | 17.2 m â—‰ |
| Height | 5.7 m â—‰ |
| Length | 18.9 m â—‰ |
| Maximum speed | 328 km/h â—‰ |
| Operational range | 1,340 km |
| Service ceiling | 7,000 m â—‰ |
| Max. takeoff weight | 5,300 kg â—‰ |
| Empty weight | 2,840 kg â—‰ |
| Total thrust | 2 x 410 kW â—‰ |
Performance Radar Chart
Photo of DHC-6 Twin Otter by De Havilland.