DHC-5 Buffalo vs DHC-6 Twin Otter
Overview
The DHC-5 Buffalo and the DHC-6 Twin Otter are both Military Transport Aircraft, manufactured by De Havilland Canada and De Havilland Canada respectively.
Top speed is 467 km/h for the DHC-5 Buffalo vs 315 km/h for the DHC-6 Twin Otter. The DHC-5 Buffalo has an operational range of 1,100 km vs 1,480 km for the DHC-6 Twin Otter. The DHC-5 Buffalo operates at altitudes up to 9,449 m compared to 7,620 m for the DHC-6 Twin Otter. At 22,317 kg MTOW, the DHC-5 Buffalo is 3.9x the DHC-6 Twin Otter's 5,670 kg.
The DHC-5 Buffalo has been produced in 122 units vs 985 for the DHC-6 Twin Otter. Unit cost is $25M for the DHC-5 Buffalo vs $7M for the DHC-6 Twin Otter. The DHC-5 Buffalo first flew 1 years before the DHC-6 Twin Otter (1964 vs 1965).
| Canadian tactical transport aircraft, primarily utilized during the 1960s, notably deployed for civilian and military air-drop operations. | |
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| Origin country | 🇨🇦 Canada |
| Category | Military Transport Aircraft |
| Manufacturer | De Havilland Canada |
| First flight | 9 April 1964 |
| Year introduced | 1965 |
| Number produced | 122 units |
| Average unit price | $25 million |
| Canadian utility aircraft, vital in civil and military operations worldwide since the 1960s, famous for its STOL capabilities. | |
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| Origin country | 🇨🇦 Canada |
| Category | Military Transport Aircraft |
| Manufacturer | De Havilland Canada |
| First flight | 20 May 1965 |
| Year introduced | 1966 |
| Number produced | 985 units |
| Average unit price | $7 million |
| Wing area | 88.0 m² ◉ |
| Wingspan | 29.0 m â—‰ |
| Height | 8.8 m â—‰ |
| Length | 24.0 m â—‰ |
| Maximum speed | 467 km/h â—‰ |
| Operational range | 1,100 km â—‰ |
| Service ceiling | 9,449 m â—‰ |
| Max. takeoff weight | 22,317 kg â—‰ |
| Empty weight | 11,412 kg â—‰ |
| Total thrust | 2 x 1,168 kW â—‰ |
| 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 | 1,480 km â—‰ |
| Service ceiling | 7,620 m â—‰ |
| Max. takeoff weight | 5,670 kg â—‰ |
| Empty weight | 3,175 kg â—‰ |
| Total thrust | 2 x 205 kW â—‰ |
Performance Radar Chart
Detailed Comparison
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