L-410 vs DHC-6 Twin Otter
| Czech twin-engine short-range transport aircraft, deployed internationally since the 70s, used in both civil and military operations. |
|
|
| Origin country |
🇨🇿 Czech Republic
|
| Category |
Military Transport Aircraft |
| Manufacturer |
Let |
| First flight |
16 April 1969 |
| Year of introduction |
1970 |
| Number produced |
1200 units
|
| Average unit price |
$-- million
|
| 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
|
| Wing area |
35.2 m²
â—‰
|
| Wingspan |
19.5 m
â—‰
|
| Height |
5.8 m
â—‰
|
| Length |
14.5 m
â—‰
|
| Maximum speed |
365 km/h
â—‰
|
| Service ceiling |
7,000 m
â—‰
|
| Max. takeoff weight |
5,800 kg
â—‰
|
| Empty weight |
3,800 kg
â—‰
|
| Total thrust |
2 x 575 kW
â—‰
|
|
|
| Wing area |
39.0 m²
â—‰
|
| Wingspan |
20.0 m
â—‰
|
| Height |
6.0 m
â—‰
|
| Length |
15.8 m
â—‰
|
| Maximum speed |
315 km/h
â—‰
|
| 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—‰
|
|
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Photo of DHC-6 Twin Otter by De Havilland.