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| No. Of Engines: |
2 |
| Aircraft Type: |
Turbo Prop |
| Passenger Capacity (Max): |
20 |
| Range (in Miles): |
745 |
| Cruising Speed (MPH): |
209 |
| Payload Capacity (in Lbs): |
4,420 |
| Wingspan: |
65 |
| Length: |
51 |
| Height: |
19 |
| Headroom: |
5 |
| Takeoff Weight (in Lbs): |
12,500 |
The
DeHavilland Canada DHC 6 Twin Otter was first flown in 1965
with deliveries beginning in 1966. Three production versions
were offered during the 22 years of production. The initial
production version was designated the -100, followed by
the -200 and -300. The -100 and -200 are better for inter-city
commuter service, while the -300 was developed to offer
increased payload capacity, higher cruising speeds, better
hot weather performance and a short takeoff distance. Production
ended with more than 800 deliveries.
The
Twin Otter is made by the DeHavilland company of Canada.
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