First built in 1965, the DeHavilland Twin Otter has proved to be one of the most successful and versatile aircraft ever built. The Twin Otter is used in may roles: cargo / passenger transport, rescue, forestry patrol, geophysical and photographic survey, and skydiving.

No light transport, in the12,500 lb. class, does such a variety of work in such diverse climatic conditions. From as far north as Norman Wells, NWT in the Canadian Arctic to the heat of Jamaica and the Virgin Isles and with 20 people on board.

With its remarkably robust landing gear - either in standard tricycle configuration supporting standard wheels, high flotation tires, skis or equipped with floats and aided by its Short Take-off and Landing capability, there are few fixed wing airstrips in the world that are not accessible to a Twin Otter.

Conventional design, with the wings incorporating double-slotted trailing edge flaps and ailerons which droop simultaneously with the use of the flaps to enhance STOL characteristics.

All systems designed to withstand the heavy grind of daily commuter landings on paved runways or improvised strips.

Basic Data
WEIGHTS DIMENSIONS
Max Takeoff weight 12,500 lb. Wingspan 65.0 ft.
Max Landing 12,300 lb. Length 51.75 ft.
Basic (Commuter) 6,873 lb. Tail Height 19.5 ft.
Maximum Fuel Capacity Cabin Height 9 ft. 8 in
- Standard 2,583 lb.
- with Wing Tanks 3,190 lb.
CABIN DIMENSIONS

BAGGAGE COMPARTMENT VOLUME

Cabin Height 4 ft. 4 in Rear Baggage 88 cu. ft.
Cabin Length 18 ft. 5 in Front Baggage 33 cu. ft.
Cabin Width 4 ft. 4 in
NUMBER OF CREW 1 or 2 NUMBER OF PASSENGERS 20

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