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Military


UV-18A Twin Otter

Specifications
Contractor de Havilland Canada
Crew 1-2
Wingspan 19.8 m
Length 15.1 m
Height 5.7 m
Wing area 39.0 sq. m
Empty weight 2654 kg
Takeoff weight 4761 kg
Engines 2 x Pratt & Whitney of Canada PT6-27, 652 hp each
Max. speed 343 km/h
Cruise speed 297 km/h
Speed Range 65-165 KIAS
Cruise ceiling 3050 m
Ceiling 25,000 ft. (Oxygen installed)
Rate of Climb 1600 fpm, typical
Range with maximum payload 200 km
Endurance - Maximum
Altitude Airspeed Fuel Burn (lbs/hr) Endurance (hrs)
Sea Level 120 kts 480 4.2
5,000' 120 kts 460 4.3
10,000' 120 kts 440 4.4
Endurance - Maximum >12 Hour Missions with Extended Fuel Tank
Payload 20 passengers or 1045 kg of payload
Payload 4500 lbs.
Power Available >4200 W
Communications VHF, UHF, HF, UHF/FM
AvionicsTacan, GPS, VHF/UHF Homing
Unit Cost $2,000,000
User CountriesArgentina, Canada, Chile, Colombia, Haiti, Kenya, Norway, Pakistan, Panama, Paraguay, People's Republic of China, Senegal, Sudan, Switzerland, USA.



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Page last modified: 07-07-2011 02:38:54 ZULU