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         Design of the Islander 
         started in 1963 and the first prototype BN-2 first flew on 13 June 
         1965, with the second prototype following on 20 August 1966. Both of 
         these had engines that were less powerful than the production versions. 
         The first production Islander first flew on 24 April 1967. 
          
         An improved version, the BN-2A, first flew in 1969. It incorporated 
         aerodynamic and flight equipment improvements as well as changes to the 
         baggage arrangements. 
          
         The Defender, a military version of the Islander, first flew on 20 May 
         1970. 
          
         In 1978 a further improved version, the BN-2B Islander II was 
         introduced. Improvements included an increased carrying capacity and 
         propeller modifications to reduce noise levels. Options that were 
         available include a long-nosed version for increased baggage capacity, 
         raked wingtip auxiliary fuel tanks and twin Allison 250-B17C turboprop 
         engines. When the latter are installed the aircraft is designated as 
         the designated the BN-2T. 
          
         An attempt to develop an Islander with an even larger capacity resulted 
         in the BN-2A Mk III Trislander. This aircraft has a stretched fuselage, 
         modified landing gear and a third (tail-mounted) engine. The prototype 
         was constructed from the original second BN-2 prototype and flew on 11 
         September 1970. 
          
         A number of other companies have also manufactured the Islander in 
         addition to Britten-Norman. URMA from Romania has been building the 
         aircraft since 1969, while a factory in Gosselies, Belgium has been 
         building it since 1973. The aircraft has also been assembled in the 
         Philippines. 
         Capacity 
         Passenger configuration: 8 
         Cargo configuration: 700kg 
          
         Performance 
         Engines: 2 x 260 HP AVCO Lycoming 
         Range: 435km 
         Take off speed: 108kph 
         Cruising speed and height: 241kph at 2,430m 
         Landing speed: 93kph 
         Fuel capacity: 354kg 
         Max take off weight: 2993kg 
         Flight deck crew: 1  
          
          
         Technical Dimensions 
         Length: 10.87m 
         Wingspan: 16.15m 
         Height: 3.9m 
         Fuselage width: 1.09m 
         Rear hold capacity: 120kg 
         Rear hold door size: 0.46m x 0.76m 
         Interior cabin dimensions in cargo config: 2.9m x 1.24m x 1.09m 
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