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      General Dynamics F-16 
      
      
      
       
       
      
      The F-16 evolved from a 1972 USAF 
      Lightweight Fighter (LWF) prototype program which sought a small, 
      lightweight, low cost, air superiority day fighter designed for high 
      performance and ease of maintenance. It achieved combat-ready status in 
      October 1980. Many foreign nations, including Belgium, Denmark, Turkey, 
      Egypt and Israel, have purchased the F-16.  
      SPECIFICATIONS
       
      (F16A Block 15)  
      Span: 32 ft. 10 in.  
      Length: 49 ft. 6 in.  
      Height: 16 ft. 6 in.  
      Weight: 29,896 lbs. loaded  
      Armament: One 20mm M-61A1 cannon and various combinations ot 
      air-to-air and air-to-ground missiles and bombs.  
      Engine: One Pratt & Whitney F100-PW-200 of 23,830 lbs. thrust with 
      afterburner.  
      Crew: One  
      Cost: $8,200,000  
      Serial number: 81-0663  
      PERFORMANCE
       
      (F16A Block 15)  
      Maximum speed: 1,345 mph.  
      Cruising speed: 577 mph.  
      Range: 1,407 miles  
      Service Ceiling: 55,000 ft.  
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