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            Lancair 
      
      320 
      
      
        
      
        
      
      The Lancair 320 has proven to be an extremely 
      popular homebuilt aircraft. There are more than 1500 Lancairs sold to 
      people all over the United States and Canada, Europe, Scandinavia, 
      Australia (where the aircraft certification authorities required the tail 
      to be enlarged before allowing them to be licensed), and South Africa. The 
      company that designed and built the Lancair, Lancair International, 
      provided for their customers a network of support which included extensive 
      free technical support, a Lancair Preflight Inspection Program, the First 
      Flight Test Program, and a Flight Training Program.  
      
      The first model, Lancair 200, designed by 
      Lance A. Neibauer, was developed in 1984. The prototype can be found in 
      the EAA museum in Oshkosh. His company’s goal was to be an important part 
      in shaping the future of modern aviation through innovation, technical 
      advances in design, aesthetics and performance. Ownership of the company 
      changed hands and is now named Columbia. 
      
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                Lycoming O-320 B1A-modified 
         Hartzell HC-F 2YL-1F, F8468-D 2 blades csu 
         21 ft .75 in 
         5 ft 10.25 in 
                23 ft 8.5 in 
         76 sq ft 
                
                x 
                1187.5 lb 
                613 lb 
                1800 lb 
         39.975 gal 
                
                x | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                x 
                
                x 
                x 
                x 
                x 
                x | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                143kt 
                235kt 
                67 kt 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
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