The FK 12 Comet has good flight performance due 
                  to optimized laminar profile with four ailerons (flaperons) 
                  over the entire wingspan. The aircraft can be adapted within 
                  minutes from open cockpit to a one or two-seater closed 
                  cockpit. 
                  
                  The wings can be folded in a matter of minutes 
                  by one person alone! – Transport width: 2.42 m. The aircraft 
                  can be bought complete or as a kit.
                  
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                
                Rotax 912ULS 
             
                
            
                Ducaine composite fixed pitch three-blade. 
                
                  
            
                  l8ft  
                
                  
            
                  6ft 2in 
                
                  
            
                  23ft 
                
                  
            
                  144.2sq ft 
                2 
                
                  
            
                  661lb 
                
                  
            
                  330lb 
                
                  
            
                  9921b 
                
                  
            
                  12.7 Imp gal 
                 
                
                x | 
               
             
            
            performance 
            
             
            
              
                
                takeoff 
                distance, ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                x 
                
            
            
                1,378ft/min 
                
                 
                x 
                
            
            
                102 knots 
                
                 
                x 
                x | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design 
                manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                
            
            
                119 knots 
                
            
            
                33 knots 
                
                 
                x | 
               
             
            
      
            
            the empty weight can be reduced to 5821b in the 
            Microlight
            category and the max AUW increased to 1,146lb in the Experimental
            category. When operated in the Experimental category the G limits
            also increase to +6/-2.66G. Folding wings 
       
               All specifications are based on 
               manufacturer's calculations 
               
      
        
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