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      DynAero 
      
      CR 100 
      
      
        
            
      
        
      
      
      
      
      
            
              
            
            
            The CR100 is a high speed aerobatic aircraft which doubles as a 
            spacious two seat tourer. Built using a blend of traditional 
            materials and Carbon Fibre it remains easy to build but gains the 
            advantages of modern composites 
      
              
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                
                  Lycoming AEIO 
                  360 B2F 180 
             
                
                  
                fixed pitch EVRA   or
                  variable pitch MT propeller 
                
                  7.50m 
                
                x 
                
            
                  8.50
                  m 
                
            
                  10.65
                  sq m 
                2 
                
                x 
                x 
                
                x 
                
                x 
                
                  560km 
                long range tank available | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                x 
                
                x 
                x 
                
                  280kph 
                x 
                x | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                
            
                  305
                  kph 
                x 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
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