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      Diamond DA20-C1 
      Evolution/Eclipse performance and specifications 
      
                              
                                
                              
                              
                              
                              Powerplant: Teledyne Continental IO240B3B, 
                              four-cylinder, horizontally opposed, fuel injected 
                              125 hp 
                              
                              
            
                            
        
                              
                              
                                
                                  | 
                                  
                                  Length | 
                                  
                                   
                                   23 ft 6 in  | 
                                 
                                
                                  | 
                                  
                                   Height | 
                                  
                                   
                                   7 ft 2 in  | 
                                 
                                
                                  | 
                                  
                                   Wingspan | 
                                  
                                   
                                   35 ft 8 in  | 
                                 
                                
                                  | 
                                  
                                   Wing Area | 
                                  
                                   
                                   125 sq ft  | 
                                 
                                
                                  | 
                                  
                                   Seats | 
                                  
                                   
                                   2  | 
                                 
                                
                                  | 
                                  
                                   Empty weight, 
                                  typical | 
                                  
                                   1,166 lb | 
                                 
                                
                                  | 
                                  
                                   Maximum gross 
                                  weight | 
                                  
                                   1,720 lb | 
                                 
                                
                                  | 
                                  
                                   Useable fuel | 
                                  
                                   24 US gal | 
                                 
                                
                                  |   | 
                                    | 
                                 
                                
                                  | 
                                  
                                   Performance | 
                                    | 
                                 
                                
                                  | 
                                  
                                   Takeoff 
                                  distance, ground roll | 
                                  
                                  
                                   1,106 ft | 
                                 
                                
                                  | 
                                  
                                   Takeoff distance 
                                  over 50-ft obstacle | 
                                  
                                   1,470 ft | 
                                 
                                
                                  | 
                                  
                                   Max demonstrated 
                                  crosswind component | 
                                  
                                   20 kt | 
                                 
                                
                                  | 
                                  
                                   Rate of climb, 
                                  sea level | 
                                  
                                   1,000 fpm | 
                                 
                                
                                  | 
                                  
                                   Cruise speed @ 
                                  75% power | 
                                  
                                   135 ktas | 
                                 
                                
                                  | 
                                  
                                   Landing distance 
                                  over 50-ft obstacle | 
                                  
                                   1,280 ft | 
                                 
                                
                                  | 
                                  
                                   Landing 
                                  distance, ground roll | 
                                  
                                   581 ft | 
                                 
                                
                                  |   | 
                                    | 
                                 
                                
                                  | 
                                  
                                   Limiting and 
                                  Recommended Airspeeds | 
                                  
                                  
                                    | 
                                 
                                
                                  | 
                                  
                                   Vx (best angle 
                                  of climb) | 
                                  
                                   60 kias | 
                                 
                                
                                  | 
                                  
                                   Vy (best rate of 
                                  climb) | 
                                  
                                   75 kias | 
                                 
                                
                                  | 
                                  
                                   Vso (stall, in 
                                  landing configuration) | 
                                  
                                   44 kcas | 
                                 
                                
                                  | 
                                  
                                    Vne (never 
                                  exceed) | 
                                  
                                   164 
                                  kias | 
                                 
                               
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