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      Hummel CA 2 
      
      
        
      
      
        
            
            The CA-2 is a light all metal legal 
            ultralight (with Rotax 277) aircraft that can be built inexpensively 
            from plans (approximately $2,000-2,500 for airframe) in 600 hours.  
            Easy construction from sheet, angle extrusions, tubing and pop 
            rivets.  No welding, gluing, machining, or difficult forming 
            required.  Fuselage assembly performed on a flat table and wing 
            assembly using a simple wood jig. 
            
             
            Strong all metal wing (utility 
            category +4.4, -2.2g), smooth push rod controls, large ailerons and 
            rudder, wide landing gear stance for easy ground handling, and wing 
            detaches with removal of three bolts.
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                
                x 
                x 
                
                
                16.5 ft
                     
                
                x 
                
                
                26 feet
                     
                
                
                17 sq. feet
                     
                1 
                
                
                250 lbs 
                x 
                
                
                500 lbs 
                
                
                5 gallons 
                    
                
                125 mile  | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                x 
                
                x 
                
                
                63 mph
                    
                 
                
                
                50 mph 
                 
                x 
                x | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                
                
                80 mph 
                
                
                26 mph 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
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