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      Jurca 
      
            
            M.J-77 Mustang (75%) 
      
      
        
      
            
             
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                
            
            Geschwender 351 HP 
                Range200-360 
                x 
                
      
                
                21,5ft 
                
      
                
                7ft 
                
      
                
                27.8ft 
                
      
                
                145sq.ft
            
            
       
                2 
                
      
                
                2200lb 
                x 
                
      
                
                2860lb
            
            
       
                
      
                
                50gal 
                
      
            
            500n.m | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                
            
            2500ft 
                
      
            
            1500fpm 
                
      
            
            289mph 
                
      
            
            230mph 
                
      
            
            1500ft 
                x | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                x 
                
      
            
            65mph 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations  | 
               
              
 
      
            
            Design needs ballast in nose if V-S engine
            is used. R (reinforced) version permits gross
            weight of 3300 pounds and has complete stress analysis.
            
            
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