| 
    | 
   
   
     
       
         | 
       
      
        
      
      
            
            Jabiru J200 
      
      
        
      
            
            
              
            
            The Jabiru J200 (2 seater)  has evolved from 
            combining the best features of the LSA, SP & UL models.  It comes 
            with the standard LSA wings with the fuel in the wings.
            The longer tail boom results in more elevator and empennage 
            authority, reducing the stall speed to 45 kts and increasing 
            directional stability. The J200 was developed as a replacement to 
            the GA alternatives i.e. Cessna 172. The aircraft had its maiden 
            flight in Bundaberg on the 16th of March.  
            
            Jabiru have increased the Maximum Take Off Weight (MTOW) 
            is now 544Kg  All of the Jabiru kitplane models have been 
            structurally tested to 8.5g. 
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                  Jabiru 3300cc 
                
                  2 Blade Fixed Pitch 
                  Wooden/Composite
                  60" dia x 53" pitch 
                
                  21' 5" 
                
                  7' 2" 
                
                  
                26’ 4" 
                
                  
                86.1 sq.ft) 
                2 
                
                x 
                
                  
                858 lbs 
                
                  
                1197 lbs 
                
                  
                36 USgals 
                
                  
                558sm | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                  
                640ft 
                
                x 
                
                  130kts 
                
                  120kts 
                
                  
                640ft 
                
                  15,000ft | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                  90kts 
                
                  138kts 
                
                  45kts 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
   | 
               
              
 
            
      
      
             | 
        
      
    
    |