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            Jabiru J400 
      
      
        
            
            
              
            The Jabiru J400 (4 seater)  has 
            evolved from combining the best features of the LSA, SP & UL models 
            all put together & coming up with a new clean sheet design that has 
            combined features. It comes with the standard LSA wing span with
            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 J400 was developed as a great 
            replacement to the GA alternatives i.e. Cessna 172. The aircraft had 
            it's maiden flight in Bundaberg in the 16th of March as a two seater. 
            The flight testing as a four seater has been completed with great 
            results. 
            The Jabiru J400 will cruises at 115 knots on 20 
            litres/hour, depending on the options selected. 
            Jabiru have increased the Maximum Take Off Weight 
            (MTOW) is now 700Kg  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 
                
                  693 lbs 
                
                  847 lbs 
                
                  1540 lbs 
                
                  36 gals 
                
                  828 sm | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                  960ft 
                
                  1000 ft/min 
                
                  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 
                
                  48kts 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
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