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            Lancair Sentry 
      
      
        
      
      
      
        
            
      
            
              
            
            
            The Lancair Sentry. This Walter powered Lancair IV is a 
            military-style tandem seat aircraft with left-side throttle 
            controls, and a rear hinge canopy. 
             
            The aircraft was designed for military training, but is still 
            available for the typical Lancair customer. Only the top segment of 
            the existing Lancair IV fuselage was modified for the new Sentry, as 
            well as portions of the vertical tail. It also offers increased yaw 
            stability and excellent visibility out of a newly designed rear 
            hinge canopy.  
            
            
            Lancair is offering rebuilt Walter 601E turbines with a TBO of 2000 
            hours or new with a TBO of 3000 hours. Currently we are using a 
            prototype 82" 3-blade Hartzell propeller; however, an 84" propeller 
            from AVIA is also available. 
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                      
                      Walter 601D 
                      
                      708 H.P 
                
                      
                      3 Blade, Constant Speed 
                
      
                      
                      26 
                ft 
                
                x 
                
      
                      
                      30.2 
                ft 
                
      
                      
                      98 sq 
                ft 
                2 
                
                      
                      2200 lbs 
                
                      
                      1350 lbs 
                
                      
                      3550 lbs 
                
                      
                      125 gal. 
                
                      
                      1150 Sm | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                      
                      1500 ft 
                
                      
                      4000 fpm 
                x 
                
                      
                      380 mph 
                
                      
                      1700 ft 
                x | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                x 
                
                      
                      74 mph 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
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