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            H-3 Pegasus 
      
      
        
      
            
             
      
            
            Award-winning cantilevered low-wing monoplane designed by Bert Howland. First flew in
            1988.
            The H-3 is a tube and fabric-covered sport plane with construction 
            methods comparable to the H-2 biplane. However, instead of strut and 
            cable-bracing, the H-3 features a cantilevered wing with a design 
            G-load of +5 to -3.  
             
            It first flew with an engine of 28 horsepower, but normally is built 
            with engines in the 40 to 50 horsepower range now.  
             
            The clean configuration gives it a very impressive cruise speed 
            compared to other very light aircraft. The design won first place 
            awards in its category at the EAA Sun 'n Fun Fly-in at Lakeland, 
            Florida in both 1989 and 1990. 
             
            The designer developed a war bird variant of the H-3 in 1993, based 
            on the P-40 Warhawk of "Flying Tiger" fame. It was designated HP-40, 
            but is not offered now as a separate set of plans. However, H-3 
            builders who wish to opt for this variant can receive supplemental 
            drawings to enable them to make the minor changes.  
             
            One of those, the substitution of tube and fabric wing tips in place 
            of fibreglass tips on the H-3, is an option that many builders 
            choose for the standard H-3. 
             
            Raw materials kit available from Wicks Aircraft Supply. 
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                
                
                Hirth 2704 HP 
                Range50/31-55 
                x 
                
      
                
                15ft 
                
      
                
                4.8ft 
                
      
                
                25ft 
                
      
                
                110sq. ft
            
            
      
                 
                1 
                
      
                
                305lb 
                x 
                
      
                
                575lb 
                
      
                
                7.5gal 
                
      
            
            120n.m | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                
            
            200ft 
                
      
            
            600fpm 
                
      
            
            mph 85mph 
                
      
            
            70mph 
                
      
            
            250ft 
                
      
                
                9500ft | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                x 
                
      
            
            30mph 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
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