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            Skylite 
      
      
        
      
      
              
      
      
      
      
            The Skylite design was started in 1988 by Ed Fisher, who wanted a 
            rag & tube ultra light aircraft with the classic parasol wing 
            configuration. He wanted an inexpensive to build, open cockpit 
            tail-dragger that would appeal to the average handyman. The Skylite 
            prototype was built, tested and debuted to the public at Oshkosh 
            1991, where it received the Grand Champion Award for Ultralights. 
            Since that time, over 90 Skylites have been built and flown, and 
            Raceair Designs continues to sell plans and components, and supports 
            builders.  
             
            The Skylite design prototyped Ed Fisher's wing rib attach cup and 
            rib angle construction for lightweight wing design, and all 
            subsequent ultralight type designs from Raceair have employed this 
            method of wing rib construction.  
             
            Ed Fisher owns Raceair Designs and is the designer and sells plans 
            for the Skylite, Micro Mong, and many others. Currently Raceair 
            offers plans and components for the Skylite, and plans for the Mong 
            Sport.
            
             
      
      
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                Rotax 277 / 28 
                hp 25-48  
                x 
                17.60 
                ft. 
                
                x 
                29.20 ft 
                117.0 
                sq. ft.  
                1 
                245 lbs. 
                
                250 lbs.  
                525 
                lbs.  
                
                x 
                120 sm | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                350 ft 
                400 fpm  
                x 
                
                45 mph  
                
                350 ft.  
                
                8,000 ft.  | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                
                60 mph  
                
                27 mph  
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
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