
      
            The Firefly which is a part 103 legal 
            ultralight, when powered by the Rotax 447 engine, takes about 150 
            hours to build from kit form. 
      
            The FireFly was first introduced in 
            1995. It features a welded steel fuselage, folding wings, full span 
            flaperons, steerable tail wheel, spring steel landing gear, 5 gallon 
            fuel tank and 2 blade wood prop. 
      
            Options include brakes, full enclosure, 
            ballistic parachute, instrument, composite prop, strobe light. The 
            craft is available in several quick build kits, partial kits and 
            fully assembled.
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                
                447 Rotax 
             
                x 
                
                x 
                
                x 
                
            
                22 ft. 
                
            
                117 sq. ft. 
             
                1 
                
            
                250 lbs. 
                x 
                
            
                500 lbs. 
             
                
                x 
                
                x | 
               
             
            
            performance 
            
             
            
              
                
                takeoff 
                distance, ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                x 
                
                x 
                x 
                
            
                60 m.p.h. 
            
                 
                x 
                x | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design 
                manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                
            
                80 m.p.h. 
            
                 
                
            
                24 m.p.h. 
            
                 
                x | 
               
             
            All specifications are based on 
            manufacturer's calculations 
   |