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            Ikarus C42 
      
      
        
      
      
        
            
            
            The best-selling microlight-type aircraft in Germany is the 
            Ikarus C42, manufactured in southern Germany by the Comco-Ikarus 
            company. The C42 was first produced in 1997, and there have 
            now been over 400 of these aircraft delivered. At present, 
            approximately 80 Ikarus C42's are produced annually with 
            about 50 being sold in Germany and about 30 being delivered in other 
            countries around the world. In Germany, the C42 now sells in 
            almost four-times the numbers each year as its nearest competitor. 
             
            The C42 has new features and improvements for 2002! The
            C42 now has a more streamlined cowling with a new air intake 
            system -- providing better efficiency and performance and 
            incorporating an effective carb anti-icing system. The Ikarus C42 
            is available with several wing colour combinations and fuselage 
            graphics packages.
            
        
            
            Ikarus C42 features and equipment . . . 
              
            
             
            two-seat (side-by-side), high wing, tricycle-gear aircraft
               
            
             
            wide, roomy cockpit with great visibility 
               
            
             
            composite shell fuselage with laminated-fabric wing sails 
               
            
             
            heavy duty suspension on all three wheels 
               
            
             
            steerable nosewheel and hydraulic disk brakes on the main 
              wheels  
            
             
            powered by the Rotax 912, 80-hp four-stroke, four-cylinder 
              engine (912S 100-hp engine is optional)  
            
             
            three-blade Warp Drive prop with spinner 
               
            
             
            stainless steel exhaust system  
            
             
            special airbox design with carb heat system
             
            
             
            cabin heater and adjustable vents in side windows 
               
            
             
            ergonomically-shaped cushioned seats  
            
             
            gull-wing doors equipped with gas-lift struts and doors 
              quick-removable (for flying without doors!)  
            
             
            door locks and floor mats  
            
             
            elevator trim and flaps  
            
             
            aerodynamic main wheel and nosewheel pants  
            
             
            fuel filler cap conveniently located (no climbing on ladders!)
               
            
             
            large instrument panel with special tilt-out design for easy 
              access  
            
             
            deluxe instrumentation including: airspeed indicator, 
              0-20,000' precision altimeter, vertical speed indicator, Silva 
              compass, slip indicator, electric fuel gauge, and E.I.S. digital 
              engine monitoring system which provides for 
             
            engine rpm, oil 
              temperature, oil pressure, water temperature, flight timer, total 
              flight hours meter, and voltmeter (and with warning light to 
              indicate if any engine parameter exceeds programmable limits)
               
            
             
            includes standard fuselage graphics with many other graphics 
              packages available  
            
             
            folding wings available as a low-cost option 
               
            
             
            options available include BRS parachute recovery system and 
              Full Lotus floats  
            
             
            the C42 is factory-built in Germany and test-flown in Germany 
              and the U.S. before delivery!  
            
              
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                
                Rotax 9125 100hp  or 
            
            
                Rotax 912UL 80hp 
                x 
                
      
                
            20ft 4in 
                
      
                
            7ft 7in 
                
      
                
            31ft 
                
                x 
                
                x 
                
      
                
            260kg 
                x 
                
      
                
            450kg 
                
      
                
            50 ltr 
                
            
                400 
                miles | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                
                
                258ft 
                
            
                
                1300fpm solo
            980fpm max weight 
                
            
                
                116mph 
                
            
                
                105mph 
                x 
                x | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                x 
                
            
                
                39mph 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
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