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            Carlson Criquet 
      
      
        
            
            
              
      
            Features take-off and landing unique 
            onto itself. This airplane responds with outstanding execution on 
            bearing mounted controls. Uncomely in appearance and uncommon in its 
            discipline, it is now available to you as the Carlson Criquet, a 3/4 
            scale of the original German Fieseler Storch. 
             
            The Carlson Wing, admired in their previous designs, has been 
            adapted to the Criquet. It has a strong, serviceable framework 
            holding 20 gallons of fuel in each wing (plus a header tank), 
            maintains a slatted S.T.O.L. leading edge, and fully supports the 
            controls necessary for low and slow manoeuvrability. Thorough 
            testing has proven the drooping ailerons and flaps work best when 
            controlled independent. The safety advantage when landing in 
            uncertain cross wind conditions far outweigh the old tandem concept 
            of long ago and its perceived benefit of using one control. 
             
            Originally designed as a utility aircraft, the possibilities of 
            service in photo work, low level reconnaissance or related activity 
            is immeasurable. With panoramic visibility all around and through 
            slanted downside side windows, it can slowly descend to land with 
            exceptionally short roll out. Truly, a joy of ultimate control on 
            take-off and landing. 
             
            Oleo strut shocks facilitate tough field landings. The full door 
            features a pneumatic lift to make the rear seat easily accessible. 
            The profile images the original with its long slender cowl. Present 
            day technological advances have affirmed this old and studied work 
            horse full status in the present as a light weight, exceptional 
            classic. 
      
            
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                      140 HP w/ Walter Lom 
                x 
                
                      24 
                      
                ft 7 
                ins 
                
                      8 ft 5 
                ins 
                
                      36 
                      
                ft 0 
                ins 
                
                x 
                      2 
                
                      1050 
                lbs 
                
                      900 
                lbs 
                
                      1950 
                lbs 
                
                x 
                
                      40 gallons Plus 2 
                      gallon header tank 
                x | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                
                      75 
                      
                ft 
                
                x 
                x 
                
            
                      95 
                mph 
                
            
                      75 
                      
                ft 
                x | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                
            
                      135 
                mph 
                
            
                      21mph 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
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