| 
       
      
        
      
      
      
      Colomban Cri Cri 
      
      
        
      
        
      This 
      aircraft was designed by the French aeronautical engineer, Michel Colomban 
      in the early 1970's. It first flew on July 19, 1973 with two 9 hp Rowena 
      engines.The engines for the Cri 
      Cri have always been it's weakness. Since the first Rowena 9hp chain saw 
      engines were attached better engines have been sought after. Quickly, the 
      designer, needed larger engines and found the Valmet and then the JPX PUL 
      212.  
      The 1998 version of the Cri Cri, the "MC 
      15 S", has a pair of 15hp single cylinder Solo 210 engines. Even with this 
      hopefully better engine, builders seem to be continually searching for 
      more horsepower, more reliability and less weight while balancing this 
      with cost. The eternal struggle in picking aircraft engines is the 
      quintessential problem for the Cri Cri.  
      Since the design was first released in 
      the early 80's more engine choices have become available from many areas. 
      Industrial engines, go-karts, motorcycles, parasailing, radio control, 
      drones, chain saws and turbine applications. Even though many of these 
      engines have many redeeming qualities one must never forget that the 
      environment of flight does put unique demands on engines. Many of these 
      engines are designed to be land based, stationary engines and therefore 
      have not anticipated the rigors of flight. The quality of these engines 
      should become evident when you look at durability and reliability. Simply 
      put, they were not designed for the job.  
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                2 x 15 Hp 
                
            Fixed pitch propellers 
                12 ft 10 in 
                
                x 
                16 ft 
                34 sq ft 
                1 
                160 lbs 
                x 
                380 lbs 
                6 US gals, 35 lbs 
                345 miles | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                400 ft 
                1200 fpm 
                127 mph 
                115 mph 
                x 
                16,000 ft+ | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                160 mph 
                42 mph 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
   | 
               
              
 
      
      
            |