| 
   
   
     
       
         | 
       
      
        
      
      
            
            Cassutt 3M 
      
      
        
            
             
            
            The Cassutt is a 
            single place, full cantilever, high performance aircraft. It is 
            fully aerobatic and meets the specifications for competitive racing, 
            “G” loading, safety characteristics and visibility.  
             
            It is powered by the Continental 0-200, 100 H.P. engine. It’s 
            economical and fuel efficient, cruising at 185-200 MPH at 
            approximately 6 gallons per hour.  
             
            The mid wing design and has a proven history since “The Golden Days 
            of Racing”. It will do any manoeuvres that the little biplanes can do 
            and take you cross country in no time.  
             
            It’s construction of steel tube, wood, fabric and fibreglass make it 
            one of the easiest aircraft to build. It is available as a kit, 
            plans or parts for the builder to choose what level of construction.
            
            
            
             
            
            Construction  
             
            Chrome moly steel tubing for fuselage and control surface 
            construction. Truss construction for strength and durability, also 
            provides easy access for inspection and repair. The fuselage is 
            fabric covered from the cockpit aft and has molded fibreglass 
            cowlings from the cockpit forward. 
             
            The wing is constructed of a one piece spruce spar, 3 ply laminated 
            with a one piece spruce rear spar. Truss ribs built of spruce with 
            skins comprised of four sheets of 3 ply plywood. 
             
            One piece spring steel landing gear, bolts to the fuselage with four 
            bolts. 
             
            Full span ailerons driven by two push rods within the fuselage. 
             
            Stabilizer and elevator are one piece tube assembly. Stabilizer 
            mounts to longeron with four bolts and elevator mounts to stabilizer 
            with three hinges. 
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                
                
                Cont. 0-200   
            
                
                100hp 
                x 
                
            
                
                16ft 
                 
                
            
                
                4ft 
                 
                
            
                
                15ft 
                 
                
            
                
                67.5sq. ft 
                 
                1 
                
            
                
                550lb 
                
                 
                x 
                
            
                
                900lb 
                
            
                
                15gal 
                
            
                
                450n.m 
                 | 
               
             
            
            performance 
            
             
            
              
                
                takeoff 
                distance, ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                
                
                450ft 
                
            
                
                500fpm 
                
            
                
                235mph 
                
                 
                
            
                
                190mph 
                
                 
                
            
                
                650ft 
                
                 
                
            
                
                16,000ft | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design 
                manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                x 
                
            
                
                65mph 
                x | 
               
             
            All specifications are based on 
            manufacturer's calculations 
   | 
               
              
 
      
          | 
        
      
    
    |