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      General Avia F-20 Pegaso performance 
      and specifications 
      
        
            
            
            
                              
                              History 
                              
                              In January 1970 Dott. Ing. Stelio Frati, renowned 
                              as a freelance designer of a series of successful  
                              light aircraft built by manufacturers such as 
                              Ambrosini, Aviamilano, Caproni, Pasotti, Procaer 
                              and SIAI Marchetti, established Construzioni 
                              Aeronautiche General Avia to construct prototypes 
                              of his designs. The first new type to be developed 
                              at the Milan workshops was the F-20 Pegaso, a 
                              six-seat twin-engined light executive transport 
                              aircraft. Work on the first prototype commenced in 
                              September 1970; it was first flown on 21 October 
                              1971, and a second prototype, slightly larger and 
                              heavier than the first, flew on 11 August 1972.
                               
                               
                              Contemporaneously with the establishment of General Avia, a 
                              publisher Dr. Gianni Mazzocchi was setting up 
                              Italair SpA to provide development, manufacturing 
                              and marketing facilities for light single- and 
                              twin-engined aircraft, and this organization took 
                              over the two prototypes to conduct the 
                              certification programme  in anticipation of 
                              production. Type approval was granted by the RAI 
                              on 19 November 1974, and by the FAA on 14 May 
                              1975. By agreement production was handed back to 
                              General Avia and the first Aircraft flew on 17 
                              December 1979, incorporating a number of minor 
                              changes which included improved cabin heating and 
                              sound-proofing and the substitution of three blade 
                              Hartzell propellers for the original two blade 
                              units.  
                               
                              A four seat military version is available as the F-20 Condor, 
                              which can be fitted three stores pylons under each 
                              wing the central carrier accepting a 50 Imp. gal. 
                              fuel tank. Military roles include long range 
                              maritime surveillance, search and rescue, and 
                              weapons training. The specification applies to the 
                              General Avia F-20 Pegaso.  
      
            
                                
                              
                              Specifications 
                               
                              
            
      
       
        
         | 
         Powered by | 
         Two 300 hp 
         Continental IO-520-K | 
         
        
         | Propeller | 
         Hartzell constant speed | 
         
        
         | Wing span | 
         33' 11" | 
         
        
         | Length | 
         26' 10-3/4" | 
         
        
         | Wing area | 
         172.4 sq ft | 
         
        
         | Gross weight | 
         5,070 lbs | 
         
        
         | Empty weight | 
         3,086 lbs | 
         
        
         | Accommodation | 
         5-6 seats | 
         
        
         | Maximum speed | 
         242 mph | 
         
        
         | Maximum cruise speed | 
         230 mph | 
         
        
         | Economy cruise speed | 
         220 mph | 
         
        
         | Stall speed | 
         72 mph | 
         
        
         | Rate of climb | 
         2,000 fpm | 
         
        
         | Service ceiling | 
         20,500 ft | 
         
        
         | Maximum range | 
         1,110 sm | 
         
        
       
      
                                                      
                                                      
                                                
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