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      Questair Venture 
      
      
        
      
            
        
            
            The 
            Questair Venture was developed as a two place, all metal, kit built 
            aircraft with the design mission of fast, all weather cross country 
            travel. As a result of its small physical size and large operating 
            envelope several interesting challenges were encountered during the 
            flight testing of the aircraft. The longitudinal flying qualities 
            were tailored to provide the feel of a much larger aircraft through 
            the use of an artificial feel system which also incorporates a trim 
            function. The low speed and stalling characteristics of the aircraft 
            were greatly improved by using a wing leading edge modification. The 
            high speed/flutter characteristics of the aircraft were tested and 
            verified using ground vibration tests and instrumented flight tests. 
            
            Without 
            doubt one of the fastest kit aircraft produced and great success has 
            been enjoyed at Reno Air Races, but the aircraft was never without 
            its problems. 
            
            
              
            
             
             
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                Cont. IO-550-G, 280 hp 
                x 
                16.25 ft. 
                
                x 
                27.5 ft 
                
                x 
                
                x 
                
                x 
                x 
                2000 lb. 
                55 gallons 
                 1,000 nautical miles | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                x 
                2200 fpm 
                x 
                x 
                x 
                x | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                300 knots 
                61 knots 
                
                 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
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