| 
   
   
     
       
         | 
       
      
        
      
            
      
      
            Super Stallion 
      
      
        
      
      
            
            
              
            
            The Super STALLION boasts over 90 miles per gallon 
            per seat passenger mile. No other aircraft comes even close. The 
            Boeing 747 is the most efficient airliner with 50 mpg per seat 
            passenger mile. The Super STALLION has a flat plate drag area of 2.8 
            sq.ft. which is close to that of a Glasair III which can carry only 
            two people. The Super STALLION carries six. 
             
            With this low drag, the cruise speed for the Super STALLION is close 
            to 200 knots with a 300 hp, IO-550-G. The Super STALLION gives you 
            the performance of a twin, turbocharged engine aircraft at the cost 
            of a non-turbocharged, single. On top of that! The operating and 
            maintenance costs are less than one third. The fuel burn at cruise 
            is 14.5 gallons per hour at 12,500 feet while carrying two or six 
            people. Add the payload of 1,100 lbs (six people or four people and 
            baggage) and a large quantity of fuel and plenty of room inside, and 
            you can see why we offer you an aircraft that is unequalled in the 
            aviation industry. With a total of 180 gallons of fuel, includes 20 
            gallons of fuel for climb-out and reserve, the Super STALLION has a 
            range of 2,500 sm. 
             
            With a large cabin and large cargo door, loading items such as 
            camping gear, motorcycle, bicycles, aircraft engines, 55 gallon 
            drum, and household furniture is easy. 
            
              
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                 Lyc. 
                
                  IO-550-G.300 hp @ 2700 rpm. 
                
                  McCauley or Hartzell, 3 bladed, 
                  constant speed. 
                
            
                  25.0 ft 
                
            
                  9.50 ft 
                
            
                  35.00 ft 
                
                x 
                
                x 
                
            
                  2,200 
                lbs 
                
            
                  1,100 
                lbs 
                
            
                  3,800 
                lbs 
                
            
                  180 gals 
                
            
                  2,200 
                n.m.  | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                
                  1,800 ft 
                
                  1,600+ fpm 
                
                  
                220 knots 
                
                  
                200 knots 
                x 
                x | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                x 
                
                  
                62 knots 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
   | 
               
              
 
            
      
             
            
             | 
        
      
    
    |