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            Grega GN-1 Air Camper 
      
      
        
      
            
             
      
            
            Early in 1958, John W. Grega, EAA 3808, 
            embarked on the Pietenpol Project, the object of which was to 
            modernize the excellent 1933 Model A Ford powered version, to a 
            Continental A-65 powered two-seat "fun plane" with good small field 
            capabilities, using modern straight forward construction methods.
             
             
            With engineering know-how available to him from his then EAA Chapter 
            5, located at the old Welcome Airport in Northfield Centre Township 
            in Ohio, John Grega enlisted the aid of a fellow member to run a 
            preliminary weight and balance on the 65 hp version of the Pietenpol 
            Aircamper. Armed with this data, John Grega, an experienced 
            woodworker, proceeded to design a new fuselage structure employing 
            Piper J-3 motor mount, landing gear, control assembly, and tail 
            wheel assembly. Using a GN modified clip wing off a J-3 Cub, for 
            which the original fuselage designed was intended.  
             
            Along with the use of a J-3 wing, an improved and modernized version 
            of the original Pietenpol Aircamper wing was initiated, lending 
            versatility to the design. The original airfoil was redesigned with 
            a more rounded leading edge for better stall characteristics, the 
            truss was improved for more strength, and spars were relocated for 
            greater depth and in keeping with modern designed parameters. 
            Construction of the GN-1 prototype was immediately started after the 
            original drawings were completed. This was to the be the J-3 wing 
            version. John Grega finished and was flying his GN-1 prototype, 
            N4705G, in 1963.  
             
            Selling plans on the GN-1 Aircamper was the furthest thing from John 
            Grega's mind, until a small article appeared in the June 1960 issue 
            of Sport Aviation, regarding the fact that the GN-1 was under 
            construction. From that time on, the amount of mail received by John 
            Grega was overwhelming, all letters expressing the desire to 
            purchase plans for the GN-1, if and when available. Most requested 
            parts were drawn up and sent out so construction could start. All 
            sketches, doodles, and bits and pieces of construction were 
            correlated into a set of drawings, first pencil tracings, and as 
            construction problems arose, they were resolved and incorporated 
            into a finished set of drawings. The finished set being officially 
            copyrighted in 1992, by John W. Grega.  
      
              
      
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                
            
            Cont. HP 
                Range65/65-90 
                x 
                
                
                18.1ft 
                
                
                6.8ft 
                
                
                29ft 
                
                
                145sq. ft
            
            
      
                 
                2 
                
                
                650lb 
                x 
                
                
                1100lb 
                
                
                12gal
            
            
      
                 
                
            
            400n.m | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                
            
            300ft 
                
            
            500fpm 
                
            
            115mph 
                
            
            87mph 
                
            
            300ft 
                
            
            12,000ft | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                x 
                
            
            25mph 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
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