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            Magnum Pickup 
      
      
        
      
            
       
            
      Designed by Terrence 
      O'Neill, President OAC, Magnum is a bush-type, originally designed to 
      suggestions offered in response to a questionnaire which was sent to all 
      Charter (bush) pilots in Alaska in 1981.  Some 22% of all Alaskan Charter 
      pilots replied.  Magnum was flown to Oshkosh back in 1944 with 
      swing-wings.  It was modified in 1986 to swingtail-loading and an 
      aero-converted Ford 351W, later supercharged to 380-hp. 
            
      Wing sweep is variable by 
      modifying the length of the front auxiliary wing mount lug.  This allows a 
      builder to compensate for different weight powerplant installation, by 
      swing the wings forward or aft, to place the mean aerodynamic chord in the 
      correct location over the CG, and no ballast is required.  Brake masters, 
      battery, etc., for service are out in the open for easy maintenance 
      access.  Tail can be made to swing open (Swingtail option) to load bulky 
      cargo, such as four-by-eight plywood sheet flat-on-the-floor, or a 
      snowmobile, or ATV.  Opening: 48.5" w. by 36" ht.   Roll control by 
      Robertson-type spoilerons for STOL aircraft. Large flaps, spanning 12 ft. 
      on each side, deflect downward 55 degrees. Horizontal stabilizer has 
      unique two-position slots which prevent tail-stall to flight angles of 
      attack of about 30 degrees, thereby  retaining un-stalling power of the 
      tail.  Slots also work to supply more pitch control margin when the full 
      flaps are deflected.  All fuel is carried in a single external under cabin 
      instantly DROPPABLE gas tank, to greatly increase passenger safety in the 
      event of a forced landing.  Angle of Attack Indicator plans are included, 
      and strongly urged to be installed, for safety.
      
      
            Large cargo loading via swing tail; cabin
            can carry 4x8 plywood flat on floor or a snow-mobile in cabin. 
            
      Plans built
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                
                
                Ford 351 cu. in. HP 
                Range380/350-450 
                x 
                
            
                
                25.67ft 
            
                 
                
                x 
                
            
                
                36ft 
            
                 
                
            
                
                189sq.ft 
                2 
                
            
                
                1900lb 
            
                
                 
                x 
                
            
                
                3800lb 
                
            
                
                110gal 
                
            
      
            875n.m 
            
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            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                
                
                1000ft 
            
                 
                
            
      
            2000fpm 
                
            
      
            180mph 
                
            
      
            140mph 
                
            
                
                1000ft 
            
                
                 
                
            
                
                20,000ft 
            
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            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                x 
                
            
      
            61mph 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
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