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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
 |  
            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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