Ex Parte MINSHULL - Page 3




              Appeal No. 2003-0371                                                                  Page 3                
              Application No. 09/465,941                                                                                  


              to the Brief (Paper No. 15) and Reply Brief (Paper No. 18) for the appellant's arguments                    
              thereagainst.                                                                                               
                                                       OPINION                                                            
                     In reaching our decision in this appeal, we have given careful consideration to                      
              the appellant's specification and claims, to the applied prior art references, and to the                   
              respective positions articulated by the appellant and the examiner.  As a consequence                       
              of our review, we make the determinations which follow.                                                     
                                                        Claim 1                                                           
                            An aircraft assembly jig loading system comprising:                                           
                     a support member;                                                                                    
                     a plurality of elongate members, each of said elongate members is                                    
                     attached at one end to said support member in spaced apart positions                                 
                     along said support member, each elongate member hanging downward                                     
                     from said support member; and                                                                        
                     at least one releasable holder on each elongate member, the holders                                  
                     positioned to support at least one aircraft stringer at spaced apart                                 
                     positions to enable the stringer to be supported at an aircraft jig for                              
                     loading thereon.                                                                                     
                                         The Rejection Under Section 102(b)                                               
                     The examiner has rejected independent claim 1 and dependent claims 3, 4, 9-11                        
              and 14-16 as being anticipated by Woods.  Anticipation is established only when a                           
              single prior art reference discloses, either expressly or under the principles of                           
              inherency, each and every element of the claimed invention.  See In re Paulsen, 30                          








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