Perform damage tolerance, fatigue, and static analysis and testing for aircraft structure utilizing fundamentals of fatigue and fracture mechanics, non-linear finite element modeling, and DaDT material allowable. Employ standard solutions to substantiate aircraft structure life and safe operating intervals and develop sound nonstandard methods and approaches to solve complicated aircraft structure problems where established solutions are insufficient. Generate structural substantiation and engineering reports in compliance with FAR requirements, and participate in Preliminary Design Review (PDR) and Critical Design Review (CDR). Review engineering change, interpret technical specifications, assess means of compliance, and disposition non- conforming manufactured par