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Airframe Stress Experience should include static and fatigue analysis of primary and secondary airframe structure of metallic or composite construction in a product development environment, finite element modeling, understanding of certification requirements to FAR Part 25 and EASA CS. CATIA V5, NASTRAN, and PATRAN, are desired.
Contributes to planning, developing and coordinating of important engineering projects. Provides specialized technical assistance to team members. Uses advanced techniques and modified extension of theories to provide technical solutions to a wide range of difficult problems. Determines and develops own approach to solutions within schedule and cost objectives. Works under limited supervision; work should only be required. to be reviewed for accuracy and consistency with meeting overall objectives. Actively works to improve daily processes and ensures all work meets customer requirements. Maintains a current knowledge of developments in the field of specialty and/or other related aircraft fields in order to recommend innovations to improve quality and effectiveness of company product.
Education and Experience Requirements
Bachelor's Degree in engineering or related curriculum required or equivalent combination of education and experience sufficient to successfully perform the essential functions of the job. 5 yrs in specific technical discipline or 10 yrs broad eng experience in several technical disciplines with Bachelors. Experience credit considered for related adv degrees limited to 2 yrs for Masters, 4 yrs for PhD in fields applicable to this job.