Detail stressing of components and mechanisms according with Airbus procedures, standards and methods
Job Summary
Detail stressing of components and mechanisms according with Airbus procedures, standards and methods.
Application of finite element method or classical analysis methods to predict the failure modes of aircraft metallic and composite structures.
This job requires an awareness of any potential compliance risks and a commitment to act with integrity, as the foundation for the Company’s success, reputation and sustainable growth.
Matching Summary
Detail stressing of components and mechanisms according with Airbus procedures, standards and methods.