-Preparation of strength analyses (static, LCF, HCF, fatigue, over-speed, FBO, crack propagation) of aero engine components (compressor, combustion chamber, turbine – static / rotative parts) using FEA (ANSYS Workbench or other) and analytical methods
-Assessment of non-conformities related to aero engine components and their effects on the product
-Technical validation (authorization for approval) of concessions related with visual, dimensional and process non-conformities of aero engines components
-Day-to-day cooperation with internal and external stakeholders from design, technology, quality and manufacturing at various stages of implementation and serial production
-Technical support to other departments for process improvement
-Defining technical solutions (request for drawing change, Production Permit, process optimization) to eliminate non-conformities on products
-Continuous improvement of existing tools and methods

-Language: English, B2
-MSc/BSc degree in engineering
-Teamwork, analytical thinking, self-motivation, ‘can-do' attitude and decision-making skills
-Ability of technical drawing interpretation
-In-depth understanding of the Theory of Elasticity, Fatigue Strength and related topics
-Professional experience as a mechanical engineer / stress engineer / FEA engineer preferably in aerospace industry
-ANSYS, Abaqus, Nastran (Patran) or HyperWorks experience

Optional
-Catia V5 experience
-Solid Edge Experience
-Language: French
-Design and GD&T experience will be considered a plus
-Knowledge of design and operation of aircraft engines