Job Description: • Should have Strong knowledge and experience in Aerospace Industry and expertise in Structural analysis ( Both Static and Fatigue) • Hands-on Experience on Aircraft Nacelle components is preferrable. • Should be well-versed with Classical and Finite element analysis approaches. Should able to review and validate the results for both Metallic and Composite structures. • Able to understand the Technical requirements to conceptualize the design through analysis validations and Should have basic understanding on loads and behavior. • Experience on basic design (CATIA) and finite element Tools is must, such as Hypermesh, Nastran, Patran. • Should be able to perform independently and communicate the technical deliverables to Stakeholders. • Should guide and support the team in providing technical assistance in both execution and reviews. • Strong expertise is preferrable in creating Certification documents and stress analysis repots or dossiers. • Knowledge on Automation or skill to develop macro is added advantage. • Strong in Analytical and problem solving skills. • Able to take the ownership & accountability and handle the project with minimum dependency. • Good knowledge on Quality and process improvements implementation skills in project would be advantage.   Basic Qualifications: • Bachelors or Masters in Mechanical engineering, Aerospace or Structural Engineering is preferred. • Relevant experience of 5 - 7 years + in the Aerospace Industry and majorly in Structural Stress Analysis, Product Certification Process