Candidate should have 6 to 10 years of good working experience on stress analysis of Aircraft structural (Primary and Secondary) components. • Candidate should have positive knowledge in Aerospace domain. Candidate should be able to co-ordinate with concerned stakeholders’ teams. Profound knowledge on Stress analysis, aircraft loads and aircraft structures are expected.
Job requirements
- Experience with Boeing component design ( Fuselage structure , Systems, Pylons, Nacelles)
- Good hands-on experience with any FE tools like Patran/Hypermesh
- Profound knowledge on Stress analysis, aircraft loads and aircraft structures are expected.
- Excellent knowledge on MS tools is mandatory.
- Boeing standards experience is preferred
- Experience in the preparation of stress reports.
- Boeing Inhouse tools. MSC Nastran Patran is an additional advantage, Basic knowledge on Catia V5.