Job Description

•Lead and Perform Static, Fatigue and Damage Tolerance (FDT) stress analysis of primary and secondary aircraft structures using classical hand calculation and Finite Element Analysis (FEA).•Should be having metallic and composite structure stress analysis working experience.•Understanding of load paths, extraction of loads from Finite Element Models (GFEM/DFEM).•Determination of critical failure modes and performing analysis to ensure structural integrity.•Mitigation techniques for low margins of safety•Preparation of stress dossiers as per certification requirements•Review and validate Stress analysis output and Stress Dossiers to ensure compliance with technical requirements.•Drive issue resolution by interfacing with cross functional teams (Design, manufacturing, quality, configuration management, etc.).•Serve as a technical representative for onsite offshore coordination, addressing queries, clarifications, and technical escalations.•Applicant sh...