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Structural Engineer with 9+ years in Aerospace Structural Analysis & FEA
Lead Structural Analysis Engineer with 10+ years of experience in stress analysis, finite element analysis (FEA), fatigue & damage tolerance, and structural integrity assessment of aero-engine metallic structural components. Experienced in production non-conformance analysis, stress liaison support, repair substantiation, certification, and airworthiness compliance for aerospace structures. Strong background in static strength, vibration, fatigue life, and fracture mechanics analysis using ANSYS Workbench, ANSYS APDL, HyperMesh, and classical hand calculations. Experienced in cross-functional collaboration with design, manufacturing, quality, and service engineering teams to resolve structural and airworthiness issues. Supported FAA compliance, certification, and airworthiness requirements through structural substantiation and analytical assessments. Provided technical guidance and mentoring support to junior engineers and team members on structural analysis methodologies and best practices.
Sha-Shib College of Engineering, Chikkaballapur
Β.Ε · Aeronautical Engineering
N/A – June 30, 2014
QuEST Global (Currently working at IHI Japan Aerospace)
Lead Structural Analysis Engineer
June 1, 2017 – Present
Hamura-shi, Tokyo, Japan
Nonlinear Structural Integrity Assessment – No.5 Bearing Housing
June 14, 2026 – Present
No. 5 Bearing Housing – Fan Blade-Off (FBO) Compliance Analysis. Conducted nonlinear FEA on No. 5 bearing housing assembly to validate compliance with fan blade-off criteria per airworthiness standards. Applied test loads and nonlinear material properties in FE tools such as SIESTA/ANSYS/HyperMesh to evaluate structural strain response. Collaborated with test teams to align simulation with physical test plans. Validated structural integrity and strain response of housing assembly under worst-case loading conditions. Evaluated structural margins and failure modes under extreme load conditions. Prepared substantiation evidence and acceptance reports for component certification and compliance.
Production Non-Conformance, Concession Analysis & Structural Disposition
June 14, 2026 – Present
Nonconformance issues due to manufacturing or aftermarket services. Evaluated manufacturing non-conformances and defined disposition: Accept-As-Is, Repair, or Reject. Performed static strength assessment (MoS) using classical hand calculations and FEA to ensure structural integrity. Conducted fatigue & damage tolerance (F&DT) analysis to verify life requirements. Performed crack growth / fracture mechanics analysis and defined safe inspection intervals. Developed repair substantiation and structural disposition solutions aligned with airworthiness requirements. Collaborated with design, manufacturing, and quality teams for disposition decisions. Prepared stress justification reports and MRB documentation supporting airworthiness compliance, FAA CFR Part 25 & 33 compliance support. Developed structural repair substantiation and disposition recommendations for manufacturing and in-service structural discrepancies. Conducted root cause analysis for recurring non-conformances. Performed stress liaison activities and structural substantiation for production non-conformances, manufacturing deviations, and concession requests. Managed multiple structural disposition activities within schedule-driven aerospace programs. Supported technical coordination and knowledge sharing across offshore engineering teams.
Cultural Fit Analysis
The candidate's experience working with global engineering teams and coordinating with offshore teams suggests a good cultural fit for organizations that value diverse collaboration and distributed work models. Their involvement in mentoring junior engineers indicates a willingness to contribute to team growth and knowledge sharing. The projects demonstrate a strong commitment to aerospace industry standards and compliance, which aligns well with a safety-critical engineering culture. The breadth of skills and project types, from nonlinear FEA to production non-conformance, shows adaptability and a comprehensive understanding of the structural engineering lifecycle in aerospace.
Soft Skills & Operational Fit
The candidate demonstrates strong soft skills in cross-functional collaboration, stakeholder communication, and team coordination, as evidenced by their project descriptions and experience. Their role as a Lead Structural Analysis Engineer also indicates leadership capabilities, including technical guidance and problem-solving. The experience with offshore engineering teams suggests adaptability to distributed work environments and effective communication across different locations and time zones. The focus on airworthiness compliance and root cause analysis highlights a detail-oriented and methodical approach to engineering challenges.