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Responsible for performing structural analysis of aircraft components, assemblies, and systems while working as an integrated team
Structural analysis includes calculation of loads, Static analysis, Fatigue analysis, Damage-Tolerance analysis, and Vibration analysis
Evaluate structural integrity of aircraft components by way of classical hand calculations and, finite element method
Generate documentation to report analysis results to support certification
Basic Qualifications:
Bachelors or Masters in Mechanical/Aerospace engineering
5-10 years of relevant experience
Experience with structural analysis of metallic and composite various airframe structures
Experience is providing the Quality Notification Stress dispositions and well wersed with the repair methedologies
Experience with static and fatigue analysis
Robust understanding of engineering fundamentals such as material properties, Free-body diagrams, loads and, analysis methods
Experience in utilizing FEM software (e.g., PATRAN/NASTRAN, Hyperworks)
Candidate demonstrates excellent analytical and problem-solving skills
Good verbal and written communication skills to liaise with several Stakeholders
Ability to work across functional teams and organizations

Keyskills: NASTRAN Structural Analysis Hand Calculation Airframe Structures Patran Fatigue Analysis Finite Element Analysis Static Analysis FEM
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