Primary responsibilities for this position include
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.
Perform the Static, Fatigue and DT analysis using classical hand calculations methods.
Understand the structure and come up with analysis approach to qualify/certify the part under minimal guidance.
Evaluate structural integrity of aircraft components by way of classical hand calculations and, finite element method.
Generate documentation to report analysis and, test results to support certification/qualification.
Support Gated Reviews to validate the quality and completeness of work packages.
Familiar with regulatory framework (FAA and Mil-Spec), for warranting safety and regulatory compliance.
Basic Qualifications (Required Skills/Experience)
Bachelors or Master’s degree in Mechanical/Aerospace/Applied Mechanics/Structural engineering and 9 to 12 years of experience in stress analysis.
Must have experience working with cross-functional teams spread across multiple products and locations within Boeing and external partners.
Must be flexible, with a high tolerance for organizational complexity and ability to work with partners from within Boeing and outside, across different cultures and time-zones.
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Communication – strong written and verbal communication skills, ability to prepare comprehensive reports, proposals. Candidate must be fluent in English, and familiar with MS Office tools.
Candidate must be a self-starter with a positive attitude, high ethics, and a track record of working successfully under pressure in a time-constrained environment.
Candidate must demonstrate excellent analytical and problem-solving skills
Ability to mentor and teach subordinates and partners to accomplish project and departmental goals and objectives.
Preferred Qualifications (Desired Skills/Experience)
Experience in structural analysis of various airframe structures.
Experience with structural analysis of metallic and composite structures.
Experience with static and fatigue analysis
Knowledge of airplane operating environments
Robust understanding of engineering fundamentals such as material properties, Free-body diagrams, structural loads and analysis methods
Experience in utilizing FEM software (e.g., ABAQUS, PATRAN/NASTRAN, Hyperworks)
Experience or training with computer programming languages (e.g., Matlab, Python, Visual Basic)
Experience in utilizing industry CAD systems (e.g., NX/Teamcenter and CATIA/ENOVIA)
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
Willingness to expand into technical areas without prior experience
Desire to continuously improve our airplanes
Typical Education & Experience
Bachelors or Master’s degree in Mechanical/Aerospace engineering and 9 - 12 years of experience in stress analysis.
