Structural Analysis Engineer - Aircraft Systems
Boeing
Rzeszów, Poland
Primary Responsibilities:
- Perform structural analysis of aircraft systems. Structural analysis includes calculation of loads, static and fatigue analyses;
- Evaluate structural integrity of aircraft components by way of classical hand calculations;
- Generate documentation (stress check notes) to report analysis results to support certification and qualification processes;
- Support in-service products by investigating failures and analyzing improvements. Develop repairs for Aircraft Systems elements;
- Work with regulatory framework (FAA) for warranting safety and regulatory compliance;
- Represent the engineering community in the build through post production environment;
- Technical rigor and focus on excellence;
- Plan, perform and lead detailed structural analysis (static strength, durability/fatigue and damage tolerance);
- Develop new materials, methods, tools, and designs to support future programs;
- Lead a team of stress analysts and provide coaching across all levels.
Basic Qualifications:
- 9+ years work experience in structural analysis engineering;
- Bachelor of Science degree in Engineering (with a focus on Mechanical, Civil, Aerospace Aeronautical or Material Sciences);
- Strong knowledge of engineering fundamentals such as material properties, free-body diagrams, load path, structural loads, joints and structural analysis methods;
- Strong knowledge of strength of materials (hand calculation, analytical methods) approach;
- Strong knowledge of aircraft design philosophy;
- Experience in structural analysis of metallic or composite structures;
- Experience in static and fatigue analyses;
- Solid communicator, Upper-intermediate level or higher in both written and verbal English;
- Readiness to work with multi-functional team in a flexible schedule (weekends/holidays support, overtime, shifted work schedule) to meet the business needs;
- Readiness for business trips – up to 25% of working time.
Preferred Qualifications:
- Experience in static, fatigue and damage tolerance analyses;
- Proven experience in structures engineering;
- Experience in leading a team of stress analysts;
- Knowledge of Boeing aircraft structures;
- Knowledge of finite element method approach;
- Experience in FAA regulations (14 CFR Part 25 & 26);
- Experience in CAD/CAE systems (Catia, Nastran/Patran).
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