Job Description:

MAIN ACTIVITIES

• Stress analysis of metallic, composite & hybrid structures, using Airbus Defence & Space methods, potentially from concept and structural development to certification and in-service maintenance.
• Sizing of the structural components, parts and assemblies from static point of view.
• Analyse and validate at component level for static strength and produce relevant strength margins or reserve factors according to validated and applicable Airbus methods & sizing processes.
• Perform detailed analysis in CAD/CAM or (software) implementation on component/ equipment/ mechanical/ software level to the specifications required.
• Continuous support/interaction with design and multifunctional teams during design process.
• Understand the overall stress environment for a system/ sub-system/ components/ equipment architecture, for analysis/testing to provide verification and validation.
• Supply outputs to support planning, organization and execution of testing, verification and validation.
• Provide stress analyses for the repair/acceptance of damaged structures.
• Understand and integrate technologies in the domain of metallic and composite materials.

RESPONSIBILITIES

• Stress analysis of structural parts, components and installations as well as integration of systems and equipment.
• Structural mechanics support to our products for the complete life cycle from concept phase to qualification and in-service support.
• Stress analysis by means of FEM techniques (preparation, validation and assessment of results) and application of traditional stress justification methods and tools.
• Definition of interfaces, functional and worst case analysis, trend and sensitivity analysis.
• Preparation of analysis reports and statements to support flight clearance and certification.
• Assessment of damages and development of repairs, generation of repair instructions and definition and analysis of structural changes.
• Assistance and local support to manufacturing and assembly lines and evaluation of concessions and deviations.

SKILLS REQUIRED

• University Aeronautical Engineering Degree or equivalent
• Knowledge of structural analysis in general and design details of airframe desirable.
• Ability to understand and perform static calculation within metallic & composite structure according to Airbus methods and sizing processes, including FEM techniques.
• Ability to provide stress analyses for the repair/acceptance of metallic & composite damaged structures.
• Ability to understand and integrate technologies in the domain of metallic & composite materials
• Fluent English language

This job requires an awareness of any potential compliance risks and a commitment to act with integrity, as the foundation for the Company’s success, reputation and sustainable growth.

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