Mechanical Stress Engineer

About this role

Requirements

• Bachelor’s Degree within Aerospace/Aeronautical/Mechanical Engineering
• Equivalent of a minimum of five (5) years relevant work experience
• Proficient in hand calculations using classic stress analysis techniques
• Proficient in Finite Element Analysis
• Proficient in Technical Report Writing
• Working knowledge of EASA regulatory and airworthiness requirements including (E)TSO, CS-25, JAR-25 and FAR 25 requirements
• Knowledge and experience of aircraft interior reconfiguration programmes and primary and secondary aircraft structures
• High level of attention to detail and professional integrity

Responsibilities

• Report to the Structures Engineering Manager and work with the global engineering team across multiple time-zones to identify requirements and solutions for active and upcoming projects
• Lead certification activities to ensure compliance with design requirements and serve as technical focal for certification and stress issues relating to large aircraft modification programmes
• Compile and critically review structural substantiation documents related to product certification and integration of new seating installations
• Substantiate monument and furniture installations such as galleys, lavatories, class dividers, first class suites and VVIP furnishing
• Address cabin interior changes including LOPAs, Passenger Service Unit layouts, LRU installations
• Manage primary structure changes including antenna installations and fuselage modification
• Promote a culture of innovation, safety, and quality throughout the engineering organization
• Act as Boeing representative during customer meetings such as ITCM, PDR, CDR and FAI and provide on-site support during embodiment phase

Benefits

• Annual incentive plans
• Continuous learning to develop the approach and skills to navigate whatever comes next