Description
You perform stress and finite element analyses for metallic aircraft structures and support certification activities in an aerospace development project.
Tasks
- Perform classical stress analyses and FEA for primary and secondary metallic aircraft structures
- Develop stress reports, structural substantiation documents, test plans, and test reports
- Support compliance demonstration activities according to CS-23 certification requirements
- Collaborate with design, certification, and multidisciplinary engineering teams
- Interface with suppliers, internal stakeholders, and airworthiness authorities
- Take ownership of structural topics within an aircraft development project
Profile
- Bachelor's or Master's degree in Aeronautical Engineering, Mechanical Engineering, or a related discipline
- Around 5+ years of experience in aerospace stress analysis, including metallic aircraft structures
- Proficiency with FEA tools such as NASTRAN, FEMAP, or comparable analysis software
- Knowledge of CS-23 certification requirements
- Experience with cabin or cockpit structures is advantageous
- Strong communication skills in English (C1), written and spoken
Offer
- 3–6 months interim, then a permanent position
- Flexible working hours
Company
Aerospace manufacturing
