JR2026514236 Mid-Level Structural Analysis Engineer - Wing & Empennage

• Perform stress analysis on Boeing 787 Wing and/or Empennage primary structures using classical hand analysis methods Finite Element tools/methods and/or Dynamic Simulation tools/methods.
• Reviews supplier documents in support of supplier technical oversight including engineering drawings analysis test plans procedures and reports.
• Develops integrates and documents structural requirements to establish the Wing and/or Empennage primary structure designs.
• Coordinates with other engineering groups to establish the product's environment such as load cases interface architecture and interface loads.
• Guides product design and verifies structural integrity throughout the product lifecycle to develop the structural environment characteristics and performance.
• Develops test plans and configurations supports test execution and analyzes/reports test results to validate and verify the primary structures meet requirements and specifications.
• Defines and documents certification and test results to substantiate for customers and regulatory agencies that requirements are satisfied.
• Supports in-service products by investigating failures and analyzing improvements.
• Develops certification related documentation to support CFR Part 25 Type Cert projects.
• Collaborates and performs oversight on projects with international partners/suppliers.
• Actively supports the growth and development of a new engineering organization.
• Works under general direction.

• Bachelor of Science degree in Engineering (with a focus on Mechanical Civil Aerospace Aeronautical or Material Sciences)
• 5+ years of related work experience or an equivalent combination of education and experience
• 3+ years of experience performing stress analysis on wing empennage or related structures
• 1+ years of experience performing stress analysis on composite structures
• Prior experience with manufacturing/production systems

• 5+ years of experience working on wing or empennage structures such as Wing tips wing leading or trailing edges wing center section wing box wing join vertical or horizontal stabilizers
• Experience developing certification related documentation
• Hands on experience with fabrication of metallic and composite structures
• Experience working as the prime technical contact with international suppliers/partners responsible for aircraft primary or other related heavy structures
• Part 21 and Part 25 Code of Federal Regulations knowledge and experience interacting with Federal Regulators

What We Do

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