Supervisor Engineering Stress

Cirrus Aircraft-posted 3 months ago
Full-time • Senior
Duluth, MN
1,001-5,000 employees
Transportation Equipment Manufacturing
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Experienced airframe structural analysis engineer for technical leadership and management of the core airframe stress analysis group. Working with other engineering functional managers, lead engineers, and certification engineers; the position is an integral part of the aircraft structures function of the Cirrus Product Development Team, including ownership of development and execution of FAA Type Certification Plans.

  • Recognized within engineering for structural technical competence.
  • Mentor and coach stress engineering team.
  • Responsible for team hiring, onboarding and technical training of stress group.
  • Anticipates project tasks, task durations, and resource needs. Work with Program Manager and Project Engineers to help define resource needs, required tasks, and schedule inputs by project.
  • Decides and leads project assignments and takes responsibility for structural substantiation used for aircraft certification.
  • Develops certification plans and project requirements documents. Collaborates with ODA unit members to ensure proper compliance with FAA regulations (primarily 14 CFR Part 23).
  • Develops and validates structural analysis methods.
  • Review aircraft structural layout and designs.
  • Review structural analysis of aircraft structures generated by stress team.
  • Review and approve analysis, design and test documentation. Includes analysis reports, design reports, test plans and test reports.
  • Foster personal and department continuous improvement activities.
  • Enforces company/area policies.
  • Minimum 4-year degree in Aerospace or Mechanical Engineering with at least 10 years of experience in aircraft structural analysis, testing and FAA certification.
  • Minimum 4 years in a technical lead position where there was oversight of other engineers or engineering Projects.
  • Ability to provide technical leadership, guidance and decision making.
  • Ability to demonstrate sound judgement and effective communication skills (written and verbal). Must be able to demonstrate ability to read, write and speak the English language.
  • Extensive knowledge of aircraft structure, materials and manufacturing processes including composites.
  • Knowledge of external loads development methods including aerodynamics and inertia.
  • Thorough understanding of structural load paths, developing internal loads and aircraft structural behavior.
  • Thorough understanding and previous use of classical hand analysis methods (including composite laminate plate theory).
  • Experience with Finite Element Analysis and model validation.
  • Experience with structural testing and data acquisition.
  • Knowledge of FAA Part 23 regulations and other guidance used for aircraft certification.
  • Methods for problem solving and analysis.
  • Introductory budget and fiscal knowledge.
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