Bachelor’s degree in Engineering with 7+ years’ experience performing stress analysis or Master’s degree with 6 years’ experience.

Strong background in structural analysis related to aircraft.

Strong understanding of load paths and various aspects of airframe design using metals and composites.

Provide technical solutions to a wide range of difficult problems. Solutions are imaginative, thorough, practicable, and consistent with organization objectives.

Develops and validates SW to solve problems. Is able to consider the impact of decisions on product metrics.

Expresses problems, issues, and opportunities to peers, supervision and leadership.

Material properties and behavior (Composite & Metallic) or structural testing experience is preferred.

Strong technical writing and PC skills with proficiency in MS Office (Word, Excel, PowerPoint).

Excellent communication and presentation skills with the ability to work closely as a team with other international locations.

Candidates must be able to communicate effectively in English, both verbally and in writing.

Formulates structural analysis of a complex nature using computer analysis.

Conducts stress, fracture and fatigue structural analysis of aerospace components.

Defines, directs and documents structural test efforts to assess the structural integrity of metallic and non-metallic aerospace products.

Provides limited direction to others in stress analysis and may act as technical lead on assigned projects.

Provides technical solutions to a wide range of difficult problems. Develops and validates standard work to solve problems.