Stress and loads analysis of primary and secondary aircraft structure, equipment racks, and interior items using classical analysis methods and finite element techniques. Provide design support, detail stress analysis, and stress support to Liaison for modification of primary aircraft structure and interior items.
Major Functions:
Stress Analysis of Primary and Secondary Aircraft Structure
Stress Support for New Design
Stress Support to Liaison Engineering
Preparation of Stress Analysis Reports
Skills/Experience:
Required Skills:
Classical Stress Analysis
Finite Element Analysis Using MSC/NASTRAN and PATRAN
Analysis of Aircraft Structural Repairs
Preparation of Stress Reports for Aircraft Certification
Microsoft Word and Excel
Desired Skills:
Fatigue and Damage Tolerance Analysis
Knowledge of Commercial and Military Aircraft Certification Requirements
Education:
Minimum of B.S. in Aerospace, Civil, or Mechanical Engineering, or equivalent field of study.
Experience:
Minimum of 18 years of aircraft structural analysis. Experience in the area of modification of transport category and general aviation aircraft is beneficial.
Would prefer candidate to have at least 1 year of previous experience with client.