Senior Stress Engineer

Job Description

The Senior Stress Engineer is responsible for analyzing primary & secondary aircraft structures to show compliance with FAA 14CFR Part 23 & Part 25 regulations.

• Provides stress analysis of metallic & composite structures using classical hand calculations and finite element modeling (FEM) with advanced meshing techniques
• Performs loads develop in support of static, dynamic and fatigue & damage tolerance assessments
• Develops Fatigue & Damage Tolerance (F&DT) reports
• Other functions may include basic thermal analysis, basic aero-elastic flutter, dynamic response, non- linear analysis, pre- and post-test analysis, structural optimization, and software programming
• Completes stress notes & develops macros using Excel and Mathcad or similar software
• Documents analyses in formal structural substantiation reports and other airworthiness documents
• Contributes to FAA STC Project Specific Certification Plans (PSCP)

Qualifications and Competencies:

• Ability to obtain and maintain a Secret Security Clearance (US Citizenship required)
• Familiarity with resources such as MMPDS, Bruhn, Roark, etc., aircraft fasteners, materials, sheet metal assemblies, machined fittings, composites (fiberglass/carbon fiber), and honeycomb and solid laminate construction
• Knowledge of and familiarity with 14 CFR Part 23 and Part 25 structures regulations
• Strong foundation in technical skills, such as stress analysis, FEM, and solid modeling.
• Solid understanding of engineering modeling techniques and principles
• Experience reviewing and interpreting engineering models, drawings and manuals
• Strong organizational, analytical and problem solving skills
• Ability to evaluate, document, and report information regarding designs based on structural trade studies
• Experience with sheet metal modeling techniques for aircraft structures
• Strong communication skills, both written and verbal.
• Proficient in MS Office for report writing and analysis preparation
• Ability to work collaboratively with the engineering team and cross functionally
• Proficient in writing technical reports and presenting data in a clear and concise manner

Experience:

• 8-10 years of classical aircraft hand stress analysis methods and NASTRAN (FEMAP) finite element modeling
• 7-10 years Experience with primary & secondary structural modifications on aircraft.

Education / Certifications:

• Degree in Aerospace or Mechanical Engineering or equivalent experience required