The Structures Company, LLC
Senior Stress Engineer
The Structures Company, LLC, Solana Beach, California, United States, 92075
Aerospace Technical Recruiter: Specializing in Aerospace Engineering: Structures, Design, Systems, and Testing
Job Description
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 load 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
Seniority level Mid-Senior level
Employment type Contract
Job function Engineering, Manufacturing, and Other
Industries Airlines and Aviation, Aviation and Aerospace Component Manufacturing, and Defense and Space Manufacturing
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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 load 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
Seniority level Mid-Senior level
Employment type Contract
Job function Engineering, Manufacturing, and Other
Industries Airlines and Aviation, Aviation and Aerospace Component Manufacturing, and Defense and Space Manufacturing
#J-18808-Ljbffr