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The Senior Stress Engineer at AEVEX Aerospace is responsible for analyzing primary & secondary aircraft structures to show compliance with FAA 14CFR Part 23 & Part 25 regulations. These analyses include loads development, classical hand calculations, Finite Element (FEM) modeling, fatigue & damage tolerance assessment and testing of aircraft modifications involving both metallic & composite structure and are thoroughly documented in formal structural substantiation reports.
Job Responsibility:
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
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)
Interfaces with Design Engineers to determine structural load paths and design optimization
Reviews & approves engineering drawings & reports
Attends design reviews as necessary
Regular and reliable attendance on a full time basis [or in accordance with posted schedule]
Responsible for exhibiting professional behavior with both internal and external business associates that reflects positively on the company and is consistent with the company's policies and practices
Embodies AEVEX’s cultural values and aligns daily actions with department goals and company culture
Requirements:
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
Driven self starter with a strong sense of accountability
Degree in Aerospace or Mechanical Engineering or equivalent experience required
8-10 years of classical aircraft hand stress analysis methods and NASTRAN (FEMAP) finite element modeling
Experience with primary & secondary structural modifications on aircraft
What we offer:
401(k)-retirement plan
comprehensive Medical, Dental, Vision, Disability and Life insurance group coverage with a portion of the premiums paid by the company
professional development funds
Employee Assistance Plan (EAP) with counseling, legal help, child and elder care support