{"schemaVersion":"jobsearcher.job.v1","id":"4db55eaac568c4aa2e7c48ad","url":"https://jobsearcher.com/jobs/4db55eaac568c4aa2e7c48ad","canonicalUrl":"https://jobsearcher.com/jobs/4db55eaac568c4aa2e7c48ad","title":"Stress Engineer","description":"Job Description\n\nJob title: Stress Engineer - AerospaceWork Location with Zip code: Richardson, TXMinimum years of experience required: 5-12 YearsMust have skills:At least bachelor's degree in mechanical or aerospace engineeringAt least 5 years (<12years) of experience in Aerospace Industry as a Stress EngineerComprehensive knowledge Stress analysis of Aero structures.Detailed Job Description:Perform Static, fatigue and damage tolerance analysis for Aircraft structures using classical hand calculation.Applicant should be familiar with Boeing Static and Book 1,2 and 3 Fatigue Analysis MethodologiesApplicant should be familiar with and have prior experience with the following Boeing Stress Tools, including IAS, XSA/SA+, FEADMS, IDTAS, Moss-Duberg, and FAMOSS Understanding of load paths, extraction of loads from Finite Element Models.Applicant should be familiar with Damage Tolerance Analysis and CFR25.571Determination of critical failure modes and performing analysis to ensure structural integrity.Analysis of aircraft primary/secondary metallic structures.Read and interpret engineering drawings.Coordinate with cross functional groups including Design, Materials & Process Engineering.Participate in review meetings with Customer and SMEs.Generate Engineering Stress Report which establishes compliance and safety.Interact with customer; understand the Scope of Work and methodology required to meet customer expectationsPreferred QualificationsKnowledge of Aerospace industry and standardsExperience in metallic and Composites structural analysisExperience in Load, stress calculations and preparing technical reportsExperience in Finite Element Analysis tools (Nastran, Patran)Experience in static, fatigue and damage tolerance calculationsStrong oral and written communication skillsKnowledge of Aerospace industry and standardsExperienced in PATRAN, NASTRAN, FEMAPExperience in MRB and SRMExperience in CATIA V5, EnoviaStrong oral and written communication and interpersonal skills.Minimum years of experience: 5-12 yearsEducation: Bachelor&#39;s or Master of Engineering","company":"Softcom Systems","rawCompany":"softcom systems","city":"Richardson","state":"TX","isRemote":false,"isActive":false,"createdAt":"2026-05-24T07:39:33.521Z","occupations":[{"code":"17-2011.00","title":"Aerospace Engineers","slug":"aerospace-engineers"},{"code":"17-2141.00","title":"Mechanical Engineers","slug":"mechanical-engineers"},{"code":"17-2199.00","title":"Engineers, All Other","slug":"engineers-all-other"}],"industries":[{"code":"541330","title":"Engineering Services","slug":"engineering-services"},{"code":"336413","title":"Other Aircraft Parts and Auxiliary Equipment Manufacturing","slug":"other-aircraft-parts-and-auxiliary-equipment-manufacturing"},{"code":"336411","title":"Aircraft Manufacturing","slug":"aircraft-manufacturing"}],"jobPosting":{"@context":"https://schema.org","@type":"JobPosting","title":"Stress Engineer","description":"Job Description\n\nJob title: Stress Engineer - AerospaceWork Location with Zip code: Richardson, TXMinimum years of experience required: 5-12 YearsMust have skills:At least bachelor's degree in mechanical or aerospace engineeringAt least 5 years (<12years) of experience in Aerospace Industry as a Stress EngineerComprehensive knowledge Stress analysis of Aero structures.Detailed Job Description:Perform Static, fatigue and damage tolerance analysis for Aircraft structures using classical hand calculation.Applicant should be familiar with Boeing Static and Book 1,2 and 3 Fatigue Analysis MethodologiesApplicant should be familiar with and have prior experience with the following Boeing Stress Tools, including IAS, XSA/SA+, FEADMS, IDTAS, Moss-Duberg, and FAMOSS Understanding of load paths, extraction of loads from Finite Element Models.Applicant should be familiar with Damage Tolerance Analysis and CFR25.571Determination of critical failure modes and performing analysis to ensure structural integrity.Analysis of aircraft primary/secondary metallic structures.Read and interpret engineering drawings.Coordinate with cross functional groups including Design, Materials & Process Engineering.Participate in review meetings with Customer and SMEs.Generate Engineering Stress Report which establishes compliance and safety.Interact with customer; 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