Stress Analyst
Listed on 2026-07-01
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Engineering
Aerospace / Aviation / Avionics, Mechanical Engineer, Engineering Design & Technologists
US Citizenship Required.
Structural analysis of aircraft modifications, including design support, and preparation of technical documentation necessary to ensure airworthiness. Determination of stress levels in primary and secondary aircraft structure, systems, and equipment resulting from applied and induced loads, as well as the comparison of these stresses with material properties to predict failure and structural instabilities given due consideration to applicable failure theories. Travel could be required to Waco for support of critical liaison activities although not expected.
Skills/Experience:
Bachelors Degree in Aerospace, Mechanical or other related engineering field with four (4-10+) years aircraft stress analysis experience or a Masters Degree in Aerospace, Mechanical or other related engineering field with two (2) years aircraft stress analysis experience
Familiarity with FAA (Part 23 or 25) or military aircraft airworthiness design approach, certification process, and requirements
Good computer skills including working knowledge of Microsoft Word and Excel
Able to generate free body diagrams and calculate internal loads and stresses
Although not expected, must be able to travel from Tulsa to Waco, TX if required.
Must be able to obtain a security clearance.
Must be proficient in Microsoft Office, and have general computer knowledge.
Good verbal and written communication skills
Desired
Finite element modeling with commercial software, Siemans FEMAP or PATRAN / NASTRAN
Automating calculations using VBA in Excel or another programming language
Reviewing engineering design data with CAD and PLM software, including NX and Teamcenter
Structural substantiation of aircraft structure with classical analysis
Results-oriented, empowering leader with direct experience exceling in a matrixed environment
Experience analyzing composite structure
Experience in Mat Lab a plus.
Experience with FAA and/or Military certification requirements.
Required Skills:- Familiarity with FAA (Part 23 or 25) or military aircraft airworthiness design approach, certification process, and requirements
- Good computer skills including working knowledge of Microsoft Word and Excel
- Able to generate free body diagrams and calculate internal loads and stresses
- Although not expected, must be able to travel from Tulsa to Waco, TX if required.
- Must be able to obtain a security clearance.
- Must be proficient in Microsoft Office, and have general computer knowledge.
- Good verbal and written communication skills
Skills:
- Finite element modeling with commercial software, Siemans FEMAP or PATRAN / NASTRAN
- Automating calculations using VBA in Excel or another programming language
- Reviewing engineering design data with CAD and PLM software, including NX and Teamcenter
- Structural substantiation of aircraft structure with classical analysis
- Results-oriented, empowering leader with direct experience exceling in a matrixed environment
- Experience analyzing composite structure
- Experience in Mat Lab a plus.
- Experience with FAA and/or Military certification requirements.
- Bachelors Degree in Aerospace, Mechanical or other related engineering field with four (4-10+) years aircraft stress analysis experience or a Masters Degree in Aerospace, Mechanical or other related engineering field with two (2) years aircraft stress analysis experience
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