Job Title: Service Related Problems (SRP) Stress Engineer
Location: Richardson TX; Wichita KS (Onsite)
Duration: 12 Months
Implementation Partner: Kaleidoscope Innovation
End Client: To be disclosed
Job Description:
- Perform Static fatigue and damage tolerance analysis for Aircraft structures using classical hand calculation.
- Understanding of load paths extraction of loads from Finite Element Models.
- Determination 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 expectations.
Required Qualifications (Nonnegotiable requirements):
- At least bachelors degree in mechanical or aerospace engineering
- At least 5 years (< 18years) of experience in Aerospace Industry as a Stress Engineer
- Comprehensive knowledge Stress analysis of Aero structures
- Having Hands on experience in one or more Finite Element Post Processing Tools (e.g. PATRAN)
Preferred Qualifications:
- Experience in providing technical solutions from conceptual to detailed design stage
- Use of Finite Element Methods for load extraction and to solve complex engineering problems
- Experience in performing Fatigue and Damage Tolerance Analysis
- Working knowledge of Boeing standards and tools.
- Working knowledge of Code of Federal Regulations Title 14 Part 25
- Experienced in PATRAN NASTRAN FEMAP
- Experience in CATIA V5 Enovia
- Strong oral and written communication and interpersonal skills.