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 Methodologies • Applicant 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 CFR25.571 • 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