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.