Perform fatigue and damage tolerance analysis of metallic and composite structures in accordance with regulatory and OEM standards e g FAA EASA Utilize tools like NASGRO DARWIN or other proprietary applications for crack growth and fracture mechanics analysis Conduct life prediction assessments under static and agile loading conditions including variable amplitude loading Support aircraft certification programs by providing substantiation reports and analysis documentation Work closely with design stress materials and manufacturing teams to define inspection intervals and structural integrity requirements Interpret test data and validate analytical models against physical test results Develop and review fatigue test plans and evaluate test outcomes Document assumptions methodologies and results in clear traceable technical reports Bachelor s or Master s degree in Mechanical Aerospace or Structural Engineering 7 to 15 years of experience in fatigue and damage tolerance analysis Hands-on experience with at least one of the following tools NASGRO DARWIN or equivalent Experience on Stress Concentration evaluation fro Joints and Notches Solid understanding of fracture mechanics crack growth behavior and fatigue life prediction methodologies Ability to use FE tools like HM and Patran for Extraction of Loads stress for FDT analysis Familiarity with aerospace materials especially metallic alloys used in aircraft structures Experience working in a regulated environment with exposure to FAA EASA certification processes Strong analytical problem-solving and documentation skills Excellent communication skills and ability to work collaboratively in a multidisciplinary team Department Transportation India Associate Skills Required Fracture Mechanics Analysis Fatigue and Damage Tolerance Analysis NASGRO Years Of Exp 7 to 15 Years Desirable Skills Fracture Mechanics Analysis Fatigue and Damage Tolerance Analysis NASGRO Designation Associate

📌 Aero Stress Fatigue And Damage Tolerance Lead (Hyderabad)
🏢 Cyient
📍 Hyderabad