Stress Engineer - F&DT

• 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 dynamic 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.
• 3 to 7 years of experience in fatigue and damage tolerance analysis.
• Hands-on experience with at least one of the following tools: NASGRO, DARWIN, or equivalent.
• Solid understanding of fracture mechanics, crack growth behaviour, and fatigue life prediction methodologies.
• 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.
• Attention to detail and accuracy in calculations and reporting.
• Proactive attitude towards continuous improvement and learning.

• Experience in aircraft structural analysis.
• Knowledge of residual strength, multiple-site damage (MSD), or widespread fatigue damage (WFD) assessments.
• Familiarity with probabilistic analysis techniques.
• Experience with scripting or automation (e.g., Python, VBA).

Cyient