Structural Repair Stress Engineer

Job description

• Good Knowledge on Aerospace domain, structure, loads, ATA chapters & Aircraft drawing.
• Good Understanding of Material properties, Drawings & GD&T.
• Strong foundation in Airframe structural analysis & load path (static failure modes & fatigue analysis) and good knowledge on non-conformances and repair techniques.
• Experience in stress analysis (Static / Fatigue & DT ) for aircraft metallic or composite structures (ATR In-service is added advantage).
• Good understanding of design solutions and its acceptance for specific damages on aircraft primary and secondary structures.
• Able to co-ordinate with design assessment team for the different solution or solution verification.
• Assess damage scenarios using appropriate inputs and aircraft configuration drawings.
• Propose and evaluate structural repair solutions considering time, cost, and safety.
• Create and manage repair documentation including Database (DB), Repair Instruction/Answer (AW), Repair Drawing (RD), and Technical Disposition (TD).
• Passion for resolving real-world, in-service aircraft structural issues.
• Experience & knowledge on Nastran /Patran is added advantage.
• Experience in-service daily and major repairs.
• Proficient in performing hand calculations for static and fatigue analysis and creating stress justification reports.
• Work with Structural Repair Manuals (SRM) and Adaption of SRM principles, Excellent communication and influencing skills 4..Ability to work independently and collaboratively.