Airframe Stress Analysis F&DT

Job description

Airframe Stress Analysis job involves investigating and producing Fatigue and damage tolerance justifications and/or Static solutions for design deviations and existing repairs for simple and complex Primary Structures of metallic Fuselage Structure. Following are the core responsibilities • Conversant with AIRBUS F&DT and/or Static methods processes & terminologies • In depth knowledge of F&DT based design philosophy • Good understanding of the Aircraft Fuselage structure (A320/A321/A330) will be added advantage). • Understand repair history of the damaged part. • Develop stress reports for the substantiation carried out for primary and secondary structures of aircraft with utmost accuracy. • Preparation of F&DT and/or Static stress justification • Identification of repair and solution. • Review of related technical documents for any discrepancies • Liaise with the customer for input requirement. Timely delivery of work based on a set completion target with high quality.