Airframe Stress Analysis F&DT

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.