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Fatigue and Damage Tolerance

1 month ago

Bengaluru, India Tata Technologies Full time

Senior Airframe Engineer job involves investigating and producing Fatigue and damage tolerance justifications 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 methods processes & terminologies

In depth knowledge of F&DT based design philosophy

Good understanding of the Aircraft Fuselage structure (A 320/A321 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 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.

Job Requirement

Bachelor/Masters Degree or equivalent relevant experience in an Aerospace/Mechanical engineering environment.

Minimally 4 to 6 years

Experience in a similar capacity work.

Good knowledge strength of materials, fatigue and fracture mechanics

In-depth knowledge of loading scenarios, free body diagrams, and structural behaviour of aircraft primary and secondary structural components.

Able to comprehend engi neering design definitions and drawings.

Proficient in MS Office (Word and Excel) and Adobe (PDF).

Good problem-solving skills and Right First Time attitude.

Meticulous to details, responsible and a team player.

Experience of Technical Review of deliverables Excellent written and verbal communication skills Work.

Proactive and good team worker.

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