Karthik R

• To assess the non-conformities encountered during fuselage production from a design perspective and provide solutions while ensuring constraints with respect to manufacturability, assembly, and reparability, duly following customer methods and processes.
• Assessing the nonconformities of various complexities arising during shell line or panel line assembly in the fuselage and providing design resolution independently.
• Checking for correctness in the design solution for clearing the non-conformance with appropriate sketches, recommendations, and specifications, and finally validating the design solution.

Technical competency:

• Work experience in working with fuselage structures for concessions for the A319, A320, and A321 (XLR).
• Having knowledge of ATA Chapter 53.
• Having a good knowledge of fuselage structure assembly (frames, stringers, skin panels, cross beams, etc.). Door surrounding areas, Section 16/18 lap joint, Section 16/18 to Section 19 orbital joint. etc,.

Acted as signatory for Airbus concession:

• Executed non-conformity analysis and concession preparation.
• Facilitated cross-functional collaboration to enhance project outcomes.
• Ensured structural integrity of aircraft through timely solutions and strict airworthiness compliance.