-Worked on ATA 53– Aircraft fuselage components stress analysis using OEM specific tools and methodologies.-Involved in creation of Static stress analysis justification reports for Single Aisle / XLR Aircraft Structural Repair Manual.-Interacting with customers to progress with the modification of stress dossiers along with mitigation approaches to follow in the analysis.

-Executing modal, random vibrational analysis on critical components of four+ generation inservice multirole light combat aircrafts.-Creating 2D and 3D mesh for finite element analysis (FEA), for optimizing mesh quality and ensure accurate simulation results.-Assisted in final quality inspections of transmission components prior to installation in Advance Light Helicopters (ALH) for certifying them as airworthy.