Worked as Fatigue and Damage Tolerance Analysis Lead Engineer for the preparation of Repair Assessment guidelines for Boeing 737- Next Generation Models.

Type Certification activities for Control surface and High lift device components of Mitsubishi Regional Jet (MRJ 90), Includes the following:- Preparation and maintenance of FEM Idealization, Internal loads and structural analysis reports of control-surfaces (Aileron, Spoiler, Elevator and Rudder) and high lift devices (Flap, Slat).- Structural Assessment of issues occurred during the production of aircraft by sufficient static, Fatigue and Damage Tolerance justification in order to ensure the structural safety.- Partner analysis report/Safety Plan/other reports check, evaluation, partner coordination.- Co-ordination between Mitsubishi and Overseas supplier and Regulatory Authorities like EASA, FAA, JCAB.

Worked as Structural Analysis Engineer on following activities:- Structural Analysis for A350-1000 metallic/composite structures for Drawing release (DFM activity)- Static, Fatigue and Damage Tolerance Analysis of several concessions occurring on multi-sites. Multi-site involves contracts like A380, A330, B767, A350, A400M and CRJ Tail Cone etc.- Repair Assessment guidelines preparation for Boeing 737- Next Generation Models worked as Fatigue and Damage Tolerance Analysis Lead Engineer.

Post production engineering - Fatigue and Damage Tolerance analysis support for repairs on Boeing 737 CL & NG, 747, 757 aircraft structures.

Worked as Fatigue and Damage Tolerance Analysis Engineer for the post production engineering on Boeing commercial Aircraft structures.