EXPERIENCE SUMMARY23 plus Years of experience in engineering consultancy organization in Aerospace domain with Design & Validation using Hand calculation methodology & FEM for Aerospace Primary & Secondary Structural components, cum F&DT Fatigue and Damage Tolerance for Life & Life extension Requirement.PROGRAMS & CLIENT ENGAGEMENTS: Experience in major Aircraft programs like Airbus A380, A350, A320, A321, Boeing 787, COMAC C-90 & Hawker COMPETENCY SKILL SET:Hand calculations for Static, F&DTMetallic Structures FEM analysis methods for Static strength & loads estimationMetallic & Composites StructurePROJECT EXPEREINCE:Static Strength & Stability Aero-Engines Design Validation of LP & HP bleed-air port for strength requirementShear Neck design of PTO Power Take off Coupling Shaft of engine gearbox for Strength Requirements & Critical Speed Analysis of PTO Coupling Shaft Aero- StructuresStructural substantiation of AFT fuselage Tail cone cutout for C90GTI Hawker BeechcraftA380 Hybrid ribs – Redesign for Static Strength and stability requirementA321 Sharklet wing Top & bottom cover analysis & check stress report creationConcessions experience for providing design solutions for any corrective action requirement or the acceptance of deviation for the Design & Stress change assessment to the Manufacturing Deviations/Production ConcessionsDesign Validation using FEM methodology for Cockpit ceiling panel structuresFatigue & Damage ToleranceFatigue & Damage Tolerance analysis of Bottom-skin under MLGWFD Structural assessment MSD (Multi-site Damage) and MED (Multi-Element Damage) is carried out for all Non-ESG candidates A330-200/300 Series, A330-200F and A340-200/300/500/600 series aircraft in order to comply with the requirements of FAR 26.21 to determine the highest possible LOV (Limit of Validity) finally to create IRD (Inspection Requirement Dossiers) for the revised maintenanceExposed to Structural Repair manual & Damage tolerance reports