Vinoth Sampath P.Eng. Pmp® Email & Phone Number

Toronto, Ontario, Canada

Mississauga

DE HAVILLAND DASH 8 (Q SERIES) - Part Design Approval (TC), Part Manufacturing Approval (FAA)• Dimensional, material analysis• 3D Scan of OEM Parts, 3D modelling & 2D Drawings• Deriving Applied loads based on Reverse Engineering• Performing Static Stress Analysis - Classical Approach• Preparation of Structural Substantiation Report

Bengaluru Area, India

AIRBUS A350-1000 COMPOSITE FRAME ANALYSIS - BCDS, PDS:• Extraction of geometry and fastener details from Catia DMU• Master Fishtails (Properties and Parameters), SE, SEA Mappings preparation • Run CFA module ISAMI 10.1 and post processing for RF• Sizing the Frame based on RF

Augsburg Area, Germany

AIRBUS A350-1000 SIDE SHELLS SIZING, PREMIUM AEROTEC, GMBH:• Sizing of Frames & Clips in the Side Shells for Section 16 18 in A350-1000 Based on Composite Frame Analysis Results• Preparation of Master Fishtails (Properties and Parameters), SE, SEA Mappings in ISAMI 10.1 CFA & Window Belt Module format.• Post processing, result interpretation and stress sizing based on the result.

Bengaluru Area, India

AIRBUS A350-900 &-1000 - SIZING - PREMIUM AEROTEC, GMBH:• Passenger Door Surround Structures • Rear Pressure Bulkhead• Performed Static and DT analysis for primary structures such as Frames, Skin, Lintel Beam, Aux. Lintel, Sill Beam, Shear Plates, Door Stop Fittings etc.• Worked on 460, 453, 399 MSNs

Augsburg Area, Germany

AIRBUS A350-900 BCDS - PREMIUM AEROTEC, GMBH:• Performed Static and Damage Tolerance analysis and ADC for primary structures such as Frames, Skin, Lintel Beam, Aux. Lintel, Sill Beam, Shear Plates, Door Stop Fittings etc for Step 7 (MSN 460) and Step 6 (MSN 316).

Bengaluru Area, India

BOMBARDIER CS100, CS300 WING CERTIFICATION: • Composite and Metallic Analysis of Rear Spar Splice and Certification report preparation• Large Damage Capability Analysis of Rear Spar Splice for CS100 & CS300• Auxiliary Spar Assembly Certification analysis, Allowable Damage Limit and ReportCFSA AIRBUS A350-1000:Static stress analysis, Analysis Certification Document (ACD4) and stress dossier for Centre Fuselage Structural Assembly for composite & metallic parts in belly fairing, lateral junction panel, lower junction panel.STATIC & DT SUBSTANTIATION OF VSTAB GREO FOR BOMBARDIER’S GLOBAL 5K, 6K:Preparation of analysis spread sheets and stress report for static & Damage Tolerance Analysis substantiation of Generic Repair Engineering Orders for Vertical Stabilizer skin.DAMAGE TOLERANCE ANALYSIS FOR BOMBARDIER GLOBAL 7000 EIS:• Performed Damage Tolerance Analysis and Certification report preparation quoting the threshold and repeat intervals for various PSEs of Enty Into Service configuration.• Longitudinal Skin Joint in Transition Section• Rear Engine Fitting Frame• Center Fuselage To Rear Fuselage Circumferential SpliceAIRBUS A350-900- SIZING - PREMIUM AEROTEC, GMBH:• Bulk Cargo Door Surround Structures - MSN 460 (STEP 7)• To perform Static and Damage Tolerance analysis for primary structures such as Frames, Skin, Lintel Beam, Aux. Lintel, Sill Beam, Shear Plates, Door Stop Fittings etc.• ADC Preparation

Bengaluru Area, India

• GLOBAL 7000 Aft Fuselage System Brackets• CS100 Wing Lower Skin Access Panel• CS100 DADT Repair and RNC

Belfast, United Kingdom

• Prepared Finite Element books for various DFEMs of CS100 such as Pylon Box, Auxiliary Spar assembly, Ribs, Rear Spar Splice and Wing Trailing edge GFEM• Analysis of PEEK brackets and certification report preparation

Bengaluru, Karnataka, India

Static Strength Substantiation of Repair Engineering Orders for Bombardier Aerospace Global 5k, 6k Aircraft. Worked on wide array of components such as Fuselage skin stringer (Cockpit, fwd, mid & aft), Frame, Bulkhead, V/Stab skin etc for various failure modes.

Master'S Degree, Aeronautical/Aerospace Engineering Technology/Technician

Bachelor'S Degree, Aerospace, Aeronautical And Astronautical Engineering, B

French As A Second Language, French Language And Literature