Experience

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  Turkish Aerospace Malaysia

  • Malaysia

  • Senior Structural Engineer

    • Nov 2022 - Present
    • Malaysia

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  Mitsubishi Heavy Industries

  • Nagoya, Aichi, Japan

  • Senior Stress Engineer at MHI Aerospace Systems Co., Ltd., Nagoya, Japan

    • Nov 2019 - Oct 2022
    • Nagoya, Aichi, Japan

    November 2019 - July 2020Detailed MHI Aerospace Co., Ltd., Related ExperienceProject: Mitsubishi Space Jet, MSJ100 Forward Fuselage Conceptual DesignNature of Work:• Creation of Global Finite Element Analysis Modeling & Simulation (Static, Buckling & Modal Frequency) of MSJ100 Forward Fuselage (GFEM).• Creation of Detailed Finite Element Analysis Modeling & Simulation (Static, Buckling & Modal Frequency) of MSJ100 Main Instrument Panel & Escape Hatch (DFEM).• Performed multiple loops / iterations of Finite Element Analysis Modeling & Simulation and post process structural analysis until a desired / workable solution achieved.• Established report by compiling structural analysis results and proposed solutions for the way forward.• Liaised with Program Manager & Structural Approver on agreement of conceptual design or weight saving activities and technical requirements/issues as well as weekly drumbeat (progress).

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  Strand Aerospace Malaysia Sdn Bhd

  • Selangor, Malaysia

  • Senior Stress Engineer

    • Dec 2014 - Nov 2019
    • Selangor, Malaysia

    December 2014 - 2019Nature of Work Involved: Seconded to Donier Seawings GmbH, Germany as Stress Approver for Dornier Seastar CD2 which is expected for First Flight in 2019.As a Lead, I am responsible to estimate man hours (per engineer and overall duration) and head counts required in order to prepare Engineering Co-ordination Memorandum (ECM) to be delivered to customers before the start of a project. The team under my supervision is responsible for developing, integrating and documenting structural requirements to establish the system design which guides the product through the design phase and verifies the structural integrity by using analytical methods, finite element models/simulations and other analysis tools throughout the product life cycle. As a lead, I also have to ensure that the on-going project progress are on track (Task Manager) and also checks on documents certification prepared by the team (Internal Checker) to substantiate for customers and regulatory agencies so that requirements are satisfied. Detailed Dornier Seawings GmbH Related ExperiencesProject: Seastar CD2 Rudder Pedal Assy, Avionics Rack, Wing Fuselage Electrical Harness (Conceptual, Weight Saving and Certification)Activities:• Initiate ECM that contains Scope of Work (SoW), data inputs required in order to start the work and deliverables upon completion of work.• Identify suitable engineers, estimates man hours required and provide quotation for the work to be performed.• Liaise with Structural Approver on agreement of conceptual design or weight saving activities. • Perform checks on structural analysis and technical documents compiled by team members to ensure that regulatory compliances are met

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  Spirit AeroSystems

  • Selangor, Malaysia

  • Stress Engineer

    • Sep 2010 - Nov 2014
    • Selangor, Malaysia

    Nature of Work:• Perform detailed stress analysis and sizing of composite and metallic of various structures.• Establish report and technical documents of composite and metallic of various structures. • Modifying Global Finite Element Model (GFEM) for analysis and perform FEM Validation • Perform repairability assessment on structures for Structural Repair Manual (SRM) & Allowable Damage Limit (ADL).Detailed ExperiencesProject: A350 Fixed Leading Edge Root End Fillet Fairing (Checkstress and Weight Saving)Activities:• Seconded to Spirit Europe, Preston, UK for 6 months as part of a team to transfer the FLE REFF work package back to Spirit AeroSystem (M).• Responsible for coordinating stressing activities, developing common spreadsheet for structural analysis and focal point of establishing technical reports.• Perform detailed stress analysis and optimisation of fixed leading edge metallic ribs & subspar of a wing structure using hand calculations and AIRBUS software (ISAMI).• Established technical documents (Stress Dossier) and ACD4 of metallic structures for EASA authorities.• Liaised with AIRBUS UK to provide progress updates and successfully passed CDR gate reviews.Project: A350 Fixed Leading Edge Upper & Lower PanelsActivities:• Perform preliminary down selection of GFEM Wing Bending Air Pressure cases and generate load combination table for detailed analysis• Modifying GFEM, perform validation and establish GFEM report for high temperature scenario• Perform detailed stress analysis (similar to REFF) for fixed leading edge composite upper panels and metallic refuel lower panel of a wing structure.• Establish report and technical documents (similar to REFF) for First Flight Certification.• Perform repair-ability assessment on fixed leading edge composite upper panel for Structural Repair Manual and Allowable Damage Limit for metallic refuel lower panel.• Perform bird strike assessment on fixed leading edge composite upper panel