Pouya S.

Structural Engineer / Fatigue & Damage Tolerance at Pilatus Aircraft Ltd
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Contact Information
us****@****om
(386) 825-5501
Location
Switzerland, CH

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5.0

/5.0
/ Based on 2 ratings
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Gianfranco Iasiello

I met Pouya when I was working on the Gulfstream G650 project in the Netherlands. I found Pouya a nice colleague as well as a good team player always ready to support each member of the team. Very calm and professional person to deal with even under intense pressure on work.

Erik Velthuis

I know Pouya as a warm person who is always willing to help out as a colleague. Pouya likes to share his knowledge and has the common team goal always on his mind. I was sorry to hear he would leave Fokker Aerostructures, but can understand that he'd like to make a move in his career.

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Experience

    • Switzerland
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • Structural Engineer / Fatigue & Damage Tolerance
      • Sep 2018 - Present

      - Lead structural engineer for the development of PC-24 Structural Repair Manual (SRM). - Leading and coordinating internal and external projects such as testing and investigating new technologies. - PC-24 in-service structural and general support. - Lead structural engineer for the development of PC-24 Structural Repair Manual (SRM). - Leading and coordinating internal and external projects such as testing and investigating new technologies. - PC-24 in-service structural and general support.

    • Switzerland
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • F&DT Specialist
      • Sep 2013 - Apr 2017

      Fatigue and Damage Tolerance Specialist and consultant at Pilatus Aircraft Ltd for PC-24 Business Jet. Area of expertise; Nose & Cockpit, Fuselage, Wing, Flight Controls, Tail and Landing Gears. - Design and development analysis of the first three PC-24 prototypes for initial flight testing and certification. - Author of PC-24 Principal Structural Elements, full scale fatigue test article, detail FE modelling description, specific Finite Element post processing guidelines and prototype fatigue critical zone inspection. - Design and development analysis of PC-24 full scale fatigue test article. - Checking and reporting of initial design, first flight and certification reports of prototype and serial Aircrafts. - F&DT justification of design engineering and production concessions. - Involved in in-house tool developments.

    • United Kingdom
    • Industrial Machinery Manufacturing
    • 1 - 100 Employee
    • F&DT / Static Stress Engineer
      • Mar 2013 - Sep 2013

      Senior F&DT and Static engineer for of Metallic & Composite parts - Initial 12 weeks onsite at Spirit AeroSystem in Wichita, USA, as part of the elite engineering management team to offload the work package to HGEL in the UK. - Airbus A350-900; Fuselage section 15; Static, Fatigue and Damage Tolerance justification of both metallic and composite concessions using ISAMI, Finite Element Modelling and other tools. - Supervisor and mentor to the new engineering team to offload the work package.

    • Lead Fatigue & Damge Tolerance, Senior F&DT/ Stress Engineer
      • Apr 2012 - Mar 2013

      Lead Fatigue and Damage Tolerance Engineer and point of contact: - Single Aisle A320/A319 NEO Flap Tracks Team Lead, Planning, Budget and Reporting. - Lead and manage the supplier on A320/A319 NEO Sharklet Device Fatigue and Damage Tolerance work package. Senior F&DT/ Stress Engineer: - Working on A320/A319 NEO Fatigue and Damage Tolerance of wing metallic parts. Such as Root joint fittings, stringers, etc. Consulting and advising solution for the critical locations. Lead Fatigue and Damage Tolerance Engineer and point of contact: - Single Aisle A320/A319 NEO Flap Tracks Team Lead, Planning, Budget and Reporting. - Lead and manage the supplier on A320/A319 NEO Sharklet Device Fatigue and Damage Tolerance work package. Senior F&DT/ Stress Engineer: - Working on A320/A319 NEO Fatigue and Damage Tolerance of wing metallic parts. Such as Root joint fittings, stringers, etc. Consulting and advising solution for the critical locations.

    • Stress Engineer
      • Oct 2005 - Oct 2011

      Conceptual Stress Engineer of Dassault private jet Empennage. - Static, Fatigue and Damage Tolerance analysis and sizing of primary and secondary structures. Metallic and Composite Stress Engineer on the Empennage of Gulfstream private jet G650: - Static, Fatigue and Damage Tolerance analysis and sizing of the G650 Horizontal Stabilizer primary and secondary structural parts and reporting. - Certification of the G650 Empennage. Stress and Fatigue & Damage Tolerance Engineer Airbus 380 J-nose: - The design of the composite J-nose and metallic parts for the A380. - Liaison between Airbus UK and Stork Fokker, - Static, Fatigue and Damage Tolerance analysis and FEA of A380 composite J-nose and the metallic parts. All the FE work was undertaken using MSC NASTRAN/PATRAN, - Documentation and Certification.

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