Asanga Jayasinghe

****, ********* ******, ******, **, L9E 0A2, Canada

Tel: 905-***-****; E-mail: add29z@r.postjobfree.com

Profile:

An experienced professional with 10+ years of experience engineering projects. Proven ability to design, develop and integrate technical solutions across the entire development cycle. Enjoys problem solving and thrives in challenging situations while delivering high quality results. Excellent knowledge on both engineering and project management fields along with ability to effectively coordinate cross-functional activities. Core Skills:

• Metallic/Composite Engineering Solutions • Project Management

• Structural Design & Development

• Technical Integration/Liaison

• Tolerance analysis/GD &T (ASME Y.14.5m)

• Certification and Testing

• Technical Leadership

• System Integration

• Manufacturing processes

• AutoCAD/Solidworks

Education:

• BEng (Hon’s) Aerospace Engineering Design, Kingston University – London 2007

• MSc Engineering Projects Management, Kingston University – London 2011

• Practical Stress Analysis (PSA) Certificate in Aircraft Stress Analysis by Jean-Claude Flabel 2019 Professional Experience:

Employer: Field Aviation Jun 2017 –Present

Project Role: Structural and Mechanical Engineer/Gulfstream G-IV Mar 2019 – Present

• Design and integrate complete supply of liquid coolant, Nitrogen, power and signal lines to mission systems located in wing pylons, nose and tail.

• Carried-out and lead the team to complete designs of major system installations, structural components

/reinforcements and structural attachments of liquid coolant and Nitrogen systems.

• Analysed and evaluated conformity of Nitrogen and liquid coolant system components to ensure that the system meets operational and certification requirements.

• Design entire system routing along with fuselage and wing LE feed-thrus which are required for supplies. Project Role: Structural and Mechanical Engineer/Bombardier Challenger 605 Jun 2017 – Mar 2019

• Designed and integrated structural installations of antennas and fairings to Bombardier Challenger 605.

• Successfully Led and carried out engineering installations of external antennas (skin penetrating) and fairing cover attachments from concept to detail designs including structural analysis and installation assessments.

• Successfully completed and coordinated engineering tasks of drawings, models and design review creations.

• Conducted and assessed findings of trial fitment exercises of machined and composite parts using 3D prints to ensure that installation does not interfere with fuselage skin and existing structures.

• Gained further structural substantiation knowledge of metallic components by carrying-out stress calculations.

• Demonstrated excellent manufacturing processes knowledge by resolving production installation related queries and actively supporting the production team.

• Technical deliverables: Complete design of antenna and radome installation, Waveguide installation, Manufacturing detail and installation drawings, PDR/ CDR, Technical assessments and installation instructions. Employer: Atkins – Aerospace department Jan 2013 -Mar 2017 Client: AIRBUS – A350XWB-900/1000 Fixed Trailing Edge - GE Project Role: Aerospace Design Engineer Sep 2014 – Mar 2017

• Incorporated a number of design modification projects on A350-900/1000 FTE components including top level installations, panel assys and detail parts.

• Worked on major installations; Pintle fitting, Landing gear support structure, TE Panel installations.

• Carried out design optimization, MRB and NCR (Non-conformance) assessments, and recommended technical solutions to resolve issues.

• Coordinated a team of 5-6 engineers from various countries to incorporate modifications on impacted aircrafts.

• Assessed and incorporated trailing edge brackets modifications to optimize overall weight of the systems.

• Gained extensive knowledge in aircraft top level breakdown structure, assembly and manufacturing philosophies, modification impacts and technical aspects of protective treatments.

• Led, assessed and implemented MSN 146+ top level tolerance updates and frontier drawings.

• Supervised 2 junior engineers; Created supporting documents to assist their tasks and verified their work. Client: Meggitt Advanced Composites and Polymers – Piaggio MPA – Avanti EVO Project Role: WP Lead Engineer/Aerospace Design Engineer May 2015 - Jun 2016

• Successfully delivered the baseline manufacturing designs and drawings of Horizontal Stabiliser work package.

• Demonstrated high quality performance in the technical lead role, with successful completion of the work package and client Critical Design Review (CDR) acceptance.

• Conducted complete tolerance analysis and fit analysis of components.

• Obtained Airbus Composite Product Design certification (CPD) and gained advanced knowledge on composites through exposure to hands-on composite manufacturing processes.

• led the team to finalise mould tool design, flatten plies, trial lay-ups, test procedures and Engineering reports.

• Technical deliverables: Composite ply definitions for manufacturing, test trials, tooling designs, designs and drawings including installations, complete tolerance analysis, CDR report, Test instructions Client: Meggitt Advanced Composites and Polymers – Raytheon Hawker Beechcraft Dorsal Fin Project Role: Mechanical Design Engineer Mar 2015 - May 2015

• Technical support to the mechanical design team to finalize Dorsal Fin assembly and components.

• Created assembly and installation drawings with build instruction reports to facilitate the build team. Client: AIRBUS - A320NEO Build Support

Project Role: Aerospace Engineer Feb 2014 - Sep 2014

• Analyzed and solved NCR (Non-conformance) and concessions; incorporated solutions to the existing design.

• Managed project resource planning, delivery tracking, quality and communication with stakeholders.

• Conducted lessons learnt root cause analysis to identify and recommend action plans for quality improvements. Client: AIRBUS- FACC - A350-900 Wing Tip and Wing Let MSN 21+ Project Role: Structural Design Engineer Jul 2013 - Feb 2014

• Led structural design tasks of Wing tip box Ribs sub-work package for the weight optimization mod.

• Analysed and reviewed the tolerance analysis and entire ICY capabilities of Wing Tip components.

• Assessed the gap and step tolerance stack-up requirements between wing skins to panel interface.

• Evaluated various WT box ribs redesign options and created project proposals to recommend the best solution in order to deliver the highest structural performance.

• Created models/drawings (metallic & composite) of ribs, covers, spars and butt-straps Client: AIRBUS - A320NEO- FLE and FTE

Project Role: Aerospace Design Engineer Jan 2013 - Jul 2013

• Completed the design of leading-edge Ribs and their system interfaces from B-scheme to manufacturing stage.

• Compiled the global Fastener BOM and assessed the fastener applicability with the interfacing components.

• Assisted design validation tasks against the legacy components.

• Liaised with the technical leads, manufacturing engineers and programme managers to ensure Ribs design tasks meet the deadlines and progress effectively.

• Design tasks: Conducted PBOM updates from detail parts to top level installations (GA/Inst), Spar bolting, Spar cap modifications and flutter ballast tolerance analysis. Employer: Sogeclair Aerospace Aug 2008 - Jan 2013

Client: Airbus - A380 Ribs Full Life Retrofit/Adaptation Repair Modification Project Role: Aero-Structures Engineer Jan 2012 - Jan 2013

• Liaised between the stress and integration teams to solve technical issues and improve overall performance.

• Incorporated structural modifications to rib geometries as per the stress team recommendations.

• Created modification impact reports and assessment reports for the structural changes.

• Improved the team efficiency and quality by initiating ‘how-to’ process and procedure guides. Client: Airbus - A350, A380 EQAM DDC Checks

Project Role: Aerospace Engineer (Technical Lead/Checker) Sep 2008 - Jan 2012

• Held signatory authority for A350 programme on Airbus drawings sign-off system.

• Led the UK team consisted of 10 engineers to perform technical checks and to deliver technical reports on time.

• Initiated successful biweekly technical presentation to improve overall quality of the engineering activities.

• Responsible for approval of the technical dossiers and reports which were compiled by the team.

• Played a pivotal role in the initial stage of the A350 DDC programme to set-up transnational teams. Engineering Tools:

• Catia V5(part/surface/CPD/kinematics), AutoCAD, Inventor, SolidWorks, Unigraphics NX

• SAP, Teamcenter, Enovia and PDM systems, MS Project, MS Office References Available upon request.

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