Supporting Military Commercial Derivative program by providing electrical design support for Electrical Power Systems, Hydraulics, systems, Mechanical systems, Fuel systems, and Avionics systems. Perform reviews of functional schematics and wire diagrams to ensure compliance to applicable design and safety requirements.Support requirements and definition and validation activities by providing technical and certification expert support during System Requirement Reviews (SRR), Preliminary Design Reviews (PDR), Critical Design Reviews (CDR), Test Readiness Reviews (TRR), and other applicable design development process milestones, include those related to product and system integration (Concept Layout & Assembly Layout).Lead FAA certification compliance strategy for VC-25B Electrical Power Systems Military Commercial Derivative Airplane modification by coordinating with systems technical leads and designers, certification specialist, Boeing leadership, Boeing Regulatory Administrators, and FAA Military Certification Office. Write FAA certification and conformity plans to support Code of Federal Regulation (CFR) Part 25 compliance and safety requirements. Support FAA Issue Paper proposals development, including cert basis development FAA issue paper.Lead certification discussions with U.S. Government customers (White House Program Office & Air Force) and supplier contracted by the government to resolve design requirements, and develop statement of work and design requirements that support FAA certification requirements.As an FAA Electrical System E-UM, review technical data such as certification test plans, conformity plans, analysis, safety assessments, and other applicable compliance showings. Provide FAA test witnessing of certification testing.Provide coaching and development mentoring for early career engineers via guidance, sharing lessons learned, and exposure to engineering opportunities internal and external to the Air Vehicle EE Subsystem team.

Provide electrical design support that included translation of design requirements into component and architectural designs. Reviewed fuel system functional schematics and wire diagrams to ensure the system design meets integration requirements and safety requirements. Support and performed voltage drop and fault current analysis and battery capacity analysis.Lead and supported 777X fuel systems architectural trades studies in that resulted in design improvements and resolving fuel system technical and certification issues.As Electrical Fuels System E-UM, supported development of 777X Fuels electrical system FAA certification compliance strategy, certification plans, and test plans via coordination with Propulsion Fuels FAA Engineering Unit Members (E-UM), various fuel system equipment managers and other system design teams and leads, and other organizational teams such as safety and regulatory compliance. Also supported system safety assessments (SSA) of fuels electrical system design and development of other analysis and safety documents. Coordinated with Supplier Management & Manufacturing Engineering organization to facilitate timely procurement of electrical fuels system components to support program development schedules. Also review supplier data submittals to ensure component design and system requirements.

Served as 737MAX equipment manager for Generator Control Unit (GCU) and Bus Power Control Unit (BPCU) components for the 737MAX Electrical Power System. Responsible for documentation of electrical systems requirements for GCU and BPCU certification. Developed wire harness design and fabrication to support certification testing. Monitored supplier performance to ensure compliance with requirements during Preliminary Design Review (PDR), Critical Design Review (CDR), and Test Readiness Review (TRR).Lead 737MAX certification activities for EE Subsystem which included coordinating EE Subsystem certification basis development with technical design leads and system experts and certification reviews with Boeing Project Administrators (PAs), and FAA & EASA regulatory administrators. Authored and approved certification plans, and provided cert plan development coaching to EE Subsystem team members and other engineering teams with certification projects. Established 737MAX EE Subsystem Certification Business Goals and Objectives for EE Subsystem team in 2014.

Managed EE Subsystem certification plans and projects as certification focal for 737NG Electrical Subsystems.Lead certification approach for newly redesign External Power receptacle by coordinating with equipment designers and stress experts to align design and certification efforts in order to drive certification issues to success. Communicated with various levels of senior and executive leadership regarding certification and design subjects.Assisted with development of design requirements for new LED Landing Light system which included coordination with external suppliers, various engineering design teams, including flight test pilots, Boeing supplier management organization. Also assisted in coordinating a demonstration test with supplier to assess the feasibility and performance of LED Landing Light system concept.Supported development of technical system requirement and design documentation such specification requirements, system description documents, and test and analysis reports.Co-lead certification strategy for 737NG Class 2 EFB (Electronic Flight Bag) and was responsible for equipment management duties that included requirements development verification and validation activities and authoring certification plan and analysis documents.

Assisted in resolving process issues related to certification activities and change management processes that affected airplane production, testing, and customer delivery by coordinating with various change management focal, design engineers, and certification coordinators and administrators.Developed and maintained metrics of key certification activities and communicated data with team lead.Supported reviews of production engineering design changes for compliance system integration and program certification processes, and to ensure scheduled certification activities and airplane production and delivery schedules are integrated and aligned appropriately.Coordinated airplane system Temporary Operating Limitations (TOLs) between Boeing Commercial Airplanes (BCA) and Boeing Defense Space & Security (BDS) engineering design teams and airplane test directors to support efficient test scheduling and issue resolution of P8 T1 airplane integration testing.