- Integrated Project Team Lead in charge of team leadership and subsystem project schedule, budget (~$10M), rig and engine test plans, and risk management for New Product Introduction program including full program resource planning.- Led and managed the technical output of 28 engineers, functional output of 33 engineers, direct management of 16 employees not including manager on my team (9 additional). Led diverse team providing coaching and career development of Design, Stress, Aero, Project, Modeling, Impact, and Thermals engineers. - Presenting to the potential customers and internal PILM gate reviews on status of program and subsystem. Worked heavily in risk assessments including root cause investigations. - Guided team through significant team hiring and team scaling (from 8 persons to 28 persons), interviews, and onboarding as well as redeployment of team in one year.

- Led team of 39 reports in 2019 through significant organization transformation- Support Head of Component Engineering in coordinating people moves and large-scale data mining and organization.- Manage Fans and Compressors Subject Matter Experts and work and coordinate with global Civil and Defense leadership on collaborative projects, personnel, and commodity strategies.- Lead the XWiki ACRE project including Program Management, managing a £2.5M budget, and delivery targeting $5.9 million in savings per year.- Evaluate existing methods, processes, and toolsets in order to define, manage, and direct projects to increase capability, efficiency, productivity through LEAN principles for all engineers. - Maintain deployed engineer roster, career data and progression, and competencies to identify capability shortfalls/risks and support career progression within skill.

Technical Leads are responsible for all technical output of the design team to achieve the program goals. Design and technical lead over Axi-CF compressor executing full scale compressor rig test from inception through completion including compressor rig concept, design, analysis, manufacturing, delivery, and testing in 23 months and $22 million.• Technically managed 15+ member outsourced design team with Indy design and interdisciplinary review team oversight• Program has passed all major technical gate reviews in first attempt, closed all actions to pass global milestones, successfully passed to test ahead of global milestone, and exceeded all performance goals.

• Prepared and presented over 68 review board presentations including PCB, DDRAM, TR, PDR, CDR, and DVR boards • Trent 1000Cx Compressor Designer – Modernized the Compressor Blade Balancing routines for strength increases using Isight optimization and Robust Design tools providing 2x increases in strength. Compressor Pitching (axial gapping), Tip Clearance, and Blades Lead Designer. Familiar with RRUK processes for designers including RRDS, DDIS, DDRAM, TRs, Comm Sheets, and MMM criteria• F136 Surge Margin Recovery Effort – OGV designer for Concept Demonstration design and procurement and Service Release Concepts using the Robust Design tool kit• AE Engine Production Support - Manage and enact projects to aid in cost savings, efficiency, and fleet issues in the Defense and Corporate and Regional AE line of engines. Solve problems in manufacturing, assembly, test, and service of compressor components including Red Tops • Experience in rotatives, airfoils, and casings including limit stacks • Analyzed and cleared current production MRB (including TARs) and in-service TVs • Proficient in Goodman and Campbell Diagrams for airfoils• AE3007A2/C2 – De facto Compressor Lead including initial project management and technical support through gated reviews including blade containment analysis, case pressure vessel requirements, mission-based lifing, and writing of compressor SSDD• BR725 – Fans designer; familiar with RRUK and RRD processes for designers including RRDS (JDS), DDIS, MRB, Dahlewitz DDRAM, Testing, Comm Sheets, and MMM criteria• Compressor Blade Tip Laser Measurement System – Envisioned, Developed, and Implemented new technology into assembly to measure compressor blade tips with a laser system at 4 global production and overhaul facilities providing extensive VBA coding and software design reducing more than 8 hours in overhaul procedure time