Minimum of 10+ years' direct experience in Gas Turbine engine design
Experience with rotors, blisks, and blades.
Functional knowledge and awareness of this area: Turbo-Machinery Design, Manufacturing, System Design, Product Safety and Product Lifecycle
Experience with Rolls-Royce and Military standards and specifications
Familiarity in Lifecycle viewer, NX and Teamcenter
Experience and demonstrated capability in root cause investigation, including evidence-based methods
Experience in safety investigations (Red Tops) involving Rolls-Royce products.
Experience and knowledge of LiftSystem product line
Breadth of Turbomachinery (compressor and blisks) engineering experience across engineering functions: design, performance, validation/verification, customer application, certification/qualification, maintenance & overhaul, repair, field service, etc.
Knowledge of components/ systems functionality and numerical methods
Ability to analyze fleet data and determine risk factors and plans.