In this role, you will own the development, documentation, and improvement of the loads development process. You will collaborate with various teams that interface with loads, including aerodynamics, airframe, engine, mass properties, mechanical systems, and propeller. Your responsibilities will include providing static and fatigue loads that are directly consumable by all downstream users, ensuring clear documentation of loads assumptions and methods to generate traceable and repeatable analyses. Additionally, you will support wind tunnel and flight test planning and execution in areas such as propeller loads, aeroelasticity, and aeromechanics, which includes test plan development, instrumentation and data acquisition definition, test monitoring and execution, data analysis and interpretation, and test report writing. You will also participate in loads means and methods of compliance discussions with the FAA, support the preparation of certification test plans, and assist with ground vibration testing.