Shall provide the technical lead in troubleshooting F-16 structural problems, developing improvements leading to the resolution of issues identified, integration, verification, qualification for airworthiness certification, and fielding of repairs and modifications as defined in, or derived from, program requirements. Recommend a minimum of five years of experience in the aircraft structural engineering field, including, but not limited to, sustainment, durability and damage tolerance analysis, fatigue and fracture mechanics and material properties, repair design and integration.