The certification requirements associated with additively manufactured (AM) parts and AM repairs, such as cold spray and wire arc additively manufactured (WAAM), are required to be consistent with MIL-STD-1530D and US the Joint Services Structural Guidelines (JSSG)-2006. The U.S. Air Force (USAF) requirements for AM parts and AM repairs are delineated in USAF Structures Bulletin (SB) EZ-19-01, which states that “the most difficult challenge is to establish an accurate prediction of structural performance related to durability and damage tolerance (DADT)”. Structural Bulletin EZ-19-01 also states that “The focus on DADT requirements is emphasized in this SB because it contains the greatest challenges”. Consequently, the primary aim of this research is to develop a fundamental understanding of this problem space, specifically focusing on the durability of AM parts and AM repairs.