Select to either research a sandwich or solid laminate aircraft composite component, and identify the flaws/defects that can be accurately picked up with the choice of DT and/or NDT method(s) during design, fabrication, or in-service phase of the product (select one). Describe how the flaws and defects picked up by the inspection technique(s) contribute to the Damage Tolerance Evaluation section in AC 20-107B for structural integrity