
Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing, Part 1 - General Requirements
NORM herausgegeben am 1.9.2026
Bezeichnung normen: SAE AMS3970/1B
Ausgabedatum normen: 1.9.2026
Land: Amerikanische technische Norm
Kategorie: Technische Normen SAE
AMS3970/1 gives information about the technical requirements and qualification procedure for carbon fiber fabric epoxy prepreg and a companion non-structural glass prepreg used for repair of carbon fiber reinforced epoxy structures. The prepreg system may include a film adhesive to be applied in a co-curing process with the prepreg for joint and sandwich bonding. The need for a film adhesive shall be established during screening tests.
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Material Specification