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Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing, Part 1 - General Requirements
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STANDARD published on 1.9.2026
Designation standards: SAE AMS3970/1B
Publication date standards: 1.9.2026
SKU: NS-1283679
Country: American technical standard
Category: Technical standards 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
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Latest update: 2026-09-17 (Number of items: 2 301 467)
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