Active standard | Published: 01/12/2016

SAE AMS3970/1A

Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements

Available languages: English

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Detail information

Designation: SAE AMS3970/1A

Publication date: 01/12/2016

Pages: 0

Country: American technical standard

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Anotation

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.

SUBJECT TAXONOMY: Maintenance and Aftermarket, Maintenance, repair, and service operations, Materials, Composite materials
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Material Specification

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