Active standard | Published: 01/12/2016

SAE AMS3970/2A

Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Carbon Prepreg, Film Adhesive and Non-Structural Glass Prepreg

Available languages: English

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Detail information

Designation: SAE AMS3970/2A

Publication date: 01/12/2016

Pages: 0

Country: American technical standard

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Anotation

AMS3970/2 gives specific information about the qualification program for carbon fiber reinforced epoxy structural repair prepreg systems, applicable for 120 °C (250 °F) vacuum curing. The prepreg system may include an epoxy 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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