AMS3970/1A: Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements - Material Specification

Features

Issuing Committee: AMS CACRC Commercial Aircraft Composite Repair Committee

Scope

Content: 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.

Rationale

Content: AMS3970/1A has been reaffirmed to comply with the SAE five-year review policy.

Meta Tags

Topics: Materials properties
Composite materials
Heat resistant materials
Coatings, colorants, and finishes
Fabrics and textiles
Fibers
Adhesives and sealants
Test procedures

Details

DOI: https://doi.org/10.4271/AMS3970/1A

Pages: 45

Citation: SAE International Material Specification, Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements, SAE Standard AMS3970/1A, Reaffirmed December 2016, Revised April 2011, Issued December 1999, https://doi.org/10.4271/AMS3970/1A.

Additional Details

Publisher: SAE International

Published: Dec 6, 2016

Product Code: AMS3970/1A

Content Type: Material Specification

Status: Reaffirmed

Language: English

Historical