SAE AMS3970/2A PDF
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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
Description
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.
History
| AMS3970/2A | 2016-12-06 | Latest | Reaffirmed |
| AMS3970/2 | 1999-12-01 | Historical | Issued |
| ISSUING COMMITTEE | AMS CACRC Commercial Aircraft Composite Repair Committee |
|---|---|
| DATE | 2016-12-06 |
| DOI | |
| ISCURRENT | Current |
| PAGE | 16 |
| PUBLISHER | SAE International |
| REVISED | REAFFIRMED |
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