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SAE AMS6891A : 2025

Carbon Fiber and Fiberglass Epoxy Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications

Standard Details

The intent of this specification is for the procurement of carbon fiber and fiberglass epoxy prepreg products with 350 °F (177 °C) cure for aerospace applications; therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program must refer to the production quality assurance section (4.3) of this base specification, AMS6891.

General Information

Status : Revised
Standard Type: Main
Document No: SAE AMS6891A : 2025
Document Year: 2025
Pages: 28

Life Cycle

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SAE AMS6891A : 2025
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