SAE AMS6891B

Detailinformationen

Bezeichnung: SAE AMS6891B

Ausgabedatum: 01.07.2026

Seiten: 0

Land: Amerikanische technische Norm

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Annotation

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 (see 4.3) of this base specification, AMS6891.

SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Material Specification