SAE AMS3914B
Current
Advanced Composites Prepreg - Nominal 250 °F (121 °C) Cure - 12K Tow Carbon Fiber and Epoxy Resin, Plain Weave Fabric
Hardcopy , PDF
English
05-14-2026
| DocumentType |
Standard
|
| Pages |
31
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
The intent of this specification is for the procurement of plain weave fabric epoxy prepreg product with 250 °F (121 °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).
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