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SAE AMS3914

Revision A, September 1, 2015

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(R) Advanced Composites Prepreg - Nominal 250 °F Cure - 12K Tow Carbon Fiber and Epoxy Resin, Plain Weave Fabric



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Product Details:

  • Revision: Revision A, September 1, 2015
  • Published Date: September 2015
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 29
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

Form

This specification establishes the requirements for a nominal 250 °F cure epoxy preimpregnated carbon fiber plain weave fabric product. The prepreg is a plain weave fabric with 12K tows, a nominal fiber areal weight of 193 gsm, and nominal resin content of 42%.

Purpose

a. The purpose of this specification is to allow procurement of a defined material corresponding to the statistically derived material properties published in CMH-17 Volume II.

b. This material is intended for use in laminate applications with a service temperature of –65 °F to 180 °F.

c. The composite may be used for the manufacture of primary and secondary aircraft structure.
AIA/NAS Aerospace Standards