Standard

SAE AMS3915A

Revised

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Abstract

Form This specification establishes the requirements for a nominal 250 °F cure epoxy preimpregnated 7781 glass fabric. The prepreg has a nominal fiber areal weight of 294 gsm, and nominal resin content of 38%.  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 to 180 °F. c. The composite may be used for the manufacture of primary and secondary aircraft structure.

Document information

  • Standard from SAE_AC
  • Published:
  • Version: 0
  • Document type: IS