a. This specification establishes the requirements for a nominal 250 °F cure epoxy preimpregnated carbon fiber unidirectional tape product.

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.

Purpose

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