P1711AA - Advanced Composites Prepreg-Nominal 250°F Cure-Carbon Fiber and Epoxy Resin, Unidirectional Tape, Thermoplastic Toughened, Flow Control

Details Not available for purchase at this time. Document Number: P1711AA Project Initiation: 11-03-2011 Project Number: Revision Number: Sponsor Name: David Richard Westlund Title Advanced Composites Prepreg-Nominal 250°F Cure-Carbon Fiber and Epoxy Resin, Unidirectional Tape, Thermoplastic Toughened, Flow Control Scope This specification establishes the requirements for FiberCote E 765 epoxy prepregs for airframe components under 14 CFR 23 requirements. Rationale The purpose of this specification is to allow procurement of a defined material corresponding to the statistically derived material properties published in CMH-HDBK-17.

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