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

Details
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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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