CACRC07AA - Glass Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 0 - Introduction

Details Not available for purchase at this time. Document Number: CACRC07AA Project Initiation: 12-20-2007 Project Number: Revision Number: Sponsor Name: Ana Teresa Rodriguez Title Glass Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 0 - Introduction Scope This Technical Specification is prepared by the Air Transport Association/International Air Transport Association/Society of Automotive Engineers, Inc. (ATA/IATA/SAE) Commercial Aircraft Composite Repair Committee - Repair Material Task Group (CACRC-RMTG). The purpose of this specification is to obtain a common Technical Specification for 120 °C (250 °F) Vacuum Curing Repair Prepreg for glass fiber reinforced epoxy structures conforming to the requirements of the Original Equipment Manufacturers (OEM). Rationale The need for developing a standard is to obtain a common Technical Specification for 120 °C (250 °F) Vacuum Curing Repair Prepreg for glass fiber reinforced epoxy structures conforming to the requirements of the Original Equipment Manufacturers (OEM).

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