SAE AMS 3970/6 : 2011

CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 6 - MATERIAL SPECIFICATION: CARBON FIBER FABRIC REINFORCED EPOXY PREPREG FOR REPAIR, PLAIN WEAVE FABRIC, 193 G/M[2], ADHESIVE FILM FOR REPAIR AND NON-STRUCTURAL GLASS FIBER FABRIC REINFORCED EPOXY PREPREG, 105 G/M[2]

SAE International

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1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. REQUIREMENTS
5. NOTES

Abstract

Describes the requirements of carbon fiber reinforced epoxy prepreg for repair, 120 degrees C (250 degrees F) Vacuum curing, Plain Weave Fabric, 193 g/m[2] and a companion non-structural glass fiber fabric reinforced epoxy prepreg, 105 g/m[2], qualified according to AMS3970/1 and AMS3970/2 for aerospace application.