Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 0 - Introduction
- Aerospace Material Specification
- AMS3970A
- Reaffirmed
Scope
Rationale
Recommended Content
Aerospace Material Specification | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Carbon Prepreg, Film Adhesive and Non-Structural Glass Prepreg |
Aerospace Material Specification | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
Aerospace Material Specification | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 4 - Purchasing Specification for Film Adhesive |
Topic
Data Sets - Support Documents
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Issuing Committee
AMS CACRC Commercial Aircraft Composite Repair Committee
Scope:The Charter of the SAE Commercial Aircraft Composite Repair Committee (CACRC) is to promote repair and modification standardization and to provide guidance to composite and bonded structure maintenance providers, airlines, regulators, material suppliers and OEMs. The seven CACRC task groups are: Design, Inspection, Mods, Procedures, Repair Materials, Repair Techniques, and Training. No copyrighted material may be posted in this forum. SAE is not liable for opinions expressed or information posted to this forum. All information posted becomes the property of SAE.