AMS3970/3: Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 3 - Purchasing Specification for Epoxy Prepreg - Material Specification

Features

Issuing Committee: AMS CACRC Commercial Aircraft Composite Repair Committee

Scope

Content: AMS 3970/3 specifies the batch release and delivery requirements for carbon fiber fabric epoxy prepreg used for repair.

Meta Tags

Topics: Maintenance, repair and overhaul (MRO)
Suppliers
Carbon fibers
Composite materials
Materials properties
Manufacturing processes
Containers
Carbon dioxide
Roll
Storage
Test procedures
Fibers
Materials handling
Production

Details

DOI: https://doi.org/10.4271/AMS3970/3

Pages: 11

Citation: SAE International Material Specification, Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 3 - Purchasing Specification for Epoxy Prepreg, SAE Standard AMS3970/3, Issued December 1999, https://doi.org/10.4271/AMS3970/3.

Additional Details

Publisher: SAE International

Published: Dec 1, 1999

Product Code: AMS3970/3

Content Type: Material Specification

Status: Issued

Language: English

Historical