AMS3970/4: Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 4 - Purchasing Specification for Film Adhesive - Material Specification

Features

Issuing Committee: AMS CACRC Commercial Aircraft Composite Repair Committee

Scope

Content: AMS 3970/4 specifies the batch release and delivery requirements for film adhesive used for repair. This specification is applicable when the film adhesive is part of the prepreg system as defined in AMS 3970 and AMS 3970/1.

Meta Tags

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

Details

DOI: https://doi.org/10.4271/AMS3970/4

Pages: 9

Citation: SAE International Material Specification, Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 4 - Purchasing Specification for Film Adhesive, SAE Standard AMS3970/4, Issued December 1999, https://doi.org/10.4271/AMS3970/4.

Additional Details

Publisher: SAE International

Published: Dec 1, 1999

Product Code: AMS3970/4

Content Type: Material Specification

Status: Issued

Language: English

Historical