AMS3970/4A: Carbon Fiber Fabric Repair Prepreg, 120 °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: AMS3970/4 specifies the batch release and delivery requirements for film adhesive used for repair. This specification is applicable only when the film adhesive is used as part of the prepreg system as defined in AMS3970 and AMS3970/1.

Rationale

Content: AMS3970/4A has been reaffirmed to comply with the SAE five-year review policy.

Meta Tags

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

Details

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

Pages: 10

Citation: SAE International Material Specification, Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 4 - Purchasing Specification for Film Adhesive, SAE Standard AMS3970/4A, Reaffirmed December 2016, Revised April 2011, Issued December 1999, https://doi.org/10.4271/AMS3970/4A.

Additional Details

Publisher: SAE International

Published: Dec 6, 2016

Product Code: AMS3970/4A

Content Type: Material Specification

Status: Reaffirmed

Language: English

Historical