Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing, Part 1 - General Requirements

Product Code: AMS3970/1

Revision Number: A
Date Published: 2011-04-06

Issuing Committee:

Ams Cacrc Commercial Aircraft Composite Repair Committee

Scope

AMS3970/1 gives information about the technical requirements and qualification procedure for carbon fiber fabric epoxy prepreg and a companion non-structural glass prepreg used for repair of carbon fiber reinforced epoxy structures. The prepreg system may include a film adhesive to be applied in a co-curing process with the prepreg for joint and sandwich bonding. The need for a film adhesive shall be established during screening tests.

Product Status: In Stock

File Size: 229K

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Current & Historical versions of this standard
Standard	Date published	?Status
AMS3970/1A	2011-04-06	Revised
AMS3970/1	1999-12-01	Issued

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Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing, Part 1 - General Requirements

Issuing Committee:

Scope

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