Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Carbon Prepreg, Film Adhesive and Non-Structural Glass Prepreg
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Product Code: AMS3970/2
Revision Number: A
Date Published: 2011-04-01
Issuing Committee:
Ams Cacrc Commercial Aircraft Composite Repair Committee
Scope
AMS3970/2 gives specific information about the qualification program for carbon fiber reinforced epoxy structural repair prepreg systems, applicable for 120 °C (250 °F) vacuum curing. The prepreg system may include an epoxy 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:
136K
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| Current & Historical versions of this standard |
|---|
| Standard |
Date published |
?Status |
| AMS3970/2A |
2011-04-01 |
Revised |
| AMS3970/2 |
1999-12-01 |
Issued |
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