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Product Code:SAE AMS3970/2
Title:Carbon Fiber Fabric Repair Prepreg, 125Mdc (250Mdf) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Resin and Film Adhesive
Issuing Committee:Ams Cacrc Commercial Aircraft Composite Repair Committee
Scope:AMS 3970/2 gives specific information about the qualification program for carbon fiber reinforced epoxy structural repair prepreg systems, applicable for 125 掳C (250 掳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.