SAE AMS3970/2 Carbon Fiber Fabric Repair Prepreg, 125 掳C (250 掳F) Vacuum Curing Part 2 - Qualification Program for Fiber
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Product Code:SAE AMS3970/2
Title:Carbon Fiber Fabric Repair Prepreg, 125 掳C (250 掳F) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Carbon Prepreg, Film Adhesive and Non-Structural Glass Prepreg
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 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.
Title:Carbon Fiber Fabric Repair Prepreg, 125 掳C (250 掳F) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Carbon Prepreg, Film Adhesive and Non-Structural Glass Prepreg
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 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.
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