SAE Standards Works
SAE Home
Contact Us
|
Help
|
Shopping Cart
User Id:
Password:
Remember Me
Home
AMS CACRC Commercial Aircraft Composite Repair Committee
AMS3970/2A - 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
Document
Main
Purchase
New Project Request
Details
Document Number:
AMS3970/2A
Revision Number:
A
Title
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
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.
Recent Activity
Date
Type