SAE AMS3970/2 PDF

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Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 2 – Qualification Program for Fiber, Fabric, Resin and Film Adhesive

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Description

AMS 3970/2 gives specific information about the qualification program for carbon fiber reinforced epoxy structural repair prepreg systems, applicable for 125 °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.

History

AMS3970/2A 2016-12-06 Latest Reaffirmed
AMS3970/2 1999-12-01 Historical Issued
ISSUING COMMITTEE

AMS CACRC Commercial Aircraft Composite Repair Committee

DATE

1999-12-01

DOI

https://doi.org/10.4271/AMS3970/2

PAGE

17

PUBLISHER

SAE International

REVISED

ISSUED

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SAE AMS3970/2 PDF
$118.00 Original price was: $118.00.$67.26Current price is: $67.26.