This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 3 - Purchasing Specification for Epoxy Prepreg
- Aerospace Material Specification
Published December 01, 1999 by SAE International in United States
Downloadable datasets availableAnnotation ability available
AMS 3970/3 specifies the batch release and delivery requirements for carbon fiber fabric epoxy prepreg used for repair.
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Unnamed Dataset 3|
|Unnamed Dataset 4|
|Unnamed Dataset 5|
AMS CACRC Commercial Aircraft Composite Repair Committee
Scope: The charter of the ATA/IATA/SAE Commercial Aircraft Composite Repair Committee (CACRC) is to develop and improve maintenance, inspection and repair of commercial aircraft composite structure and components. The seven CACRC task groups are: Repair Materials, Repair Techniques, Analytical Repair Techniques, Design, Inspection, Training and Airline Inspection & Repair Conditions.No copyrighted material may be posted in this forum. SAE is not liable for opinions expressed or information posted to this forum. All information posted becomes the property of SAE.
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.