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Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 5 - Purchasing Specification for Companion Non-Structural Glass Fiber Fabric Prepreg
- Aerospace Material Specification
Published December 05, 2016 by SAE International in United States
Downloadable datasets availableAnnotation ability available
The PS, AMS3970/5, specifies the batch release and delivery requirements for the companion non-structural glass fiber fabric prepreg.
AMS3970/5 has been reaffirmed to comply with the SAE five-year review policy.
Data Sets - Support Documents
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|TABLE 1||BATCH RELEASE FOR UNCURED NON-STRUCTURAL GLASS PREPREG - PHYSICAL AND PHYSIOCHEMICAL PROPERTIES|
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.
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