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SAE International - AMS2950/1

Paste Adhesive for Core Restoration Part 1 - General Requirements

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Organization: SAE International
Publication Date: 17 September 2019
Status: active
description:

This Technical Specification gives information about technical requirements and qualification procedures of adhesive paste with or without thickening agent for core restoration of aircraft... View More

Document History

AMS2950/1
September 17, 2019
Paste Adhesive for Core Restoration Part 1 - General Requirements
This Technical Specification gives information about technical requirements and qualification procedures of adhesive paste with or without thickening agent for core restoration of aircraft components.

References

This document references:
AIR4844 - COMPOSITES AND METAL BONDING GLOSSARY
Published by SAE International on December 1, 1994
The following terminology has been generated by the ATA/IATA/SAE Commercial Aircraft Composite Repair Committee (CACRC) and provides terminology for design, fabrication, and repair of composite and...
This document references:
AMS2980/1 - TECHNICAL SPECIFICATION: CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL PART 1 - GENERAL REQUIREMENTS
Published by SAE International on November 1, 1996
AMS 2980/1 gives information about the technical requirements and qualification procedure for carbon fiber fabric and epoxy resin systems used for wet lay-up repair of carbon fiber reinforced epoxy...
This document references:
AMS2980/5 - Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Part 5 - Material Specification: Carbon Fiber Fabrics, Plain Weave, 193 g/m2, and Epoxy Resin
Published by SAE International on January 26, 2006
This Material Specification defines the requirements of carbon fiber fabric and epoxy resin systems used for wet lay-up repair of carbon fiber reinforced epoxy structures, qualified according to AMS...
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