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
- Aerospace Material Specification
- AMS2980/5
- Issued
Scope
Rationale
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Table 1 | Material Description | |
Table 2 | Cure Cycle | |
Table 3 | Wet Lay-Up Process | |
Table 4 | Resin Work Life and Storage Conditions | |
Table 5 | Properties of Unmixed Resin and Curing Agent | |
Table 6 | Properties of Mixed Uncured Resin | |
Table 7 | Properties of Cured Neat Resin | |
Table 8 | Requirements for Carbon Fiber | |
Table 9 | Requirements for Carbon Fabric | |
Table 10 | Main Laminate Composite Properties | |
Table 11 | Fluid Resistance and Glass Transition Temperature | |
Table 12 | Composite Design Related Properties | |
Table 13 | Composite Joint Properties | |
Table 14 | Composite Properties – Vertical Bleeding Process |
Issuing Committee
AMS CACRC Commercial Aircraft Composite Repair Committee
Scope:The Charter of the SAE Commercial Aircraft Composite Repair Committee (CACRC) is to promote repair and modification standardization and to provide guidance to composite and bonded structure maintenance providers, airlines, regulators, material suppliers and OEMs. The seven CACRC task groups are: Design, Inspection, Mods, Procedures, Repair Materials, Repair Techniques, and Training. 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.