Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 1 - General Requirements
- Aerospace Material Specification
- AMS6885/1
- Issued
Scope
Rationale
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
Unnamed Dataset 3 | ||
Unnamed Dataset 4 | ||
Unnamed Dataset 5 | ||
Unnamed Dataset 6 | ||
Unnamed Dataset 7 | ||
Table 1 | Defect description and criteria for carbon fiber tape prepreg | |
Table 2 | Defect description and criteria for film adhesive | |
Table 3 | Side qualification program | |
Table 4 | Storage conditions and times for laminate specimens | |
Table 5 | Storage conditions and times for sandwich specimens | |
Table 6 | Fluid types for immersion testing | |
Unnamed Dataset 14 | ||
Unnamed Dataset 15 | ||
Unnamed Dataset 16 |
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.
Reference
Number | Title |
---|