Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 6 - Material Specification: Carbon Fiber Fabric Reinforced Epoxy Prepreg for Repair, Plain Weave Fabric, 193 g/m2, Adhesive Film for Repair and Non-Structural Glass Fiber Fabric Reinforced Epoxy Prepreg, 105 g/m2
- Aerospace Material Specification
- AMS3970/6
- Reaffirmed
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 | ||
| TABLE 1 | CARBON FIBER REINFORCED EPOXY PREPREG MATERIAL DESCRIPTION | |
| TABLE 2 | ADHESIVE FILM MATERIAL DESCRIPTION | |
| TABLE 3 | NON-STRUCTURAL GLASS FIBER REINFORCED EPOXY PREPREG MATERIAL DESCRIPTION | |
| TABLE 4 | CARBON FIBER REINFORCED EPOXY PREPREG CURE CYCLE , | |
| TABLE 5 | CARBON FIBER REINFORCED EPOXY PREPREG WORK LIFE AND STORAGE CONDITIONS | |
| TABLE 6 | ADHESIVE FILM WORK LIFE AND STORAGE CONDITIONS | |
| TABLE 7 | NON-STRUCTURAL GLASS FIBRE REINFORCED EPOXY PREPREG WORK LIFE AND STORAGE CONDITIONS | |
| TABLE 8 | PHYSICAL AND PHYSICOCHEMICAL PROPERTIES OF UNCURED CARBON PREPREG | |
| TABLE 9 | PHYSICAL AND PHYSICOCHEMICAL PROPERTIES OF UNCURED ADHESIVE | |
| TABLE 10 | PHYSICAL AND PHYSICOCHEMICAL PROPERTIES OF UNCURED NON-STRUCTURAL GLASS PREPREG | |
| TABLE 11 | PHYSICOCHEMICAL PROPERTIES OF UNCURED CARBON AND GLASS PREPREG (MIXED) COMPATIBILITY | |
| TABLE 12 | PHYSICAL PROPERTIES OF CURED CARBON PREPREG | |
| TABLE 13 | PHYSICAL PROPERTIES OF CURED ADHESIVE | |
| TABLE 14 | PHYSICAL PROPERTIES OF CURED NON-STRUCTURAL GLASS PREPREG | |
| TABLE 15 | MAIN LAMINATE COMPOSITE PROPERTIES (CARBON PREPREG) (AR) | |
| TABLE 16 | MAIN LAMINATE COMPOSITE PROPERTIES (CARBON PREPREG) (WET) | |
| TABLE 17 | FLUID RESISTANCE (CARBON PREPREG) | |
| TABLE 18 | COMPOSITE DESIGN RELATED PROPERTIES (CARBON PREPREG) (AR) | |
| TABLE 19 | COMPOSITE DESIGN RELATED PROPERTIES (CARBON PREPREG) (WET) | |
| TABLE 20 | COMPOSITE JOINT PROPERTIES | |
| TABLE 21 | COMPOSITE SANDWICH PROPERTIES | |
| TABLE 22 | CURED ADHESIVE - SHEAR STRESS-STRAIN PROPERTIES. | |
| Unnamed Dataset 28 | ||
| TABLE 23 | CURED ADHESIVE - SHEAR STRESS-STRAIN PROPERTIES. | |
| Unnamed Dataset 30 |
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.