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Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Part 5 - Carbon Fiber Fabrics, Plain Weave, 193 g/m2, and Epoxy Resin
- Aerospace Material Specification
- AMS2980/5A
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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 AMS2980/1 and AMS2980/2.
Unless otherwise specified by the drawing, the order or the inspection schedule, the present specification shall be used in conjunction with the referenced documents.
Rationale
AMS2980/5A is a Five Year Review and update of this specification.
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 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.
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