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Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 5 - Material Specification for Unidirectional Carbon Fiber Tape Epoxy Prepreg for Repair and Film Adhesive for Repair, 120 to 145 °C (250 to 290 °F) Curing
- Aerospace Material Specification
- AMS6885/5
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
AMS6885/5 is the Material Specification (MS) which defines the requirements of a unidirectional carbon fiber tape epoxy repair prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. It also defines the requirements of an epoxy film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding.
Rationale
AMS6885/5 defines the requirements of a unidirectional carbon fiber tape epoxy prepreg for repair and film adhesive for repair to be cured in the range of 120 to 145 °C (250 to 290 °F).
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Table 1 | Carbon fiber tape prepreg description | |
| Table 2 | Film adhesive description | |
| Table 3 | Cure cycle | |
| Table 4 | Carbon fiber tape prepreg and film adhesive work life and storage life | |
| Table 5 | Physical and chemical properties of uncured carbon fiber tape prepreg | |
| Table 6 | Physical and chemical properties of uncured film adhesive | |
| Table 7 | Physical properties of cured carbon fiber tape prepreg | |
| Table 8 | Physical properties of cured film adhesive | |
| Table 9 | Main laminate composite properties (carbon fiber tape prepreg - Grade 134) | |
| Table 10 | Main laminate composite properties (carbon fiber tape prepreg - Grade 194) | |
| Table 11 | Fluid resistance (carbon fiber tape prepreg and composite joint) | |
| Table 12 | Composite design related properties (carbon fiber tape prepreg - Grade 134 and Grade 194) | |
| Table 13 | Composite joint properties | |
| Table 14 | Composite sandwich properties | |
| Table 15 | Cured film adhesive - bondline properties |
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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