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Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 1 - General Requirements
- Aerospace Material Specification
- AMS6885/1
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
AMS6885/1 gives information about the technical requirements and qualification procedure for unidirectional carbon fiber tape epoxy repair prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. The repair system includes an epoxy film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding.
Rationale
Provide a unidirectional carbon fiber tape epoxy repair prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. The repair system includes a film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding. AMS6885/1 defines the qualification process and test methods.
Topic
Data Sets - Support Documents
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| 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 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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