This Purchasing Specification, AMS6885/4, specifies the batch release and delivery requirements for film adhesive used for repair. This specification is applicable only when the film adhesive is used as part of the repair system defined in AMS6885 and AMS6885/1.
This specification also defines the procedure and requirements for storage life extension of materials purchased against this specification. It is only applicable for materials qualified against AMS6885 (refer to PRI-QPL-AMS6885), and shall be carried out within the responsibility of the purchaser and under control of its Quality organisation.
Rationale
Provide a unidirectional carbon fiber tape epoxy prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. The prepreg system includes a film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding. AMS6885/4 is the purchasing specification for the film adhesive.
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.
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AMS6885/4
Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 4 - Purchasing Specification for Film Adhesive
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Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 4 - Purchasing Specification for Film Adhesive
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