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Standard

Composites and Metal Bonding Glossary

2017-06-20
CURRENT
AIR4844C
The following terminology has been generated by the ATA/IATA/SAE Commercial Aircraft Composite Repair Committee (CACRC) and provides terminology for design, fabrication, and repair of composite and bonded metal structures.
Book

Care and Repair of Advanced Composites, Second Edition

2005-06-22
A worldwide reference for repair technicians and design engineers, the book is an outgrowth of the course syllabus that was developed by the Training Task Group of SAE's Commercial Aircraft Composite Repair Committee (CACRC) and published as SAE AIR 4938, Composite and Bonded Structure Technician Specialist Training Document.
Standard

COMPOSITES AND METAL BONDING GLOSSARY

1997-03-01
HISTORICAL
AIR4844A
The following terminology has been generated by the ATA/IATA/SAE Commercial Aircraft Composite Repair Committee (CACRC) and provides terminology for design, fabrication, and repair of composite and bonded metal structures.
Standard

Composites and Metal Bonding Glossary

1999-09-01
HISTORICAL
AIR4844B
The following terminology has been generated by the ATA/IATA/SAE Commercial Aircraft Composite Repair Committee (CACRC) and provides terminology for design, fabrication, and repair of composite and bonded metal structures.
Standard

COMPOSITES AND METAL BONDING GLOSSARY

1994-12-01
HISTORICAL
AIR4844
The following terminology has been generated by the ATA/IATA/SAE Commercial Aircraft Composite Repair Committee (CACRC) and provides terminology for design, fabrication, and repair of composite and bonded metal structures.
Book

Care and Repair of Advanced Composites, 3rd Edition

2020-12-31
Chesmar is also an active member of SAE International's CACRC (Commercial Aircraft Composite Repair Committee), an elite group of industry experts dedicated to the standardization, safety, security, and efficiency of composite repairs in the airline industry.
SAE MOBILUS Subscription

MRO Standards Subscription

2017-11-30
The MRO Standards Subscription is an annual subscription to the historical and current standards output by the following committees: AGE-3 Aircraft Ground Support Equipment Committee Aerospace Industry Steering Committee on Structural Health G-19 Counterfeit Electronic Parts Committee G-19A Test Laboratory Standards Development Committee G-19AD Authorized Distributor Committee E-32 Aerospace Propulsion Systems Health Management Committee HM-1 Integrated Vehicle Health Management Committee AMS AM Additive Manufacturing Metals Committee AMS AM Additive Manufacturing Polymer Committee AMS CACRC Commercial Aircraft Composite Repair Committee G-19C Standards Compliance Verification Committee G-19C1 Continuous Improvment Committee G-19D Distributor Committee G-19DR Distributor Risk Characterization Committee G-19T Terms and Definitions Committee G-20 Airport Lighting Committee G-21 Counterfeit Material Committee G21R Counterfeit Refrigerants Committee G-23 Manufacturing Management Committee G-25 Avionics and Electronics Corrosion Committee G-11 Reliability Maint Support and Probabilistic Methods Committee G-11M Maintainability, Supportability and Logistics Committee G-11PM Probabilistic Methods Committee G-11R Reliability Committee AMS J Aircraft Maintenance Chemicals and Materials Committee G-45 Human Systems Integration Committee ASEC Aerospace Surface Enhancement Committee AMS G8 Aerospace Organic Coatings Committee AMS G9 Aerospace Sealing Comittee G-41 Reliability Committee G-47 Systems Engineering Committee G-48 System Safety Committee EIDM Enterprise Information and Data Management Committee Updated as new standards are published, users will have access to all the latest aerospace standards surrounding MRO methods, materials, and technologies.
Standard

Composites and Metal Bonding Glossary

2019-04-24
WIP
AIR4844D
The following terminology has been generated by the ATA/IATA/SAE Commercial Aircraft Composite Repair Committee (CACRC) and provides terminology for design, fabrication, and repair of composite and bonded metal structures. ...The purpose of this AIR is to provide terminology that should be used when developing CACRC repair documents or repair documents produced by airlines or airframe and engine manufacturers.
Standard

Reporting of Damage to Composite Structure

2021-03-29
WIP
AIR7509
A guidance document is proposed as the initial step in which it is documented what essential information is required for a composite repair with the aim to reduce to number of back and forward communications, improve the documents to define damage such as mapping, damage descriptions, sketches, pictures. CACRC Procedures Task Group will be drafting the document.
Standard

Mixing Resins, Adhesives and Potting Compounds

2022-02-02
CURRENT
ARP5256A
This SAE Aerospace Recommended Practice (ARP) describes and gives general guidelines on use and applicability of the standard method for mixing resins, adhesives, and potting compounds.
Standard

Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Part 5 - Carbon Fiber Fabrics, Plain Weave, 193 g/m2, and Epoxy Resin

2021-09-24
CURRENT
AMS2980/5A
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.
Standard

Carbon Fiber Fabric and Epoxy Resin Wet Lay-Up Repair Material Part 0 - Introduction

2021-09-23
CURRENT
AMS2980B
This document (Technical Specification) gives information about qualification rules and the relation between the different specification parts involved, such as Technical Specification (TS), Material Specification (MS), and Purchasing Specification (PS). The link to material qualification and qualified products is presented.
Standard

DRYING OF THERMOSETTING COMPOSITE MATERIALS

2021-05-14
CURRENT
ARP4977
This SAE Aerospace Recommended Practice (ARP) describes standard methods for drying commercial aircraft composite structures prior to repair and gives general guidelines on use and applicability. It addresses the removal of liquids that have collected inside the structures through open damage, microcracks, or porosity and the removal of absorbed moisture from the composite material. The methods described in this document shall only be used when specified in an approved repair document or with the agreement of the original equipment manufacturer (OEM) or regulatory authority. If this document is used for the drying of materials other than thermosetting composite materials, the fitness for this purpose must be determined by the user.
Standard

Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 1 - General Requirements

2021-02-23
CURRENT
AMS6885/1
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.
Standard

Unidirectional Carbon Fiber Tape Epoxy Repair Prepreg, Vacuum Curing Part 2 - Qualification Program for Fiber, Carbon Fiber Tape Prepreg, and Film Adhesive

2021-02-23
CURRENT
AMS6885/2
AMS6885/2 gives specific information about the qualification program for unidirectional carbon fiber tape epoxy repair prepreg capable of curing under vacuum for repair of carbon fiber reinforced epoxy structures. The prepreg system shall include an epoxy film adhesive to be applied in a co-bonding process with the prepreg for solid laminate and sandwich bonding.
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