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Meet the SAE CACRC

2019-08-19
Meet the SAE CACRC, a collection of industry experts dedicated to the safety, security, and efficiency of composite repairs in the airline industry. ...Get involved and learn more about CACRC here.
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

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.
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.
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

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

2014-03-17
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

Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 0 - Introduction

2011-04-01
CURRENT
AMS3970A
This document (Technical Specification) gives information about qualification rules and the relation between the different specification parts involved, such as the Technical Specification (TS), Material Specification (MS), and Purchasing Specification (PS). The link to the material qualification and qualified products is presented.
Standard

Solid Composite Laminate NDI Reference Standards

2011-12-20
CURRENT
ARP5605A
This recommended practice establishes a generic composite reference standard that will accommodate nondestructive inspections (NDI) on the full array of glass fiber and carbon fiber laminates found on aircraft.
Standard

Maintenance Life Cycle Cost Model

2010-03-22
CURRENT
AIR5416
This document describes a life cycle cost model for commercial aircraft composite structure. The term life cycle cost used herein, refers to the airline costs for maintenance, spares support, fuel, repair material and labor associated with composites after introduction into service and throughout its useful life. This document contains the equations that can be programmed into software which is used to estimate the total cost of ownership aircraft, including structure. Modification costs and operating costs are estimated over a specified life (any period up to 30 years). Modification costs include spares holding, training, support equipment, and other system related costs. Annual operating costs include: Schedule interruption, fuel, spares, insurance, and maintenance. Maintenance costs are separated by scheduled maintenance or unscheduled damage, or can by grouped into the typical organizations of line, shop, and hangar maintenance.
Standard

Composite Honeycomb NDI Reference Standards

2011-12-20
CURRENT
ARP5606A
This recommended practice establishes generic reference standards that will accommodate nondestructive inspections (NDI) on a broad range of non-metallic composite honeycomb structures found on aircraft.
Standard

Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 6 - Material Specification: Carbon Fiber Fabric Reinforced Epoxy Prepreg for Repair, Plain Weave Fabric, 193 g/m2, Adhesive Film for Repair and Non-Structural Glass Fiber Fabric Reinforced Epoxy Prepreg, 105 g/m2

2011-04-01
CURRENT
AMS3970/6
This Material Specification defines the requirements of carbon fiber reinforced epoxy prepreg for repair, 120 °C (250 °F) Vacuum curing, Plain Weave Fabric, 193 g/m2 and a companion non-structural glass fiber fabric reinforced epoxy prepreg, 105 g/m2, qualified according to AMS3970/1 and AMS3970/2 for aerospace application. The prepreg system may include an epoxy film adhesive to be applied in a co-curing process with the prepreg for joint and sandwich bonding. The need for a film adhesive shall be established during screening tests. If included, the requirements to be met by the adhesive are also defined in this document.
Standard

COMPOSITE REPAIR NDT/NDI HANDBOOK

1996-11-01
CURRENT
ARP5089
This document provides background information on the design, application, repair and inspection of composite structures, including metal bonding, used on civil transport aircraft. The objective of this document is to assist inspectors to know where to expect composite and metal bonded parts on the aircraft, to understand the capabilities of current NDT methods and to aid interpretation of inspection results. This document does not contain inspection procedures. It is intended to be informative and should not be used singularly, that is, it does not override any instructions that may be issued within a manufacturer's or operator's published documentation.
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