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SAE Standards

AMS CACRC Commercial Aircraft Composite Repair Committee

Current List of Works In Progress (WIP):
For more information, click on the Document Number

Document Number
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Title
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AIR4844C   Composites and Metal Bonding Glossary
AIR4938A AIR4938 Composite and Bonded Structure Technician/Specialist: Training Document
AIR5367   Machining of Epoxy and Polyester Matrix Thermosetting Composite Structures
AIR5416   Maintenance Life Cycle Cost
AIR5702   Storage and Handling of Epoxy Thermosetting Composite Materials
AIR5946   Design and Application of Composite Repairs for Thermosetting Composites
AMS2950   Paste Adhesive For Core Restoration
AMS3970/1A   Carbon Fiber Fabric Repair Prepreg, 125Mdc (250Mdf) Vacuum Curing Part 1 - General Requirements
AMS3970/2A   Carbon Fiber Fabric Repair Prepreg, 125Mdc (250Mdf) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Resin and Film Adhesive
AMS3970/3A   Carbon Fiber Fabric Repair Prepreg, 125Mdc (250Mdf) Vacuum Curing Part 3 - Purchasing Specification for Epoxy Prepreg
AMS3970/4A   Carbon Fiber Fabric Repair Prepreg, 125Mdc (250Mdf) Vacuum Curing Part 4 - Purchasing Specification for Film Adhesive
AMS3970/5   Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing. Part 5 – Purchasing Specification for Companion Non-Structural Glass Fiber Fabric Prepreg
AMS3970A   Carbon Fiber Fabric Repair Prepreg, 125Mdc (250Mdf) Vacuum Curing Part 0 - Introduction
ARP5701   Lay-up of Pre-preg Composite Materials
CACRC07AA   Glass Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 0 - Introduction
CACRC07AB   Glass Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing. Part 1 - General Requirements
CACRC07AC   Glass Fiber Reinforced Repair Prepreg, 120 °C (250 °F) Vacuum Curing. Part 2 – Qualification Program for Fiber, Reinforced, Epoxy, Glass Prepreg, Film Adhesive and Non-Structural Glass Prepreg
CACRC07AD   Glass Fiber Reinforced Repair Prepreg, 120 °C (250 °F) Vacuum Curing.Part 3 – Purchasing Specification for Fiber, Reinforced, Epoxy, Glass Prepreg
CACRC07AE   Glass Fiber Reinforced Repair Prepreg, 120 °C (250 °F) Vacuum Curing. Part 4 – Purchasing Specification for Film Adhesive
CACRC07AF   Glass Fiber Reinforced Repair Prepreg, 120 °C (250 °F) Vacuum Curing. Part 5 – Purchasing Specification for Companion Non-Structural Glass Fiber Fabric Prepreg

Committee Document List

For individual committee information and Works In Progress lists, please click below:

Aerospace Materials Division (Coordinating Committee)
AMS CACRC Commercial Aircraft Composite Repair Committee

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