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Standard

Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 4 - Purchasing Specification for Film Adhesive

1999-12-01

HISTORICAL

AMS3970/4

AMS 3970/4 specifies the batch release and delivery requirements for film adhesive used for repair. This specification is applicable when the film adhesive is part of the prepreg system as defined in AMS 3970 and AMS 3970/1.

Standard

Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Resin and Film Adhesive

1999-12-01

HISTORICAL

AMS3970/2

AMS 3970/2 gives specific information about the qualification program for carbon fiber reinforced epoxy structural repair prepreg systems, applicable for 125 °C (250 °F) vacuum curing. 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.

Standard

Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 1 - General Requirements

1999-12-01

HISTORICAL

AMS3970/1

AMS 3970/1 gives information about the technical requirements and qualification procedure for carbon fiber fabric epoxy prepreg used for repair of carbon fiber reinforced epoxy structures. The prepreg system may include a 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.

Standard

Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 3 - Purchasing Specification for Epoxy Prepreg

1999-12-01

HISTORICAL

AMS3970/3

AMS 3970/3 specifies the batch release and delivery requirements for carbon fiber fabric epoxy prepreg used for repair.

Standard

Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 0 - Introduction

1999-12-01

HISTORICAL

AMS3970

AMS 3970 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

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

Core Restoration of Thermosetting Composite Components

1998-12-01

HISTORICAL

ARP4991

This SAE Aerospace Recommended Practice (ARP) describes standard methods for restoring damaged core on commercial aircraft sandwich structures. It currently applies to wet lay up repairs only. The methods shall only be used when specified in an approved repair procedure or with the agreement of the Original Equipment Manufacturer (OEM) or regulatory authority. The repair materials shall be defined in the approved repairs referencing these methods.

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

TECHNICAL SPECIFICATION: CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL PART 2 - QUALIFICATION PROGRAM

1996-11-01

HISTORICAL

AMS2980/2

AMS 2980/2 gives specific information about the qualification program for carbon fiber fabric, epoxy systems and the material combination used for wet lay-up repair of carbon fiber reinforced epoxy structures.

Standard

TECHNICAL SPECIFICATION: CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL PURCHASING SPECIFICATION - RESIN

1996-11-01

HISTORICAL

AMS2980/4

This PS specifies the batch release and delivery requirements for epoxy resin systems (base resin and curing agent) used for wet lay-up repair purposes.

Standard

TECHNICAL SPECIFICATION: CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL PURCHASING SPECIFICATION - FABRIC

1996-11-01

HISTORICAL

AMS2980/3

This PS specifies the batch release and delivery requirements for carbon fiber and carbon fabric used for wet lay-up repair purposes.

Standard

TECHNICAL SPECIFICATION: CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL PART 1 - GENERAL REQUIREMENTS

1996-11-01

HISTORICAL

AMS2980/1

AMS 2980/1 gives information about the technical requirements and qualification procedure for carbon fiber fabric and epoxy resin systems used for wet lay-up repair of carbon fiber reinforced epoxy structures.

Standard

COMPOSITE AND BONDED STRUCTURE TECHNICIAN/SPECIALIST: TRAINING DOCUMENT

1996-09-01

HISTORICAL

AIR4938

This is a general curriculum that has been developed to identify the minimum knowledge and skill requirements of a composite and metal bond repair technician/specialist. Teaching levels have been assigned to the curriculum to define the knowledge, skills and abilities graduates will need to make safe, effective repairs. Minimum hours of instruction have been provided to ensure adequate coverage of all subject matter - lecture and laboratory. These minimums may be exceeded, and may include an increase in the total number of training hours and/or increases in the teaching levels.

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.