SAE AMS3970/1A
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements
Available format(s)
Hardcopy , PDF
Superseded date
24-10-2019
Language(s)
English
Published date
06-12-2016
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. REQUIREMENTS
5. QUALIFICATION
6. COMPOSITE TEST METHODS AND SPECIMEN MANUFACTURING
7. NOTES
APPENDIX A - AUTHORIZED ANCILLARY MATERIALS
Provides information about the technical requirements and qualification procedure for carbon fiber fabric epoxy prepreg and a companion non-structural glass prepreg used for repair of carbon fiber reinforced epoxy structures.
| DocumentType |
Standard
|
| Pages |
45
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| Supersedes |
AMS3970/1 gives information about the technical requirements and qualification procedure for carbon fiber fabric epoxy prepreg and a companion non-structural glass 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.
| SAE AMS3970A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 0 - Introduction |
| SAE AMS 3970/2 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 2: QUALIFICATION PROGRAM FOR FIBER, FABRIC, CARBON PREPREG, FILM ADHESIVE AND NON-STRUCTURAL GLASS PREPREG |
| SAE AMS 3970/6 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 6 - MATERIAL SPECIFICATION: CARBON FIBER FABRIC REINFORCED EPOXY PREPREG FOR REPAIR, PLAIN WEAVE FABRIC, 193 G/M[2], ADHESIVE FILM FOR REPAIR AND NON-STRUCTURAL GLASS FIBER FABRIC REINFORCED EPOXY PREPREG, 105 G/M[2] |
| SAE AMS3970/3A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 3 - Purchasing Specification for Carbon Prepreg |
| SAE AMS 3970/5 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 5: PURCHASING SPECIFICATION FOR COMPANION NON-STRUCTURAL GLASS FIBER FABRIC PREPREG |
| SAE AMS 3970/4 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 4: PURCHASING SPECIFICATION FOR FILM ADHESIVE |
| EN 2559:1997 | Aerospace series - Carbon fibre preimpregnates - Determination of the resin and fibre content and the mass of fibre per unit area |
| EN 2565:2013 | Aerospace series - Preparation of carbon fibre reinforced resin panels for test purposes |
| ASTM D 5961/D5961M : 2017 : REDLINE | Standard Test Method for Bearing Response of Polymer Matrix Composite Laminates |
| SAE AMS 3970/6 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 6 - MATERIAL SPECIFICATION: CARBON FIBER FABRIC REINFORCED EPOXY PREPREG FOR REPAIR, PLAIN WEAVE FABRIC, 193 G/M[2], ADHESIVE FILM FOR REPAIR AND NON-STRUCTURAL GLASS FIBER FABRIC REINFORCED EPOXY PREPREG, 105 G/M[2] |
| ISO 10119:2002 | Carbon fibre Determination of density |
| PREN 2379 : 200P1 | AEROSPACE SERIES - FLUIDS FOR ASSESSMENT OF NON-METALLIC MATERIALS |
| SAE AMS 3970/2 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 2: QUALIFICATION PROGRAM FOR FIBER, FABRIC, CARBON PREPREG, FILM ADHESIVE AND NON-STRUCTURAL GLASS PREPREG |
| ISO 10120:1991 | Carbon fibre — Determination of linear density |
| PREN 6062 : 200P1 | AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - TEST METHOD - FLATWISE TENSILE TEST OF COMPOSITE SANDWICH PANEL |
| PREN 6060 : 200P1 | AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - TEST METHOD - DETERMINATION OF THE TENSILE SINGLE LAP SHEAR STRENGTH |
| EN 2563:1997 | Aerospace series - Carbone fibre reinforced plastics - Unidirectional laminates - Determination of the apparent interlaminar shear strength |
| PREN 3003 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - DETERMINATION OF MASS PER UNIT AREA OF FILM ADHESIVES - TEST METHOD |
| ASTM D 5229/D5229M : 2014-06 | TEST METHOD FOR MOISTURE ABSORPTION PROPERTIES AND EQUILIBRIUM CONDITIONING OF POLYMER MATRIX COMPOSITE MATERIALS |
| EN 6034:2015 | Aerospace series - Carbon fibre reinforced plastics - Test method - Determination of interlaminar fracture toughness energy - Mode II - GIIC |
| EN 6038:2015 | Aerospace series - Fibre reinforced plastics - Test method - Determination of the compression strength after impact |
| ISO 1890:2009 | Reinforcement yarns Determination of twist |
| ISO 11357-5:2013 | Plastics — Differential scanning calorimetry (DSC) — Part 5: Determination of characteristic reaction-curve temperatures and times, enthalpy of reaction and degree of conversion |
| EN 6037:2015 | Aerospace series - Fibre reinforced plastics - Test method - Determination of bearing strength |
| EN 6031:2015 | Aerospace series - Fibre reinforced plastics - Test method - Determination of in-plane shear properties (± 45° tensile test) |
| ASTM D 5528 : 2013 : REDLINE | Standard Test Method for Mode I Interlaminar Fracture Toughness of Unidirectional Fiber-Reinforced Polymer Matrix Composites |
| ASTM C 393 : 2000 | Standard Test Method for Flexural Properties of Sandwich Constructions |
| SAE AMS 3970/5 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 5: PURCHASING SPECIFICATION FOR COMPANION NON-STRUCTURAL GLASS FIBER FABRIC PREPREG |
| ASTM D 2344/D2344M : 2016 : REDLINE | Standard Test Method for Short-Beam Strength of Polymer Matrix Composite Materials and Their Laminates |
| PREN 6043 : 200P1 | AEROSPACE SERIES - THERMOSETTING RESIN SYSTEMS - TEST METHOD - DETERMINATION OF GEL TIME AND VISCOSITY |
| EN 2329:1993 | Aerospace series - Textile glass fibre preimpregnates - Test method for the determination of mass per unit area |
| EN 2561:1995 | Aerospace series - Carbon fibre reinforced plastics - Unidirectional laminates - Tensile test parallel to the fibre direction |
| EN 2489:1995 | Aerospace series - Fibre reinforced plastics - Determination of the action of test fluids |
| SAE AMS 3970/4 : 2011 | CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 4: PURCHASING SPECIFICATION FOR FILM ADHESIVE |
| EN 6033:2015 | Aerospace series - Carbon fibre reinforced plastics - Test method - Determination of interlaminar fracture toughness energy - Mode I - GIC |
| ISO 11357-2:2013 | Plastics Differential scanning calorimetry (DSC) Part 2: Determination of glass transition temperature and glass transition step height |
| ISO 10618:2004 | Carbon fibre — Determination of tensile properties of resin-impregnated yarn |
| PREN 6066 : 200P1 | AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - TEST METHOD - DETERMINATION OF TENSILE STRENGTH OF A TAPERED AND STEPPED JOINTS |
| ISO 1183:1987 | Plastics Methods for determining the density and relative density of non-cellular plastics |
| EN 2560:1998 | Aerospace series - Carbon fibre preimpregnates - Determination of the resin flow |
| PREN 2823 : 200P2 | AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - DETERMINATION OF THE EFFECT OF EXPOSURE TO HUMID ATMOSPHERE ON PHYSICAL AND MECHANICAL CHARACTERISTICS |
| EN 2330:1993 | Aerospace series - Textile glass fibre preimpregnates - Test method for the determination of the content of volatile matter |
| ISO 10548:2002 | Carbon fibre — Determination of size content |
| ASTM D 3518/D3518M : 2013-09 | TEST METHOD FOR IN-PLANE SHEAR RESPONSE OF POLYMER MATRIX COMPOSITE MATERIALS BY TENSILE TEST OF A +/-45 DEGREES LAMINATE |
| ASTM D 4440 : 2015 : REDLINE | Standard Test Method for Plastics: Dynamic Mechanical Properties Melt Rheology |
| ISO 472:2013 | Plastics — Vocabulary |
| EN 6032:2015 | Aerospace series - Fibre reinforced plastics - Test method - Determination of the glass transition temperatures |
| EN 6036:2015 | Aerospace series - Fibre reinforced plastics - Test method - Determination of notched, unnotched and filled hole compression strength |
| SAE ARP 4916 : 1997 | MASKING AND CLEANING OF EPOXY AND POLYESTER MATRIX THERMOSETTING COMPOSITE MATERIALS |
| ASTM D 3171 : 2015 : REDLINE | Standard Test Methods for Constituent Content of Composite Materials |
| MIL-DTL-83133 Revision J:2015 | TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34), NATO F-35, AND JP-8+100 (NATO F-37) |
| ASTM D 3531/D3531M : 2016 : REDLINE | Standard Test Method for Resin Flow of Carbon Fiber-Epoxy Prepreg |
| ASD-STAN prEN 6061 P1:1995 | AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - TEST METHOD - DETERMINATION OF SANDWICH FLEXURAL STRENGTH 4 POINT BENDING |
| PREN 6041 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - TEST METHOD - ANALYSIS ON NON-METALLIC MATERIALS (UNCURED) BY DIFFERENTIAL SCANNING CALORIMETRY (DSC) |
| ASTM C 297 : 1994 : R1999 | Standard Test Method for Flatwise Tensile Strength of Sandwich Constructions |
| MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
| PREN 6040 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - TEST METHOD - ANALYSIS OF THERMOSET SYSTEMS BY HIGH PERFORMANCE - LIQUID CHROMATOGRAPHY (HPLC) |
| ISO 9000:2015 | Quality management systems — Fundamentals and vocabulary |
| PREN 3615 : 200P2 | AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - DETERMINATION OF THE CONDITIONS OF EXPOSURE TO HUMID ATMOSPHERE AND OF MOISTURE ABSORPTION |
| ASTM D 3039/D3039M : 2017 : REDLINE | Standard Test Method for Tensile Properties of Polymer Matrix Composite Materials |
| PREN 6064 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - ANALYSIS OF NON-METALLIC MATERIALS (CURED) FOR THE DETERMINATION OF THE EXTENT OF CURE BY DIFFERENTIAL SCANNING CALORIMETRY (DSC) |
| SAE AMS C 9084 : 2013 | CLOTH, GLASS, FINISHED, FOR RESIN LAMINATES |
| PREN 2850 : 200P2 | AEROSPACE SERIES - CARBON FIBRE THERMOSETTING RESIN UNIDIRECTIONAL LAMINATES - COMPRESSION TEST PARALLEL TO FIBRE DIRECTION |
| SAE AMS3970/3A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 3 - Purchasing Specification for Carbon Prepreg |
| EN 6035:2015 | Aerospace series - Fibre reinforced plastics - Test method - Determination of notched and unnotched tensile strength |
| PREN 6042 : 200P1 | AEROSPACE SERIES - ORGANIC COMPOUNDS - TEST METHOD - ANALYSIS BY INFRARED SPECTROSCOPY |
| EN 2558:1997 | Aerospace series - Carbon fibre preimpregnates - Determination of the volatile content |
| ASTM D 6484/D6484M : 2014 : REDLINE | Standard Test Method for Open-Hole Compressive Strength of Polymer Matrix Composite Laminates |
| EN 2557:1997 | Aerospace series - Carbon fibre preimpregnates - Determination of mass per unit area |
| SAE AIR4844B | Composites and Metal Bonding Glossary |
| EN 2331:1993 | Aerospace series - Textile glass fibre preimpregnates - Test methods for the determination of the resin and fibre content and mass of fibre per unit area |
| SAE AMS3970A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 0 - Introduction |
| ASTM D 7137/D7137M : 2017 : REDLINE | Standard Test Method for Compressive Residual Strength Properties of Damaged Polymer Matrix Composite Plates |
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