SAE AMS 3970/6 : 2011
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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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]
Available format(s)
Hardcopy , PDF
Superseded date
11-08-2020
Superseded by
Language(s)
English
Published date
01-01-2011
Publisher
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. REQUIREMENTS
5. NOTES
Describes the requirements of carbon fiber reinforced epoxy prepreg for repair, 120 degrees C (250 degrees F) Vacuum curing, Plain Weave Fabric, 193 g/m[2] and a companion non-structural glass fiber fabric reinforced epoxy prepreg, 105 g/m[2], qualified according to AMS3970/1 and AMS3970/2 for aerospace application.
| Committee |
AMS CACRC
|
| DocumentType |
Standard
|
| Pages |
24
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| 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 AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
| EN 2559:1997 | Aerospace series - Carbon fibre preimpregnates - Determination of the resin and fibre content and the mass of fibre per unit area |
| ASTM D 5961/D5961M : 2017 : REDLINE | Standard Test Method for Bearing Response of Polymer Matrix Composite Laminates |
| 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 |
| 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 |
| 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 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 |
| 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 |
| EN 2330:1993 | Aerospace series - Textile glass fibre preimpregnates - Test method for the determination of the content of volatile matter |
| 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 |
| 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 |
| 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 |
| PREN 6040 : 200P1 | AEROSPACE SERIES - NON-METALLIC MATERIALS - TEST METHOD - ANALYSIS OF THERMOSET SYSTEMS BY HIGH PERFORMANCE - LIQUID CHROMATOGRAPHY (HPLC) |
| 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 |
| SAE AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
| 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 |
| EN 2557:1997 | Aerospace series - Carbon fibre preimpregnates - Determination of mass per unit area |
| 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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