EN 2489:1995
Current
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The latest, up-to-date edition.
Aerospace series - Fibre reinforced plastics - Determination of the action of test fluids
Published date
20-09-1995
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Foreword
1 Scope
2 Normative references
3 Principle
4 Test fluids
5 Apparatus
6 Specimens
7 Procedure
8 Expression of results
9 Designation
10 Test report
This standard specifies the method of immersion of fibre reinforced plastics in test fluids. It does not give any directives to meet health and safety requirements. It is the responsibility of the user of this standard to adopt appropriate health and safety precautions.
| Committee |
ASD-STAN
|
| DevelopmentNote |
Supersedes PREN 2489. (11/2003)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| DIN EN 2489:1995-11 | Identical |
| UNI EN 2489 : 1995 | Identical |
| SNV DIN EN 2489 : 1995 | Identical |
| PN EN 2489 : 1999 | Identical |
| BS EN 2489:1995 | Identical |
| NBN EN 2746 : 1998 | Identical |
| NBN EN 2489 : 1996 | Identical |
| NS EN 2489 : 1ED 1995 | Identical |
| I.S. EN 2489:1996 | Identical |
| UNE-EN 2489:1996 | Identical |
| NEN EN 2489 : 1995 | Identical |
| NF EN 2489 : 1996 | Identical |
| 93/706616 DC : 0 | PREN 2833-1 - AEROSPACE SERIES - TECHNICAL SPECIFICATION - GLASS FIBER THERMOSETTING PREIMPREGNATES - PART 1: GENERAL |
| PREN 2833-3 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 3: GLASS FABRIC/EPOXY RESIN PREIMPREGNATE CURING AT UP 180 DEGREES C FOR CONTINUOUS USE UP TO 120 DEGREES C |
| I.S. EN 6035:2015 | AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - TEST METHOD - DETERMINATION OF NOTCHED AND UNNOTCHED TENSILE STRENGTH |
| SAE AMS 2980/1 : 2014 | CARBON FIBER FABRIC AND EPOXY RESIN WET LAY-UP REPAIR MATERIAL - PART 1 - GENERAL REQUIREMENTS |
| I.S. EN 6036:2015 | AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - TEST METHOD - DETERMINATION OF NOTCHED, UNNOTCHED AND FILLED HOLE COMPRESSION STRENGTH |
| I.S. EN 2833-005:2013 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 005: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE |
| EN 2850:2017 | Aerospace series - Carbon fibre thermosetting resin - Unidirectional laminates - Compression test parallel to fibre direction |
| DIN EN 2561:1995-11 | AEROSPACE SERIES - CARBON FIBRE REINFORCED PLASTICS - UNIDIRECTIONAL LAMINATES - TENSILE TEST PARALLEL TO THE FIBRE DIRECTION |
| DIN EN 2746:1998-10 | AEROSPACE SERIES - GLASS FIBRE REINFORCED PLASTICS - FLEXURAL TEST, THREE POINT BEND METHOD |
| BS EN 2597:1998 | Carbon fibre reinforced plastics. Unidirectional laminates. Tensile test perpendicular to the fibre direction |
| BS EN 2850:2017 | Aerospace series. Carbon fibre thermosetting resin - Unidirectional laminates. Compression test parallel to fibre direction |
| BS EN 6035:2015 | Aerospace series. Fibre reinforced plastics. Test method. Determination of notched and unnotched tensile strength |
| UNI EN 2833-005 : 2014 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 005: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE |
| PREN 2833-5 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 5: GLASS FABRIC/PHENOLIC RESIN PREIMPREGNATE |
| DIN EN 2562:1997-05 | AEROSPACE SERIES - CARBON FIBRE REINFORCED PLASTICS - UNIDIRECTIONAL LAMINATES - FLEXURAL TEST PARALLEL TO THE FIBRE DIRECTION |
| DIN EN 2597:1998-08 | AEROSPACE SERIES - CARBON FIBRE REINFORCED PLASTICS - UNIDIRECTIONAL LAMINATES - TENSILE TEST PERPENDICULAR TO THE FIBRE DIRECTION |
| EN 6035:2015 | Aerospace series - Fibre reinforced plastics - Test method - Determination of notched and unnotched tensile strength |
| EN 2562:1997 | Aerospace series - Carbon fibre reinforced plastics - Unidirectional laminates - Flexural test parallel to the fibre direction |
| 95/714421 DC : 0 | PREN 2833-3 - AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 3: GLASS FABRIC/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 180 DEGREE C FOR CONTINUOUS USE UP TO 120 DEGREE C |
| 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] |
| BS EN 6036:2015 | Aerospace series. Fibre reinforced plastics. Test method. Determination of notched, unnotched and filled hole compression strength |
| BS EN 6031:2015 | Aerospace series. Fibre reinforced plastics. Test method. Determination of in-plane shear properties (± 45° tensile test) |
| BS EN 2563:1997 | Carbon fibre reinforced plastics. Unidirectional laminates. Determination of the apparent interlaminar shear strength |
| BS EN 2747:1998 | Glass fibre reinforced plastics. Tensile test |
| BS EN 2561:1995 | Carbon fibre reinforced plastics. Undirectional laminates. Tensile test parallel to the fibre direction |
| BS EN 2746:1998 | Glass fibre reinforced plastics. Flexural test. Three point bend method |
| EN 2597:1998 | Aerospace series - Carbon fibre reinforced plastics - Unidirectional laminates - Tensile test perpendicular to the fibre direction |
| EN 2747:1998 | Aerospace series - Glass fibre reinforced plastics - Tensile test |
| EN 2561:1995 | Aerospace series - Carbon fibre reinforced plastics - Unidirectional laminates - Tensile test parallel to the fibre direction |
| EN 2746:1998 | Aerospace series - Glass fibre reinforced plastics - Flexural test - Three point bend method |
| EN 2563:1997 | Aerospace series - Carbone fibre reinforced plastics - Unidirectional laminates - Determination of the apparent interlaminar shear strength |
| EN 6031:2015 | Aerospace series - Fibre reinforced plastics - Test method - Determination of in-plane shear properties (± 45° tensile test) |
| EN 2833-005:2013 | Aerospace series - Glass fibre thermosetting preimpregnates - Technical specification - Part 005: Glass fabric/phenolic resin preimpregnate |
| EN 6036:2015 | Aerospace series - Fibre reinforced plastics - Test method - Determination of notched, unnotched and filled hole compression strength |
| I.S. EN 6031:2015 | AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - TEST METHOD - DETERMINATION OF IN-PLANE SHEAR PROPERTIES (+/- 45 DEGREES TENSILE TEST) |
| SAE AMS3970/1A | Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 1 - General Requirements |
| DIN EN 6061:1996-04 (Draft) | AEROSPACE SERIES - FIBRE REINFORCED PLASTICS - TEST METHOD - DETERMINATION OF SANDWICH FLEXURAL STRENGTH, 4 POINT BENDING |
| 93/711194 DC : 0 | PREN 2833-2 - TECHNICAL SPECIFICATION - GLASS FIBRE THERMOSETTING PREIMPREGNATES - PART 2: GLASS FABRIC/EPOXY RESIN PREIMPREGNATES CURING AT 125 DEGREES C FOR CONTINUOUS USE UP TO 80 DEGREES C |
| BS EN 2833-005:2013 | Aerospace series. Glass fibre thermosetting preimpregnates. Technical specification Glass fabric/phenolic resin preimpregnate |
| 95/714422 DC : 0 | PREN 2833-4 - AEROSPACE SERIES - GLASS FIBER THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 4: UNIDIRECTIONAL GLASS/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 125 DEGREE C FOR CONTINUOUS USE UP TO 80 DEGREE C |
| PREN 2833-4 : 200P1 | AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 4: UNIDIRECTIONAL GLASS/EPOXY RESIN PREIMPREGNATE CURING AT UP TO 125 DEGREES C FOR CONTINUOUS USE UP TO 80 DEGREES C |
| I.S. EN 2850:2017 | AEROSPACE SERIES - CARBON FIBRE THERMOSETTING RESIN - UNIDIRECTIONAL LAMINATES - COMPRESSION TEST PARALLEL TO FIBRE DIRECTION |
| PREN 2379 : 200P1 | AEROSPACE SERIES - FLUIDS FOR ASSESSMENT OF NON-METALLIC MATERIALS |
| PREN 2743 : 200P1 | AEROSPACE SERIES - REINFORCED PLASTICS - STANDARD PROCEDURES FOR CONDITIONING PRIOR TO TESTING |
| EN 2744:1992 | Aerospace series - Non metallic materials - Preferred test temperatures |
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