DIN 65074:1999-03
Current
The latest, up-to-date edition.
AEROSPACE - ADHESIVE FILMS AND PRIMERS FOR STRUCTURAL ASSEMBLIES - TECHNICAL SPECIFICATION
Hardcopy , PDF
German
01-01-1999
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Vorwort
1 Anwendungsbereich
2 Normative Verweisungen
3 Definitionen
3.1 Klebfolie
3.2 Träger
3.3 Haftgrundmittel (Primer)
3.4 Inhibitor
3.5 Klebstoffsystem
3.6 Fertigungslos
3.7 Qualitätsprüfung
3.7.1 Qualifikationsprüfung
3.7.2 Abnahmeprüfung
4 Formelzeichen und Einheiten
5 Anforderungen
5.1 Werkstoffe
5.1.1 Klebfolien
5.1.2 Haftgrundmittel
5.2 Masse, Massen
5.3 Fehler
5.3.1 Klebfolien
5.3.2 Haftgrundmittel
6 Qualitätsprüfung
6.1 Qualifikationsprüfung
6.1.1 Prüfungen im ungehärteten Zustand
6.1.2 Prüfungen im gehärteten Zustand
6.2 Abnahmeprüfung
6.2.1 Probenahme
6.2.2 Prüfungen
6.2.3 Abnahmeprüfzeugnis
7 Lieferart
7.1 Aufmachung und Verpackung
7.1.1 Klebfolien
7.1.2 Haftgrundmittel
7.2 Kennzeichnung
7.2.1 Klebfolien
7.2.2 Haftgrundmittel
7.2.3 Sicherheitstechnische Angaben
8 Lagerung
Anhang A (normativ) Abnahmeprüfzeugnis 3.1.B (Muster)
für Klebfolien
Anhang B (normativ) Abnahmeprüfzeugnis 3.1.B (Muster)
für Haftgrundmittel
Diese Norm ist anzuwenden für Klebfolien und Haftgrundmittel, die zur Herstellung tragender Strukturen aus metallischen Fügeteilen verwendet werden.
| DocumentType |
Standard
|
| Pages |
33
|
| PublisherName |
German Institute for Standardisation (Deutsches Institut für Normung)
|
| Status |
Current
|
| Supersedes |
| DIN 29978:1994-12 | AEROSPACE - HONEYCOMB CORES, HEXAGONAL EXPANDED, IN WROUGHT ALUMINIUM ALLOY, CORROSION PROTECTED, UNPERFORATED OR PERFORATED - TECHNICAL SPECIFICATION |
| DIN 50021:1988-06 | SPRAY TESTS WITH DIFFERENT SODIUM CHLORIDE SOLUTIONS |
| WL 5.4201 : 1998 | AEROSPACE SERIES - WASH PRIMERS FOR STRUCTURAL ADHESIVES ACCORDING TO 5.4101 PART 2 |
| DIN 54456:2006-01 | TESTING OF STRUCTURAL ADHESIVES; TEST OF RESISTANCE TO CLIMATIC CONDITIONS |
| WL 5.4110 : 1998 | AEROSPACE SERIES - STRUCTURAL ADHESIVE FILMS ON A MODIFIED EP BASIS - STANDARD CURING TEMPERATURE 125 C, APPLICABLE FROM - 55 DEGREE C TO 80 DEGREE C |
| LN 29975:1998-08 | Aerospace - Honeycomb cores, hexagonal expanded, in wrought aluminium alloy 5052, corrosion protected, unperforated or perforated - Dimensions, masses |
| WL 5.4111 : 1998 | AEROSPACE - STRUCTURAL ADHESIVE FILMS ON A MODIFIED EP BASIS - STANDARD CURING TEMPERATURE 175 DEGREES C, APPLICABLE FROM -55 DEGREES C TO 135 DEGREES C |
| WL 5.4211 : 1998 | AEROSPACE - PRIMER FOR STRUCTURAL ADHESIVE FILMS IN ACCORDANCE WITH WL 5.4111 - APPLICABLE FROM -55 DEGREE C TO 135 DEGREE C |
| DIN EN 2243-2:2006-10 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - TEST METHOD - PART 2: PEEL METAL-METAL |
| WL 5.4100-1 : 1998 | AEROSPACE SERIES - STRUCTURAL ADHESIVE FOR LONG-TERM UTILIZATION FROM -55 TO +80 DEGREES C |
| DIN EN 2558:1997-03 | AEROSPACE SERIES - CARBON FIBRE PREIMPREGNATES - DETERMINATION OF THE VOLATILE CONTENT |
| WL 5.4100-2 : 1998 | AEROSPACE SERIES - STRUCTURAL ADHESIVE FOR LONG-TERM UTILIZATION FROM -55 TO +80 DEGREES C - PROPERTIES IN THE TEST SPECIMEN - PROPERTIES IN THE TEST SPECIMEN |
| WL 5.4210 : 1998 | AEROSPACE SERIES - PRIMER FOR STRUCTURAL ADHESIVE FILMS IN ACCORDANCE WITH WL 5.4110 - APPLICABLE FROM -55 DEGREE C TO 80 DEGREE C |
| WL 5.4101-2 : 1998 | AEROSPACE SERIES - STRUCTURAL ADHESIVE FOR LONG-TERM UTILIZATION FROM -55 TO +135 DEGREES C - PROPERTIES IN THE TEST SPECIMEN |
| WL 3.1364-1 : 1987 | AEROSPACE; WROUGHT ALUMINIUM ALLOY WITH APPROX. 4,4CU-1,5MG-0,6MN; CLAD SHEET, STRIP AND PLATE |
| DIN EN 2781:1998-08 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - TEST METHODS - DETERMINATION OF THE PRIMER THICKNESS |
| DIN EN 2243-3:2006-10 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - TEST METHOD - PART 3: PEELING TEST METAL-HONEYCOMB CORE |
| ISO 2555:1989 | Plastics Resins in the liquid state or as emulsions or dispersions Determination of apparent viscosity by the Brookfield Test method |
| WL 5.4250 : 1998 | AEROSPACE - PRIMERS, INHIBITING CORROSION, FOR STRUCTURAL ADHESIVES ACCORDING TO 5.4100 PART 2 |
| DIN EN 10204:2005-01 | Metallic products - Types of inspection documents; German version EN 10204:2004 |
| WL 5.4200 : 1998 | AEROSPACE SERIES - WASH PRIMERS FOR STRUCTURAL ADHESIVES ACCORDING TO 5.4100 PART 2 |
| WL 5.4101-1 : 1998 | AEROSPACE SERIES - STRUCTURAL ADHESIVE FOR LONG-TERM UTILIZATION FROM -55 TO +135 DEGREES C |
| DIN EN 12701:2001-12 | STRUCTURAL ADHESIVES - STORAGE - DETERMINATION OF WORDS AND PHRASES RELATING TO THE PRODUCT LIFE OF STRUCTURAL ADHESIVES AND RELATED MATERIALS |
| DIN EN 2243-4:2006-10 | AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVES - TEST METHOD - PART 4: METAL-HONEYCOMB CORE FLATWISE TENSILE TEST |
| DIN EN 2757:2011-08 | Aerospace series - Structural adhesives system - Test method - Determination of the drying and ignition residues of primers; German and English version EN 2757:2011 |
| DIN 50014:1985-07 | CLIMATES AND THEIR TECHNICAL APPLICATION; STANDARD ATMOSPHERES |
| DIN 53213-1:1978-04 | TESTING OF PAINTS, VARNISHES AND SIMILAR PRODUCTS CONTAINING SOLVENTS - FLASHPOINT TEST USING CLOSED CUP, DETERMINATION OF FLASHPOINT |
| DIN 65467:1999-03 | |
| DIN EN 3665:1997-08 | AEROSPACE SERIES - TEST METHODS FOR PAINTS AND VARNISHES - FILIFORM CORROSION RESISTANCE TEST ON ALUMINIUM ALLOYS |
| DIN 54451:1978-11 | TESTING OF ADHESIVES FOR METALS AND BONDED METAL JOINTS; TENSILE SHEAR TEST FOR THE DETERMINATION OF THE SHEAR STRESS-STRAIN DIAGRAM OF AN ADHESIVE IN A BONDED JOINT |
| ISO 1817:2015 | Rubber, vulcanized or thermoplastic Determination of the effect of liquids |
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