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PREN 6064 : 200P1

Withdrawn
Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

AEROSPACE SERIES - NON-METALLIC MATERIALS - ANALYSIS OF NON-METALLIC MATERIALS (CURED) FOR THE DETERMINATION OF THE EXTENT OF CURE BY DIFFERENTIAL SCANNING CALORIMETRY (DSC)
Available format(s)

Hardcopy , PDF

Withdrawn date

21-12-2023

Language(s)

English

1 Scope
2 Normative references
3 Definitions
4 Principle of the method
5 Designation of the method
6 Apparatus
7 Test Specimen
8 Procedure
9 Presentation of the results
10 Test report
Annex A - Equipment

Covers the procedure for the estimation of the extent of cure of certain non-metallic materials (e.g. adhesives, preimpregnated and neat resin systems) for aerospace use. The extent of cure is estimated by Differential Scanning Calorimetry (DSC) measurements of uncured (reference) and cured materials. Extra evidence on the extent of cure may be gained by combining results from this method with those obtained by other techniques.

Committee
AIB/TF6
DocumentType
Draft
Pages
10
ProductNote
Superseded by DIN EN 6064(2018-03)
PublisherName
Aerospace & Defence Industries Association of Europe
Status
Withdrawn

Standards Relationship
NF EN 6064 : 2017 PR Identical

SAE AMS 2950/1 : 2008 PASTE ADHESIVE FOR CORE RESTORATION - PART 1: GENERAL REQUIREMENTS
BS EN 4106:2013 Aerospace series. Non-metallic materials. Structural adhesive systems. Paste adhesive. Technical specification
PREN 4106 : 200P1 AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION
UNI EN 4106 : 2014 AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION
SAE AMS 3970/1 : 2011 CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 1 - GENERAL REQUIREMENTS
EN 4106:2013 Aerospace series - Non-metallic materials - Structural adhesive systems - Paste adhesive - Technical specification
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]
I.S. EN 4106:2013 AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION
SAE AMS 2950/1 : 2008(R2019) PASTE ADHESIVE FOR CORE RESTORATION - PART 1: GENERAL REQUIREMENTS

PREN 2743 : 200P1 AEROSPACE SERIES - REINFORCED PLASTICS - STANDARD PROCEDURES FOR CONDITIONING PRIOR TO TESTING
PREN 2559 : 1988 CARBON FIBRE PREIMPREGNATES - TEST METHOD FOR THE DETERMINATION OF THE RESIN AND FIBRE CONTENT AND THE MASS OF FIBRE PER UNIT AREA
EN 2331 : 1993 AEROSPACE SERIES - TEXTILE GLASS FIBRE PREIMPREGNATES - TEST METHOD FOR THE DETERMINATION OF THE RESIN AND FIBRE CONTENT AND MASS OF FIBRE PER UNIT AREA

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