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ASD-STAN
PREN 6042 : 200P1

PREN 6042 : 200P1

Current

Current

The latest, up-to-date edition.

AEROSPACE SERIES - ORGANIC COMPOUNDS - TEST METHOD - ANALYSIS BY INFRARED SPECTROSCOPY

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

30-11-1995

Publisher

Aerospace & Defence Industries Association of Europe

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 - Pellitization
Annex B - Deposit on a plate
Annex C - Deposit between two plates
Annex D - Dissolution and pellitization (Dispas)
Annex E - Total dissolution (Distot)
Annex F - Liquid cell
Annex G - Gas cell

Describes the principles applicable to infrared transmission spectrophotometric analysis of origin compounds (elastomers, basic, resins, resin mixes or resin systems) used as the matrix in reinforced polymers, adhesives, bonding primers and, in general terms, all organic compounds.

DocumentType
Draft
Pages
20
PublisherName
Aerospace & Defence Industries Association of Europe
Status
Current

Standards Relationship
DIN EN 6042:1996-04 (Draft) Identical

PREN 4689 : 200P1 AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENTS COLD CURING POLYURETHANE FINISH - HIGH FLEXIBILITY AND CHEMICAL AGENT RESISTANCE FOR MILITARY APPLICATION
PREN 6085 : 200P1 AEROSPACE SERIES - NON-METALLIC MATERIALS - EPOXY SURFACING FILMS
BS EN 4689:2012 Aerospace series. Paints and varnishes. Two components cold curing polyurethane finish. High flexibility and chemical agent resistance for military application
BS EN 4106:2013 Aerospace series. Non-metallic materials. Structural adhesive systems. Paste adhesive. Technical specification
UNI EN 4689 : 2013 AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENTS COLD CURING POLYURETHANE FINISH - HIGH FLEXIBILITY AND CHEMICAL AGENT RESISTANCE FOR MILITARY APPLICATION
EN 4689:2012 Aerospace series - Paints and varnishes - Two components cold curing polyurethane finish - High flexibility and chemical agent resistance for military application
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 AMS 3970/3 : 2011 CARBON FIBER FABRIC REPAIR PREPREG, 120 DEGREES C (250 DEGREES F) VACUUM CURING - PART 3: PURCHASING SPECIFICATION FOR CARBON PREPREG
PREN 2833-1 : 200P2 AEROSPACE SERIES - GLASS FIBRE THERMOSETTING PREIMPREGNATES - TECHNICAL SPECIFICATION - PART 1: GENERAL REQUIREMENTS
PREN 2434-05 : 200P1 AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENT COLD CURING POLYURETHANE FINISH - PART 05: HIGH FLEXIBILITY AND CHEMICAL AGENT RESISTANCE FOR MILITARY APPLICATION
PREN 6044-1 : 200P1 AEROSPACE SERIES - CARBON FIBRE REINFORCED EPOXY PREPREG - TECHNICAL SPECIFICATION - GENERAL REQUIREMENTS
PREN 4106 : 200P1 AEROSPACE SERIES - NON-METALLIC MATERIALS - STRUCTURAL ADHESIVE SYSTEMS - PASTE ADHESIVE - TECHNICAL SPECIFICATION
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
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
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
17/30371344 DC : 0 BS EN 4689 - AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENTS COLD CURING POLYURETHANE FINISH - HIGH FLEXIBILITY AND CHEMICAL AGENT RESISTANCE FOR MILITARY APPLICATION
EN 2434-005:2006 Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 005: High flexibility and chemical agent resistance for military application
EN 4106:2013 Aerospace series - Non-metallic materials - Structural adhesive systems - Paste adhesive - Technical specification
I.S. EN 4689:2012 AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENTS COLD CURING POLYURETHANE FINISH - HIGH FLEXIBILITY AND CHEMICAL AGENT RESISTANCE FOR MILITARY APPLICATION
SAE AMS 2950/1 : 2008 PASTE ADHESIVE FOR CORE RESTORATION - PART 1: GENERAL REQUIREMENTS
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
BS EN 2434-005 : 2006 AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENT COLD CURING POLYURETHANE FINISH - PART 005: HIGH FLEXIBILITY AND CHEMICAL AGENT RESISTANCE FOR MILITARY APPLICATION

EN 2743:2001 Aerospace series - Fibre reinforced plastics - Standard procedures for conditioning prior to testing unaged materials

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Hardcopy - English
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