49.025.40 - Rubber and plastics
ICS 49.025.40 Details
Rubber and plastics
Kunststoffe. Gummi
Caoutchouc et plastiques
Guma in polimerni materiali
General Information
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This document specifies methods for determining the resin content, fibre content and mass of fibre per unit area of fibre preimpregnates for aerospace use.
- Amendment4 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies methods for determining the resin content, fibre content and mass of fibre per unit area of fibre preimpregnates for aerospace use.
- Amendment4 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the required characteristics of loop style clamps ("P" type) in aluminium alloy with various cushion materials.
These clamps are used for supporting aerospace pipe assemblies and electrical cable bundles.
They are used up to 80 °C max.
Usage at a higher temperature is at the option of the user.
For temperature range and environmental considerations, see the various cushion material standards.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the required characteristics for heat-shrinkable limited fire hazard identification sleeves for use in aircraft electrical systems at operating temperatures between −30 °C and 105 °C.
This document is for the characterization of identification sleeves only. This sleeving is flexible, flame retarded and emits minimum smoke, gases and corrosive by-products when exposed to fire. It is suitable for use in areas where smoke, gases or corrosive by-products would constitute a particular hazard.
It is available with a shrink ratio of 2:1.
The product is normally supplied with internal diameters up to 51 mm.
The standard colours are white or yellow.
Sizes or colours other than those specifically listed in this document can be available. These items are considered to comply with this standard if they comply with the property requirements listed in Tables 2 and 3 except for dimensions and mass.
As the sleeving to be tested is a printed article, the complete system is to be recorded as part of the evaluation. The sleeve will only be considered as meeting the requirements of this specification if printed with the printer, ribbon, inks and settings referenced within the test report.
Mark adherence and print permanence are determined in this specification using method EN 6059-407.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This test method describes the principles applicable to infrared transmission spectrophotometric analysis of organic 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.
The method could also be applied to some inorganic products.
It is intended to be used jointly with special test conditions specified in the materials specification invoking the test.
This document does not give any directions necessary to meet the health and safety requirements. It is the responsibility of the user of this document to adopt appropriate health and safety precautions.
- Standard27 pagesEnglish languagesale 10% offe-Library read for1 day
This document lists the product standards, covered by technical specification EN 4708-001, for heat
shrinkable sleeves.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This test method describes the principles applicable to infrared transmission spectrophotometric analysis of organic 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.
The method could also be applied to some inorganic products.
It is intended to be used jointly with special test conditions specified in the materials specification invoking the test.
This document does not give any directions necessary to meet the health and safety requirements. It is the responsibility of the user of this document to adopt appropriate health and safety precautions.
- Standard27 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the required characteristics for heat-shrinkable polyolefin identification
sleeving for use in aircraft electrical systems at operating temperatures between −55 °C and 135 °C.
This specification is for the characterisation of identification sleeves only.
This sleeving is flexible and flame retarded, and is available with 2:1 and 3:1 shrink ratios.
The product is normally supplied with internal diameters up to 57 mm.
The standard colours are white or yellow.
Sizes or colours other than those specifically listed in this standard may be available. These items are
considered to comply with this document if they comply with the property requirements listed in tables 3
and 4 except for dimensions and mass.
As the sleeving to be tested is a printed article the complete system is to be recorded as part of the
evaluation. The sleeve will only be considered as meeting the requirements of this document if printed
with the printer, ribbon, inks, and settings referenced within the test report.
Mark adherence and print permanence are determined in this document using method EN 6059-407.
- Standard13 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the required characteristics for heat-shrinkable semi rigid polyvinylidene identification sleeves for use in aircraft electrical systems at operating temperatures between -55 °C and 225 °C.
This specification is for the characterisation of Identification sleeves only.
This sleeving is a semi rigid tough product and is suitable for use where high temperatures and extreme fluid resistance properties are required.
It is available with a shrink ratio of 2:1.
The product is normally supplied with internal diameters up to 38 mm
The standard colours are white, black or yellow
For use at temperatures above 200 °C black with white or silver ink is recommended
Sizes or colours other than those specifically listed in this standard may be available. These items shall be considered to comply with this document if they comply with the property requirements listed in tables 2 and 3 except for dimensions and mass.
As the sleeving to be tested is a printed article the complete system is to be recorded as part of the evaluation. The sleeve will only be considered as meeting the requirements of this specification if printed with the printer, ribbon/inks and settings referenced within the test report.
Mark adherence and print permanence are determined in this document using method EN 6059-407.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of self-extinguishing and low smoke emission semi-finished polycarbonate sheets with and without UV radiation protection requirement, as used for aircraft equipment, such as internal panelling, simple internal glazing, sound-proofing panels, light covers, etc.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of self-extinguishing and low smoke emission semi-finished polycarbonate sheets with and without UV radiation protection requirement, as used for aircraft equipment, such as internal panelling, simple internal glazing, sound-proofing panels, light covers, etc.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies methods for determining the resin content, fibre content and mass of fibre per unit area of fibre preimpregnates for aerospace use.
- Standard13 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies methods for determining the resin content, fibre content and mass of fibre per unit area of fibre preimpregnates for aerospace use.
- Standard13 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements of a thermoplastic composite stock shape material (e.g. tape,
rod etc.) consisting of polyetheretherketone with 55 % continuous glass fibres by volume (PEEK–GF55)
for aerospace applications, which is presupposed to be used in a further thermal moulding process for
forming parts described in EN 4714 1).
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements of a thermoplastic composite stock shape material (e.g. tape,
rod, etc.) consisting of polyetheretherketone with 55 % continuous carbon fibres by volume (PEEK–
CF55) for aerospace applications, which is presupposed to be used in a further thermal moulding
process for forming parts described in EN 4714 1).
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements of a thermoplastic composite stock shape material (e.g. tape,
rod etc.) consisting of polyetheretherketone with 55 % continuous glass fibres by volume (PEEK–GF55)
for aerospace applications, which is presupposed to be used in a further thermal moulding process for
forming parts described in EN 4714 1).
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements of a thermoplastic composite stock shape material (e.g. tape,
rod, etc.) consisting of polyetheretherketone with 55 % continuous carbon fibres by volume (PEEK–
CF55) for aerospace applications, which is presupposed to be used in a further thermal moulding
process for forming parts described in EN 4714 1).
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This document defines the requirements of ethylene propylene elastomer (EPM/EPDM) for seal elements for use as static seals in hydraulic systems using phosphate ester fluids, hardness 80 IRHD (International Rubber Hardness Degree) for long term application for aerospace application.
Unless otherwise specified in the drawing, order or inspection schedule, this document shall be used in conjunction with the referenced documents.
Applicable temperature range:
- Continuous service: −55 °C to 107 °C
- Intermittent service: −55 °C to 120 °C
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This document defines the requirements of ethylene propylene elastomer (EPM/EPDM) for seal elements for use as static seals in hydraulic systems using phosphate ester fluids, hardness 80 IRHD (International Rubber Hardness Degree) for long term application for aerospace application.
Unless otherwise specified in the drawing, order or inspection schedule, this document shall be used in conjunction with the referenced documents.
Applicable temperature range:
- Continuous service: −55 °C to 107 °C
- Intermittent service: −55 °C to 120 °C
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the required characteristics for heat-shrinkable elastomeric semi-rigid, boots for use in aircraft electrical systems at operating temperatures between -75 °C and 150 ° C. The moulded shapes may be supplied with a pre-coated adhesive. Refer to the manufacturers/suppliers for options. A guide to adhesive compatibility is given in Annex A (informative). These moulded shapes are normally supplied in the styles and dimensions given in EN 4840-002 Table 1 to Table 22. The colour is normally black. Styles and dimensions other than those specifically listed in EN 4840-002 Table 1 to Table 22 may be available as custom items. These items shall be considered to comply with this standard if they comply with the property requirements listed in Table 1 with the exception of dimensions.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the properties of fluorocarbon rubber (FKM)1), hardness 90 IRHD, for aerospace applications.
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the properties of fluorocarbon rubber (FKM)1), hardness 80 IRHD, for aerospace
applications.
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the properties of fluorocarbon rubber (FKM) ), low compression set, hardness 80 IRHD, for aerospace applications.
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the properties of fluorocarbon rubber (FKM)1), hardness 70 IRHD, for aerospace
applications.
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This standard specifies the required characteristics for a heat-shrinkable, polytetrafluoroethylene sleeving for use in aircraft electrical systems at operating temperatures between ? 65 °C and 260 °C. This sleeving is basically translucent. It is semi-rigid, and suitable for use where resistance to chemicals and high temperature performance are required. It is flame resistant and available in low and high shrink ratios. Type A Low Shrink Ratio; Type B High Shrink Ratio .
- Standard12 pagesEnglish languagesale 10% offe-Library read for1 day
This standard specifies the required characteristics for four types of heat-shrinkable limited fire hazard sleevings for use in aircraft electrical systems at operating temperatures between - 65 °C and 150 °C. This sleeving is flexible, flame retarded and emits minimum smoke, gases and corrosive by-products when exposed to fire. It is available with various wall thicknesses and also in a higher shrink ratio according to the application and degree of mechanical protection required. It is suitable for use (e.g. as cable protection) in areas where smoke, gases or corrosive by-products would constitute a particular hazard. Type A: Medium wall, shrink ratio 2:1 and is normally supplied with internal diameters up to 30 mm. The standard colour is black. Sizes or colours other than those specifically listed in this document may be available. These items shall be considered to comply with this document if they comply with the property requirements listed in Table 2 except for dimensions and mass.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the required characteristics for a heat-shrinkable, semi-flexible polyvinylidene sleeving for use in aircraft electrical systems at operating temperatures between − 55 °C and 150 °C. This sleeving is basically transparent, but may be tinted. It is semi-flexible tough and abrasion resistant, and is suitable for use where strain relief and mechanical protection are required, or where their transparent properties are desirable. It is not suitable for use where contamination from phosphate ester based hydraulic fluid is possible. These sleevings are normally supplied with internal diameters up to 25,4 mm for shrink ratios of 2:1. Sizes other than those specifically listed in this standard may be available. These items shall be considered to comply with this standard if they comply with the property requirements listed in Tables 2, 3 and 4 except for dimensions and mass.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the required characteristics, test methods, qualification and production routine testing of Heat shrinkable sleeving for binding, insulation and identification.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the properties of fluorocarbon rubber (FKM)1), hardness 80 IRHD, for aerospace
applications.
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the properties of fluorocarbon rubber (FKM) ), low compression set, hardness 80 IRHD, for aerospace applications.
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the properties of fluorocarbon rubber (FKM)1), hardness 90 IRHD, for aerospace
applications.
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the required characteristics for two types a heat-shrinkable, fluoroelastomer sleeving for use in aircraft electrical systems at operating temperatures between -55 °C and 200 °C.
Type A Thick wall
Type B Thin wall
This sleeving has good flexibility, is flame retarded and has a thick wall for mechanical protection. It is for use in areas subject to prolonged contamination by aircraft fuel and fluids with the exception of phosphate ester-based hydraulic fluids. The standard colour is black.
These sleevings are normally supplied with internal diameters up to 50 mm for shrink ratios of 2:1. They are available in black only.
Sizes other than those specifically listed in this standard may be available. These items shall be considered to comply with this standard if they comply with the property requirements listed in Tables 2, 3 and 4 except for dimensions and mass.
- Standard12 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the properties of fluorocarbon rubber (FKM)1), hardness 70 IRHD, for aerospace
applications.
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the methods for determining the fibre content by volume and mass and, by correlation, the resin content by volume and mass and void content by volume, of carbon fibre laminates, for aerospace applications.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the properties of fluorocarbon rubber (FKM) 1), low compression set, hardness 60 IRHD, for aerospace applications.
1) Symbol as per ISO 1629.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the properties of fluorocarbon rubber (FKM) ), low compression set, hardness 90 IRHD, for aerospace applications.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day
This document defines tests on the susceptibility to corrosion in a damp atmosphere of metals in contact with vulcanized rubbers.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the methods for determining the fibre content by volume and mass and, by correlation, the resin content by volume and mass and void content by volume, of carbon fibre laminates, for aerospace applications.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the required characteristics for heat-shrinkable polyolefin semi-rigid, limited fire hazard heat-shrinkable boots for use in aircraft electrical systems at operating temperatures between - 30 °C and 105 °C.
The moulded shapes may be supplied with a pre-coated adhesive. Refer to the manufacturers/suppliers for options. A guide to adhesive compatibility is given in Annex A.
These moulded shapes are normally supplied in the styles and dimensions given in EN 4840-002 Tables 1 to 22. The colour is normally black.
Styles and dimensions other than those specifically listed in EN 4840-002 Tables 1 to 22 may be available as custom items. These items shall be considered to comply with this standard if they comply with the property requirements listed in Table 1 with the exception of dimensions.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the properties of fluorocarbon rubber (FKM) ), low compression set, hardness 50 IRHD, for aerospace applications.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day
This European standard specifies the required characteristics, test methods, qualification and production
routine testing of heat shrinkable moulded shapes.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the properties of fluorocarbon rubber (FKM)1), low compression set,
hardness 60 IRHD, for aerospace applications.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the properties of fluorocarbon rubber (FKM)1), low compression set,
hardness 90 IRHD, for aerospace applications.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day
This document defines tests on the susceptibility to corrosion in a damp atmosphere of metals in
contact with vulcanized rubbers.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard defines a method for the determination of stress at failure and Young's modulus in compression of carbon thermosetting resin unidirectional laminates.
The method only covers test pieces the axis of which is parallel to the fibre direction.
This method covers fibres (or fabrics) other than carbon, when the relevant technical specification explicitly mentions it.
- Standard16 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the properties of fluorocarbon rubber (FKM)1), low compression set, hardness
50 IRHD, for aerospace applications.
- Standard6 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard defines a method for the determination of stress at failure and Young's modulus
in compression of carbon thermosetting resin unidirectional laminates.
The method only covers test pieces the axis of which is parallel to the fibre direction.
This method covers fibres (or fabrics) other than carbon, when the relevant technical specification
explicitly mentions it.
- Standard16 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the method for determining the effect of exposure to a humid atmosphere on the physical and mechanical characteristics of fibre reinforced plastics.
This standard applies to all laminates, whatever the nature of the reinforcement and organic matrix used, unless otherwise indicated in the material standard and/or technical specification.
- Standard12 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the method for determining the effect of exposure to a humid
atmosphere on the physical and mechanical characteristics of fibre reinforced plastics.
This standard applies to all laminates, whatever the nature of the reinforcement and organic matrix used,
unless otherwise indicated in the material standard and/or technical specification.
- Standard12 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard defines the procedure to be used to determine the bearing strength of fibre composites with multidirectional reinforcement. This standard is applicable to composite laminates manufactured from unidirectional tape or woven fabric reinforcement.
This standard does not give any directions necessary to meet health and safety requirements. It is the responsibility of the user of this standard to consult and establish appropriate health and safety precautions.
- Standard13 pagesEnglish languagesale 10% offe-Library read for1 day