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).

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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).

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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

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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.

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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.

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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 .

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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.

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This document specifies the required characteristics, test methods, qualification and production routine testing of Heat shrinkable sleeving for binding, insulation and identification.

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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.

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This European Standard specifies the properties of fluorocarbon rubber (FKM) ), low compression set, hardness 80 IRHD, for aerospace applications.

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This document specifies the properties of fluorocarbon rubber (FKM)1), hardness 70 IRHD, for aerospace
applications.

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This document specifies the properties of fluorocarbon rubber (FKM)1), hardness 80 IRHD, for aerospace
applications.

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This document specifies the properties of fluorocarbon rubber (FKM)1), hardness 90 IRHD, for aerospace
applications.

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This European Standard specifies the properties of fluorocarbon rubber (FKM) ), low compression set, hardness 80 IRHD, for aerospace applications.

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This document specifies the properties of fluorocarbon rubber (FKM)1), hardness 90 IRHD, for aerospace applications.

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This document specifies the properties of fluorocarbon rubber (FKM)1), hardness 80 IRHD, for aerospace
applications.

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This document specifies the properties of fluorocarbon rubber (FKM)1), hardness 70 IRHD, for aerospace
applications.

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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.

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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.

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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.

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This European standard specifies the required characteristics, test methods, qualification and production
routine testing of heat shrinkable moulded shapes.

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This European Standard specifies the properties of fluorocarbon rubber (FKM)1), low compression set,
hardness 90 IRHD, for aerospace applications.

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This European Standard specifies the properties of fluorocarbon rubber (FKM)1), low compression set,
hardness 60 IRHD, for aerospace applications.

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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.

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This European Standard specifies the properties of fluorocarbon rubber (FKM) ), low compression set, hardness 90 IRHD, for aerospace applications.

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This document defines tests on the susceptibility to corrosion in a damp atmosphere of metals in
contact with vulcanized rubbers.

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This document defines tests on the susceptibility to corrosion in a damp atmosphere of metals in contact with vulcanized rubbers.

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This document specifies the properties of fluorocarbon rubber (FKM)1), low compression set, hardness
50 IRHD, for aerospace applications.

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This document specifies the properties of fluorocarbon rubber (FKM) ), low compression set, hardness 50 IRHD, for aerospace applications.

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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.

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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.

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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.

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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.

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This standard specifies the procedure to determine the mode II interlaminar fracture toughness energy GIIC of carbon fibre composites manufactured from unidirectional tape or woven fabric.
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.

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This standard specifies the procedure to determine the mode I interlaminar fracture toughness energy GIC of carbon fibre composites manufactured from unidirectional tape or woven fabric.
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.

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This standard defines a method to be used to determine the compression strength of notched, unnotched and filled hole fibre reinforced plastics.
It is applicable to composite laminates with unidirectional layers or woven fabric reinforcement.
This standard does not give any direction 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.

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This standard defines a method to be used to determine the tensile strength of notched and unnotched fibre reinforced plastics.
It is applicable to composite laminates with unidirectional plies or woven fabrics reinforcement.
This standard does not give any direction 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.

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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.

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This European Standard specifies the procedure for the determination of the in-plane shear strength
and modulus of fibre composites. The procedure is based on the uni-axial tensile stress-strain response
of a ± 45° laminate which is symmetrically laminated about the mid-plane.
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 the health and safety requirements. It is
the responsibility of the user of this standard to consult and establish appropriate health and safety
precautions.

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This standard specifies a method to determine the apparent glass transition temperatures of non-metallic materials.
This standard is applicable to unidirectional tape and woven fabric reinforced plastic or plastic materials like adhesive or neat resin for comparison of the influence on the glass transition temperature resulting from processing-parameters of non-metallic parts, for compatibility tests for checking co-curing effects of different prepreg types or with adhesive.
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.

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This European Standard defines a method to be used to measure the low speed impact resistance
characteristics of fibre reinforced plastics.
It is applicable to composite laminates with unidirectional plies or woven fabric reinforcement.
This standard does not give any direction 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.

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This standard specifies a method to determine the apparent glass transition temperatures of non-metallic materials.
This standard is applicable to unidirectional tape and woven fabric reinforced plastic or plastic materials like adhesive or neat resin for comparison of the influence on the glass transition temperature resulting from processing-parameters of non-metallic parts, for compatibility tests for checking co-curing effects of different prepreg types or with adhesive.
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.

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This standard specifies the procedure to determine the mode I interlaminar fracture toughness energy GIC of carbon fibre composites manufactured from unidirectional tape or woven fabric.
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.

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This European Standard defines a method to be used to measure the low speed impact resistance characteristics of fibre reinforced plastics.
It is applicable to composite laminates with unidirectional plies or woven fabric reinforcement.
This standard does not give any direction 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.

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This standard specifies the procedure to determine the mode II interlaminar fracture toughness energy GIIC of carbon fibre composites manufactured from unidirectional tape or woven fabric.
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.

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This European Standard specifies the procedure for the determination of the in-plane shear strength and modulus of fibre composites. The procedure is based on the uni-axial tensile stress-strain response of a  45° laminate which is symmetrically laminated about the mid-plane.
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 the health and safety requirements. It is the responsibility of the user of this standard to consult and establish appropriate health and safety precautions.

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This standard defines a method to be used to determine the compression strength of notched, unnotched and filled hole fibre reinforced plastics.
It is applicable to composite laminates with unidirectional layers or woven fabric reinforcement.
This standard does not give any direction 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.

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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.

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This standard defines a method to be used to determine the tensile strength of notched and unnotched fibre reinforced plastics.
It is applicable to composite laminates with unidirectional plies or woven fabrics reinforcement.
This standard does not give any direction 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.

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This standard specifies the properties of fluorosilicone rubber (FVMQ)1), hardness 80 IRHD, for aerospace
applications.

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