49.060 - Aerospace electric equipment and systems
ICS 49.060 Details
Aerospace electric equipment and systems
Elektrische Anlagen. Flugzeugbordnetze
Équipement et systemes électriques aérospatiaux
Letalska in vesoljska električna oprema in sistemi
General Information
Frequently Asked Questions
ICS 49.060 is a classification code in the International Classification for Standards (ICS) system. It covers "Aerospace electric equipment and systems". The ICS is a hierarchical classification system used to organize international, regional, and national standards, facilitating the search and identification of standards across different fields.
There are 3207 standards classified under ICS 49.060 (Aerospace electric equipment and systems). These standards are published by international and regional standardization bodies including ISO, IEC, CEN, CENELEC, and ETSI.
The International Classification for Standards (ICS) is a hierarchical classification system maintained by ISO to organize standards and related documents. It uses a three-level structure with field (2 digits), group (3 digits), and sub-group (2 digits) codes. The ICS helps users find standards by subject area and enables statistical analysis of standards development activities.
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This document specifies a method for the high temperature exposure of protection sleeves for electrical cable and cable bundles for aerospace applications.
It is used together with EN 6059-100.
- Standard5 pagesEnglish languagee-Library read for1 day
This document specifies methods for measuring the transfer impedance of a cable.
It is intended to be used together with EN 3475-100 and IEC 62153-4-3.
- Standard5 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of close tolerance pins, swage locking, 100° countersunk reduced head, shear type, in aluminium alloy 7050-T73 with chemical film, inch series, with a maximum operating temperature of 80 °C for aerospace application.
- Standard10 pagesEnglish languagee-Library read for1 day
This document specifies a method of testing the fire resistance of "fire-proof" electrical cables.
- Standard14 pagesEnglish languagee-Library read for1 day
This document specifies methods for measuring the structural return loss of symmetrical cables for digital data transmission.
It is applicable together with EN 3475-100 and EN 50289-1-11. Attention is drawn in particular to correction procedures detailed in EN 50289-1-11:2016, Annex B, to minimize negative effects of cable preparation in the purpose of high frequency range measurements.
- Standard5 pagesEnglish languagee-Library read for1 day
This document specifies a method of testing the fire resistance of "fire-proof" electrical cables.
- Standard14 pagesEnglish languagee-Library read for1 day
This document specifies methods for measuring the transfer impedance of a cable.
It is intended to be used together with EN 3475-100 and IEC 62153-4-3.
- Standard5 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of close tolerance pins, swage locking, 100° countersunk reduced head, shear type, in aluminium alloy 7050-T73 with chemical film, inch series, with a maximum operating temperature of 80 °C for aerospace application.
- Standard10 pagesEnglish languagee-Library read for1 day
This document specifies methods for measuring the structural return loss of symmetrical cables for digital data transmission.
It is applicable together with EN 3475-100 and EN 50289-1-11. Attention is drawn in particular to correction procedures detailed in EN 50289-1-11:2016, Annex B, to minimize negative effects of cable preparation in the purpose of high frequency range measurements.
- Standard5 pagesEnglish languagee-Library read for1 day
This document specifies a method of determining the attenuation variation of an optical cable during mechanical bending under load at the maximum and minimum operating temperatures.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies a method for the high temperature exposure of protection sleeves for electrical cable and cable bundles for aerospace applications.
It is used together with EN 6059 100.
- Standard5 pagesEnglish languagee-Library read for1 day
This document specifies a method of determining the attenuation variation of an optical cable during mechanical bending under load at the maximum and minimum operating temperatures.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the required characteristics, tests and tooling applicable to male electrical contacts, type A, crimp, class S, used in elements of connection according to EN 3155 002.
It is used together with EN 3155 001.
The tests as applied in this document do not permit the full qualification and are expected to be completed with associated components.
- Standard16 pagesEnglish languagee-Library read for1 day
This document specifies the required characteristics, tests and tooling applicable to male electrical contacts 004, type A, crimp, class T, used in elements of connection according to EN 3155 002.
It is used together with EN 3155 001.
The associated female contacts are specified in EN 3155 005.
The contacts specified by this document are applicable for connector classes specified in EN 2997 series.
This document specifies two contact types (M and H) depending on connector class.
- Standard19 pagesEnglish languagee-Library read for1 day
This document specifies the required characteristics of a coaxial cable, 50 Ω, type WD, for use in aircraft electrical systems at operating temperature between -55 °C and 200 °C and specially for high frequency up to 6 GHz. Nevertheless, if needed, −65 °C is also acceptable as shown by thermal stability test.
- Standard17 pagesEnglish languagee-Library read for1 day
This document specifies the required characteristics of coaxial cables, 50 Ω, type WM, for use in aircraft electrical systems at operating temperatures between −55 °C and 200 °C and specially for high frequency up to 6 GHz.
The document encloses also a reinforced cable version (code R) which is used for sensitive systems with controlled VSWR.
- Standard18 pagesEnglish languagee-Library read for1 day
This document specifies the required characteristics and tests applicable to female electrical contacts 005, type A, crimp, class T, used in elements of connection according to EN 3155-002.
It is used together with EN 3155-001.
The associated male contacts are specified in EN 3155-004.
The contacts specified by this document are applicable for connector classes specified in EN 2997 series.
This document specifies two contact types (F and H) depending on connector class.
- Standard20 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of post installation flexible self-wrapping fire protection sleeves for electrical cable and cable bundles, providing 360° fire protection to electrical harnesses. The sleeve assembly gives fire resistance protection to the internal electrical harness against fire for five minutes and ensures that the electrical characteristics of cables will not be degraded.
- Standard12 pagesEnglish languagee-Library read for1 day
This document specifies the required characteristics of coaxial cables, 50 Ω, type WN, for use in aircraft electrical systems at operating temperatures between −55 °C and 200 °C and specially for high frequency up to 6 GHz.
The document encloses also a reinforced cable version (code R) which is used for sensitive systems with controlled VSWR.
- Standard19 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of UV laser printable coaxial cables, 50 Ω, type WZ, for use in aircraft electrical systems at operating temperatures between −65 °C and 200 °C and specially for high frequency up to 6 GHz.
The document encloses also a reinforced cable version (code R) which is used for sensitive systems with controlled VSWR.
- Standard19 pagesEnglish languagee-Library read for1 day
This document specifies the list of product standards and common characteristics of electrical cables for use in the on-board electrical systems of aircraft at operating temperatures between -55 °C and 260 °C (except otherwise specified in product standards).
- Standard12 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of UV laser printable DR family, single and multicore screened (spiral) and jacketed electrical lightweight cables for use in the on-board electrical systems of aircraft, at operating temperatures between −55 °C and 260 °C. Nevertheless, if needed, −65 °C is also acceptable as shown by cold test.
It is also possible to mark these cables by qualified compatible marking.
These markings are compliant with EN 3838.
- Standard14 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of UV laser printable DR family, single and multicore screened (spiral) and jacketed electrical lightweight cables for use in the on-board electrical systems of aircraft, at operating temperatures between −55 °C and 260 °C. Nevertheless, if needed, −65 °C is also acceptable as shown by cold test.
It is also possible to mark these cables by qualified compatible marking.
These markings are compliant with EN 3838.
- Standard14 pagesEnglish languagee-Library read for1 day
This document specifies the list of product standards and common characteristics of electrical cables for use in the on-board electrical systems of aircraft at operating temperatures between -55 °C and 260 °C (except otherwise specified in product standards).
- Standard12 pagesEnglish languagee-Library read for1 day
This document specifies the required characteristics of coaxial cables, 50 Ω, type WM, for use in aircraft electrical systems at operating temperatures between −55 °C and 200 °C and specially for high frequency up to 6 GHz.
The document encloses also a reinforced cable version (code R) which is used for sensitive systems with controlled VSWR.
- Standard18 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of UV laser printable coaxial cables, 50 Ω, type WZ, for use in aircraft electrical systems at operating temperatures between −65 °C and 200 °C and specially for high frequency up to 6 GHz.
The document encloses also a reinforced cable version (code R) which is used for sensitive systems with controlled VSWR.
- Standard19 pagesEnglish languagee-Library read for1 day
This document specifies the required characteristics and tests applicable to female electrical contacts 005, type A, crimp, class T, used in elements of connection according to EN 3155-002.
It is used together with EN 3155-001.
The associated male contacts are specified in EN 3155-004.
The contacts specified by this document are applicable for connector classes specified in EN 2997 series.
This document specifies two contact types (F and H) depending on connector class.
- Standard20 pagesEnglish languagee-Library read for1 day
This document specifies the required characteristics, tests and tooling applicable to male electrical contacts 004, type A, crimp, class T, used in elements of connection according to EN 3155 002.
It is used together with EN 3155 001.
The associated female contacts are specified in EN 3155 005.
The contacts specified by this document are applicable for connector classes specified in EN 2997 series.
This document specifies two contact types (M and H) depending on connector class.
- Standard19 pagesEnglish languagee-Library read for1 day
This document specifies the required characteristics, tests and tooling applicable to male electrical contacts, type A, crimp, class S, used in elements of connection according to EN 3155 002.
It is used together with EN 3155 001.
The tests as applied in this document do not permit the full qualification and are expected to be completed with associated components.
- Standard16 pagesEnglish languagee-Library read for1 day
This document specifies the required characteristics of a coaxial cable, 50 Ω, type WD, for use in aircraft electrical systems at operating temperature between -55 °C and 200 °C and specially for high frequency up to 6 GHz. Nevertheless, if needed, −65 °C is also acceptable as shown by thermal stability test.
- Standard17 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of post installation flexible self-wrapping fire protection sleeves for electrical cable and cable bundles, providing 360° fire protection to electrical harnesses. The sleeve assembly gives fire resistance protection to the internal electrical harness against fire for five minutes and ensures that the electrical characteristics of cables will not be degraded.
- Standard12 pagesEnglish languagee-Library read for1 day
This document specifies the required characteristics of coaxial cables, 50 Ω, type WN, for use in aircraft electrical systems at operating temperatures between −55 °C and 200 °C and specially for high frequency up to 6 GHz.
The document encloses also a reinforced cable version (code R) which is used for sensitive systems with controlled VSWR.
- Standard19 pagesEnglish languagee-Library read for1 day
This document specifies a method of evaluating the performance of a cable after exposure to a thermal shock.
It is intended to be used together with EN 3475-100.
- Standard6 pagesEnglish languagee-Library read for1 day
This document specifies a method of evaluating the performance of a cable after exposure to a thermal shock.
It is intended to be used together with EN 3475-100.
- Standard6 pagesEnglish languagee-Library read for1 day
This document specifies the dimensions, linear resistance, mechanical characteristics, construction and mass of conductors in aluminium or aluminium alloy for electrical cables for aerospace applications.
It applies to stranded conductors with nominal cross-sections of 5 mm2 to 115 mm2 inclusive.
- Standard11 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of three-pole circuit breakers, temperature compensated with a rated current from 1 A to 25 A, used in aircraft on-board circuits at a temperature between −55 °C and 125 °C for ratings ≤ 15 A and −55 °C and 90 °C for ratings > 15 A and at an altitude of 22 000 m max.
These circuit breakers are operated by a push-pull type single push button (actuator), with delayed action “trip-free” tripping with a polarized signal contact which is open when main contacts are closed, and inversely.
They will continue to function up to the short-circuit current.
- Standard14 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of three-pole circuit breakers, temperature compensated with a rated current from 1 A to 25 A, used in aircraft on-board circuits at a temperature between
-55 °C and 125 °C for ratings ≤ 15 A and -55 °C to 90 °C for ratings > 15 A and at an altitude of 22 000 m max.
These circuit breakers are operated by a push-pull type single pushbutton (actuator), with delayed action "trip-free" tripping with a signal contact which is open when main contacts are closed, and inversely.
They will continue to function up to the short-circuit current.
- Standard13 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of three-pole circuit breakers, temperature compensated with a rated current from 1 A to 25 A, used in aircraft on-board circuits at a temperature between −55 °C and 125 °C for ratings ≤ 15 A and −55 °C and 90 °C for ratings > 15 A and at an altitude of 22 000 m max.
These circuit breakers are operated by a push-pull type single push button (actuator), with delayed action “trip-free” tripping with a polarized signal contact which is open when main contacts are closed, and inversely.
They will continue to function up to the short-circuit current.
- Standard14 pagesEnglish languagee-Library read for1 day
This document specifies the dimensions, linear resistance, mechanical characteristics, construction and mass of conductors in aluminium or aluminium alloy for electrical cables for aerospace applications.
It applies to stranded conductors with nominal cross-sections of 5 mm2 to 115 mm2 inclusive.
- Standard11 pagesEnglish languagee-Library read for1 day
This document specifies the characteristics of three-pole circuit breakers, temperature compensated with a rated current from 1 A to 25 A, used in aircraft on-board circuits at a temperature between
-55 °C and 125 °C for ratings ≤ 15 A and -55 °C to 90 °C for ratings > 15 A and at an altitude of 22 000 m max.
These circuit breakers are operated by a push-pull type single pushbutton (actuator), with delayed action "trip-free" tripping with a signal contact which is open when main contacts are closed, and inversely.
They will continue to function up to the short-circuit current.
- Standard13 pagesEnglish languagee-Library read for1 day
This document specifies a method of determining the ability of elements of connection to withstand sinusoidal or random vibrations of specified severities.
It is used together with EN 2591-100.
This test is based on EN 60068-2-6 and EN 60068-2-64.
- Standard14 pagesEnglish languagee-Library read for1 day
This document specifies the test methods to evaluate the performance of coaxial, quadrax and databus cables after the installation of plastic cable ties.
It is expected to be used together with EN 3475 100.
- Standard12 pagesEnglish languagee-Library read for1 day
This document specifies the dimensions, tolerances, required characteristics and the mass of an AWG 24 shielded quad cable, type KL, intended for high speed (100 Mbit/s) full duplex Ethernet networks.
Linked to this particular application, the operating temperatures of the cable are between −65 °C and 125 °C.
This cable is laser markable, this marking satisfies the requirements of EN 3838.
The characteristics impedance is 100 Ω ± 15 Ω.
- Standard19 pagesEnglish languagee-Library read for1 day
This document specifies the general characteristics, conditions for qualification, acceptance and quality assurance for a fibre optic cable with a 62,5 µm/125 µm graded index fibre nominal, 1,8 mm outside diameter and of semi-loose buffer construction.
- Standard17 pagesEnglish languagee-Library read for1 day
This document specifies:
- the electrical, mechanical, environmental and dimensional characteristics of electrical contacts used in elements of connection, including coaxial, triaxial and quadrax contacts;
- the conditions for qualification, acceptance testing and quality assurance;
- the test programs and groups.
It is applicable to removable crimp contacts, wrap contacts, solder contacts used in connectors or in other elements of electrical connection.
In case of conflict or missing information between the EN 3155-001 and the product standards, the product standard takes precedence.
- Standard53 pagesEnglish languagee-Library read for1 day
This document specifies the required characteristics and tests applicable to sealing sleeves used in elements of connection according to EN 3155 002 and EN 4530-002.
- Standard9 pagesEnglish languagee-Library read for1 day
This document specifies the general characteristics, conditions for qualification, acceptance and quality assurance for a fibre optic cable with a 62,5 µm/125 µm graded index fibre nominal, 1,8 mm outside diameter and of semi-loose buffer construction.
- Standard17 pagesEnglish languagee-Library read for1 day
This document specifies the test methods to evaluate the performance of coaxial, quadrax and databus cables after the installation of plastic cable ties.
It is expected to be used together with EN 3475 100.
- Standard12 pagesEnglish languagee-Library read for1 day
This document specifies the dimensions, tolerances, required characteristics and the mass of an AWG 24 shielded quad cable, type KL, intended for high speed (100 Mbit/s) full duplex Ethernet networks.
Linked to this particular application, the operating temperatures of the cable are between −65 °C and 125 °C.
This cable is laser markable, this marking satisfies the requirements of EN 3838.
The characteristics impedance is 100 Ω ± 15 Ω.
- Standard19 pagesEnglish languagee-Library read for1 day
This document specifies a method of determining the ability of elements of connection to withstand sinusoidal or random vibrations of specified severities.
It is used together with EN 2591-100.
This test is based on EN 60068-2-6 and EN 60068-2-64.
- Standard14 pagesEnglish languagee-Library read for1 day