This document specifies the characteristics of hermetic jam-nut mounted receptacles in the family of circular electrical connectors coupled by threaded ring.
It is applicable to the class specified in Table 4.
For plugs and protective covers, see EN 2997-008 and EN 2997-009 respectively. For spare jam-nuts and O-rings, see EN 2997-012 and EN 2997-013 respectively.

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This document specifies the characteristics of jam-nut mounted receptacles in the family of circular electrical connectors coupled by threaded ring.
It is applicable to the class specified in Table 4.
For contacts, filler plugs, and rear accessories associated with this receptacle, see EN 2997-002. For plugs and protective covers, see EN 2997-008 and EN 2997-009 respectively. For spare jam-nuts and o-rings, see EN 2997-012 and EN 2997-013 respectively.

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This document specifies the required characteristics for heat-shrinkable limited fire hazard identification sleeves for use in aircraft electrical systems at operating temperatures between −40 °C and 105 °C.
This document is only applicable for the characterization of identification sleeves. This sleeving is flexible, flame retarded and emits minimum smoke, gases and corrosive by-products when exposed to fire. This sleeving is only applicable 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 document if they comply with the property requirements listed in Table 2 and Table 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 document 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.

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This document lists the product standards, covered by technical specification EN 4708-001, for heat shrinkable sleeves.

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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 15 000 m max.
These circuit breakers are operated by a push-pull type single pushbutton (actuator), with delayed action "trip-free" tripping.
They will continue to function up to the short-circuit current.

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This document specifies the characteristics of electrical wires DZA family for use in the on board:
- 115 VAC (phase to neutral) or 200 VAC (phase to phase) electrical network of aircraft;
- 230 VAC (phase to neutral) or 400 VAC (phase to phase) electrical network of aircraft and particularly use in non-pressurized areas.
This cable family is used at operating temperature between -65 °C and 260 °C. These cables are demonstrated to be arc resistant for both networks (115 VAC and 230 VAC).

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This document specifies the characteristics of UV laser printable electrical wires DZ family for use in the on board:
- 115 VAC (phase to neutral) or 200 VAC (phase to phase) electrical network of aircraft;
- 230 VAC (phase to neutral) or 400 VAC (phase to phase) electrical network of aircraft and particularly use in non-pressurized areas.
This cable family is used at operating temperature between -65 °C and 260 °C. These cables are demonstrated to be arc resistant for both networks (115 VAC and 230 VAC).

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This document specifies the required characteristics for fluoroelastomeric, heat-shrinkable boots for use in aircraft electrical systems at operating temperatures between −55 °C and 200 °C.
The moulded shapes can 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. The colour is normally black.
Styles and dimensions other than those specifically listed in EN 4840 002 can be available as custom items. These items are considered to comply with this document if they comply with the property requirements listed in Table 1 with the exception of dimensions.

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This document lists the product standards, covered by technical specification EN 4840-001, for heat-shrinkable moulded shapes.

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This document specifies the required characteristics of single braid, 120 ohms, size 26, electrical cable type WX, UV laser markable, intended for digital data transmissions.
It is used together with EN 3375 001.

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This document specifies methods of measuring thickness of electro-deposited gold or gold alloys coatings on contacts of elements of connection.

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This document specifies methods of verifying adhesion of electrodeposited gold and gold alloy coatings on contacts.

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This document defines a number of conditions common to rectangular electrical modular connectors for receptacles, plugs and rack and panel, with interchangeable modules and continuous operating temperature 175 °C.

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This document specifies a method of measuring the tensile properties of stranded conductors, single strands, solid conductors and braids.
When required, it can be used also on insulated wires and cables after removing the insulation.
It is intended to be used together with EN 3475-100.

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This document is applicable to the marking of aerospace vehicle electrical wires and cables using ultraviolet (UV) lasers.
This document specifies the process requirements for the implementation of UV laser marking of aerospace electrical wire and cable and fibre optic cable to achieve an acceptable quality mark using equipment designed for UV laser wire marking of identification codes on aircraft wire and cable subject to EN 3475-100, Aerospace series - Cables, electrical, aircraft use - Test methods - Part 100: General. Wiring specified as UV laser markable and which has been marked in accordance with this document will conform to the requirements of EN 3838.
This document is applicable to the marking of airframe electrical wires and cables using ultraviolet (UV) lasers. The laser process practices defined in this document are mandatory.

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This document specifies the required characteristics of cable ties with a metallic locking device manufactured from plastics material, for installation under controlled tension on aircraft cable harnesses.
It is used together with EN 4056-001.

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This document specifies the requirements and test procedures of switching devices for use in aircraft
electrical systems to EN 2282.

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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 impedance is 100 Ω ± 15 Ω.

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This document specifies the required characteristics, test methods, qualification and acceptance conditions of single and multicore cables, screened, jacketed and multicore jacketed cables for use in aircraft electrical systems.

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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.

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This document specifies the performance and contact arrangements of circular electrical connectors, coupled by threaded ring. It also lists the product standards and models available for selection in this series.

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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.

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This document specifies the characteristics of UV laser printable multicore jacketed electrical cables for use in the on-board electrical systems of aircraft at operating temperatures between −55 °C and 200 °C.

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This document specifies the general characteristics, the conditions of qualification, acceptance and quality assurance, as well as the test programs and groups for terminal lugs and in-line splices designed for crimping on copper and copper alloy conductors and on aluminium and aluminium alloy conductors.

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This document specifies tests that are to be performed on markings applied by the user to ensure that their durability is satisfactory and that, after application of markings directly to the cable insulation, jacket or sheath, the cable will meet the performance requirements laid down.

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This document defines a range of cable outlets, style K, 90°, shielded, sealed, self-locking (anti rotational) for heat shrinkable boot, and or with metallic bands under the following conditions.
The mating connectors are listed in EN 3660-002.
Temperature range,
Class N : -65 °C to 200 °C;
Class K : -65 °C to 260 °C;
Class W : -65 °C to 175 °C;
Class T : -65 °C to 175 °C (Nickel PTFE plating);
Class Z : -65 °C to 175 °C (Black zinc nickel plating).
Associated electrical accessories : EN 3660-033 Metallic band (for shield termination).
These cable outlets are designed for termination of overall shielding braid and/or individual cable shields. They accommodate/permit the termination of heat shrinkable boots.

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This product standard defines a range of cable outlets, style K, straight, shielded, sealed, self-locking (anti-rotational), heat shrinkable boot, and / or metallic bands for use under the following conditions:
The mating connectors are listed in EN 3660-002.
Temperature range,   
Class N   :   - 65 °C to 200 °C;
Class K   :   - 65 °C to 260 °C;
Class W   :   - 65 °C to 175 °C;
Class T   :   - 65 °C to 175 °C (Nickel PTFE plating);
Class Z   :    - 65 °C to 175 °C (Black zinc nickel plating).
Associated electrical accessories: EN 3660-033 Metallic band (for shield termination).
These cable outlets are designed for termination of overall shielding braid and / or individual cable shields. They accommodate/permit the termination of heat shrinkable boots.

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This document evaluates the resistance of the fiber optic cable to humidity changes at different
temperatures.

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This product standard defines a range of cable outlets, style K, straight, shielded, sealed, self-locking (anti-rotational), heat shrinkable boot, and / or metallic bands for use under the following conditions:
Associated electrical connector(s) EN 3660-002.
Temperature range,   Class N   :   - 65 °C to 200 °C;
Class K   :   - 65 °C to 260 °C;
Class W   :   - 65 °C to 175 °C;
Class T   :   - 65 °C to 175 °C (Nickel PTFE plating);
Class Z   :    - 65 °C to 175 °C (Black zinc nickel plating).
Associated electrical accessories: EN 3660-033 Metallic band (for shield termination).
These cable outlets are designed for termination of overall shielding braid and/or individual cable shields. They accommodate/permit the termination of heat shrinkable boots.

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This product standard defines a range of cable outlets, style K, 90°, shielded, sealed, self-locking (antirotational), for heat shrinkable boot, and/ or metallic bands for use under the following conditions:
The mating connectors are listed in EN 3660-002.
Temperature range, Class N : − 65 °C to 200 °C;
Class K : − 65 °C to 260 °C;
Class W : − 65 °C to 175 °C;
Class T : − 65 °C to 175 °C (Nickel PTFE plating);
Class Z : − 65 °C to 175 °C (Black zinc nickel plating).
Associated electrical accessories: EN 3660-033 Metallic band (for shield termination).
These cable outlets are designed for termination of overall shielding braid and/or individual cable
shields. They accommodate/permit the termination of heat shrinkable boots.

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This document specifies a method to determine the expansion range of protection sleeve for electrical cable and cable bundles, it is used together with EN 6059-100.

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This document specifies the required characteristics, tests and tooling applicable to female electrical
quadrax contacts, shielded, size 8, type E characteristic impedance 100 Ω, crimp, class R, used in
elements of connection according to EN 3155-002.
It is used together with EN 3155-001.
The associated male contacts are defined in EN 3155-074

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This document specifies the required characteristics, test methods, qualification and acceptance conditions of signal data transmission electrical cables.

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This document specifies the general characteristics, conditions for qualification, acceptance and quality assurance for a fibre optic cable with a 50/125 μm Graded Index fibre core, 1,8 mm outside diameter for non pull-proof contact designs.

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This document specifies the general characteristics, the conditions for qualification, acceptance and quality assurance, as well as the test programs and groups for threaded ring coupling circular connectors, fire resistant, intended for use in a temperature range from -65 °C to 175 °C continuous or 200 °C continuous according to the classes.

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This document specifies the characteristics of UV laser printable, single and multicore silver-plated copper screened (spiral) and jacketed electrical cables for use in the on-board electrical systems of aircraft, at operating temperatures between −55 °C and 200 °C.
It is also possible to mark these cables by qualified compatible marking. These markings are in accordance with EN 3838.

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This document specifies the process to be applied for measuring the contrast of wire and cable identification markings against the background of the unmarked wire insulation. It has been developed primarily to define a reproducible process of contrast value determination for use both to determine the intrinsic laser markability of wires at the time of manufacture or later, and to enable electrical wiring systems manufacturers to ensure that the whole process of wire marking is carried out to the required standard.

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This document defines the method to establish an electrical load analysis which is used to compare the supply capacity of an electrical power generation system with the power demand of the connected electrical utilisation equipment.
It shall prove that the power sources are capable of supplying these loads under all electrical power system states and aircraft operating conditions and that specified growth capacity for future requirements is ensured.

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This document specifies the three-pole temperature compensated circuit breakers with signal contacts, polarized or not, rated from 1 A to 25 A and used in aircraft on-board circuits. It describes specific environmental, electrical and mechanical characteristics and the stringency of tests to be applied according to test methods of EN 3841 100.
These circuit breakers are intended for use in aircraft with electrical supplies in accordance with EN 2282 (all categories).

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This document specifies the single-pole temperature compensated circuit breakers with signal contacts, polarized or not, rated from 1 A to 25 A and used in aircraft on-board circuits. It describes specific environmental, electrical and mechanical characteristics and the stringency of tests to be applied according to test methods of EN 3841 100.
These circuit breakers are intended for use in aircraft with electrical supplies in accordance with EN 2282 (all categories).

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This document specifies the single-pole temperature compensated circuit breakers rated from 20 A to 50 A and used in aircraft on-board circuits. It describes specific environmental, electrical and mechanical characteristics and the stringency of tests to be applied according to test methods of EN 3841 100.
These circuit breakers are intended for use in aircraft with electrical supplies in accordance with EN 2282 (all categories).

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This document specifies the three-pole temperature compensated circuit breakers without signal contacts, rated from 20 A to 50 A and used in aircraft on-board circuits. It describes specific environmental, electrical and mechanical characteristics and the stringency of tests to be applied according to test methods of EN 3841 100.
These circuit breakers are intended for use in aircraft with electrical supplies in accordance with EN 2282.

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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 document).

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This document specifies a range of cable outlets, style A, straight, unsealed with clamp strain relief for use under the following conditions:
Associated electrical connector(s): EN 3660 002
Temperature range,   Class N:   −65 °C to 200 °C
   Class W:   −65 °C to 175 °C
   Class K:   −65 °C to 260 °C
   Class A:   −65 °C to 200 °C
   Class T:   −65 °C to 175 °C (nickel PTFE plating)
   Class Z:   −65 °C to 175 °C (black zinc nickel plating)

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This document specifies a range of cable outlets, style A, 90°, unsealed with clamp strain relief for use under the following conditions:
Associated electrical connector(s): EN 3660 002
Temperature range,   Class N:   −65 °C to 200 °C
   Class W:   −65 °C to 175 °C
   Class K:   −65 °C to 260 °C
   Class A:   −65 °C to 260 °C
   Class T:   −65 °C to 175 °C (nickel PTFE plating)
   Class Z:   −65 °C to 175 °C (black zinc nickel plating)

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This document specifies a range of grommet nuts, style A, for use under the following conditions:
Associated electrical connector(s): EN 3660 002
Temperature range,   Class N:   −65 °C to 200 °C
   Class W:   −65 °C to 175 °C
   Class K:   −65 °C to 260 °C
   Class A:   −65 °C to 200 °C
   Class T:   −65 °C to 175 °C
   Class Z:   −65 °C to 175 °C

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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 15 000 m max.
These circuit breakers are operated by a push-pull type single pushbutton (actuator), with delayed action "trip-free" tripping.
They will continue to function up to the short-circuit current.

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This document specifies the characteristics of single-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 and at an altitude of 15 000 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.

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This document specifies the characteristics of electrical cables for use in the on-board electrical systems of aircraft at operating temperatures between -55 °C and 260 °C for cross sections equal to and greater than 5 mm2.

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