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
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This standard defines the requirements for selection, control, procurement and usage of EEE components for space projects.
This standard differentiates between three classes of components through three different sets of standardization requirements (clauses) to be met.
The three classes provide for three levels of trade-off between assurance and risk. The highest assurance and lowest risk is provided by class 1 and the lowest assurance and highest risk by class 3. Procurement costs are typically highest for class 1 and lowest for class 3. Mitigation and other engineering measures may decrease the total cost of ownership differences between the three classes. The project objectives, definition and constraints determine which class or classes of components are appropriate to be utilised within the system and subsystems.
a. Class 1 components are described in Clause 4.
b. Class 2 components are described in Clause 5
c. Class 3 components are described in Clause 6.
The requirements of this document apply to all parties involved at all levels in the integration of EEE components into space segment hardware and launchers.
- Standard103 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft126 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard20 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard20 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard26 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft22 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies a method of measuring the tensile properties of stranded conductors, strands, solid conductors and braids.
When required, it can be used also on finished cables.
It is intended to be used together with EN 3475-100.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft8 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft9 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard26 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft22 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft8 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements and test procedures of switching devices for use in aircraft
electrical systems to EN 2282.
- Standard42 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 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.
- Standard20 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft19 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies a test that determines the ability of electrical equipment to withstand wet atmospheres in combination with variable ambient air pressure in particular in an aircraft installation. The main adverse effects to be anticipated are fluid ingress and related insulation breakdown.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft10 pagesEnglish languagesale 10% offe-Library read for1 day
This document defines 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.
- Standard31 pagesEnglish languagesale 10% offe-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 impedance is 100 Ω ± 15 Ω.
- Standard15 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft15 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft14 pagesEnglish languagesale 10% offe-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 impedance is 100 Ω ± 15 Ω.
- Standard15 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft15 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft14 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard20 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft19 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 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.
- Standard31 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 a test that determines the ability of electrical equipment to withstand wet atmospheres in combination with variable ambient air pressure in particular in an aircraft installation. The main adverse effects to be anticipated are fluid ingress and related insulation breakdown.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft10 pagesEnglish languagesale 10% offe-Library read for1 day
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.
It is also possible to mark these cables with qualified compatible markings. These markings are supposed to be in accordance with EN 3838.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft10 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft10 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard14 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft12 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard25 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard20 pagesEnglish languagesale 10% offe-Library read for1 day
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
- Standard15 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard24 pagesEnglish languagesale 10% offe-Library read for1 day
This document evaluates the resistance of the fiber optic cable to humidity changes at different
temperatures.
- Standard7 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard21 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard20 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard5 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the required characteristics, test methods, qualification and acceptance
conditions of signal data transmission electrical cables.
- Standard14 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft14 pagesEnglish languagesale 10% offe-Library read for1 day
IEC 62668-1:2019 defines requirements for avoiding the use of counterfeit, recycled and fraudulent components used in the aerospace, defence and high performance (ADHP) industries. It also defines requirements for ADHP industries to maintain their intellectual property (IP) for all of their products and services. The risks associated with purchasing components outside of franchised distributor networks are considered in IEC 62668-2. Although developed for the avionics industry, this document can be applied by other high performance and high reliability industries at their discretion. This first edition cancels and replaces the third edition of IEC TS 62668-1 published in 2016. This edition includes the following significant technical changes with respect to the previous edition: a) added a reference to AS/EN/JISQ 9100 and AS/EN/JISQ 9110 which contain anti-counterfeit requirements b) added reference to USA DFAR rule 252.246.7008 and to UK Defence Standard 05-135; c) added reference to more GAO, OECD and ICC reports d) updated weblinks and other references; e) added new Annex E with figures describing how anti-counterfeit documents can be used in supply chains; f) added a reference to the new IECQ OD 3702 traceability audit; g) added new definition for re-manufactured components with a warning that these are not recommended.
- Standard90 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the required characteristics, test methods, qualification and acceptance conditions of signal data transmission electrical cables.
- Standard14 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft14 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard107 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft109 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard107 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft109 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard22 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft10 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard12 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft12 pagesEnglish languagesale 10% offe-Library read for1 day
IEC 62668-2:2019, defines requirements for avoiding the use of counterfeit, recycled and fraudulent components when these components are not purchased from the original component manufacturer (OCM) or are purchased from outside of franchised distributor networks for use in the aerospace, defence and high performance (ADHP) industries. This practice is used, as derogation, only when there are no reasonable or practical alternatives. NOTE: Typically this document is used in conjunction with IEC 62239-1 and IEC 62668-1, enabling ADHP industries to manage and avoid the use of counterfeit, recycled and fraudulent components in their supply chains. Although developed for the ADHP industry, this document can be used by other high-performance and high-reliability industries, at their discretion. This first edition cancels and replaces the second edition of IEC TS 62668-2 published in 2016. This edition constitutes a technical revision. This edition includes the following significant technical changes with respect to the second edition of IEC TS 62668-2: a) updates to the risk assessment process, including reference to SAE AS6081; b) updates to the test methods, including reference to the SAE AS6171 test methods published and in development; c) updates in line with IEC 62668-1 for definitions and references to DFARS.
- Standard59 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the general requirements and test methods for auto-transformer rectifier units (ATRUs) for use in aircraft electrical systems. This document is mainly applicable to ATRUs of 18-pulse and 24-pulse types.
- Standard14 pagesEnglish languagesale 15% off
This document specifies the requirements and test procedures of switching devices for use in aircraft
electrical systems to EN 2282.
- Standard42 pagesEnglish languagesale 10% offe-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 document).
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft10 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard14 pagesEnglish languagesale 10% offe-Library read for1 day
- Draft12 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard25 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard24 pagesEnglish languagesale 10% offe-Library read for1 day
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
- Standard15 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard20 pagesEnglish languagesale 10% offe-Library read for1 day