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Uued standardid


EVS-EN 4309:2016
Hind 6,47 EUR
Identne EN 4309:2016
Aerospace series - Nuts, hexagon, self-locking by plastic ring, normal height, normal across flats, in alloy steel, cadmium plated - Classification: 900 MPa (at ambient temperature) / 120 °C
This European Standard specifies the characteristics of hexagonal nuts, self-locking by plastic ring, normal height, normal across flats, in alloy steel, cadmium plated. Classification: 900 MPa / 120 °C

EVS-EN 3902:2016
Hind 5,62 EUR
Identne EN 3902:2016
Aerospace series - Washers for rivet assemblies, in aluminium alloy, anodized, metric series
This standard specifies the characteristics of washers for rivet assemblies, in aluminium alloy, anodized, metric series, for maximum operating temperature 120 °C, for aerospace applications.

EVS-EN 3672:2016
Hind 6,47 EUR
Identne EN 3672:2016
Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated, for 30°C swage - Classification: 1 210 MPa (at ambient temperature) / 730°C
No scope available

EVS-EN 2714-002:2016
Hind 8,72 EUR
Identne EN 2714-002:2016
Aerospace series - Cables, electrical, single and multicore for general purpose - Operating temperatures between - 55 °C and 260 °C - Part 002: Screened and jacketed - General
This European Standard specifies the list of product standards and common characteristics of single and multicore screened and jacketed electrical cables for use in the on-board electrical systems of aircraft, at operating temperatures between 55 °C and 260 °C (unless otherwise specified in product standards).

EVS-EN 2811:2016
Hind 6,47 EUR
Identne EN 2811:2016
Aerospace series - Nuts, hexagon, slotted/ castellated in steel cadmium plated - Classification: 1 100 MPa/235 °C
No scope available

EVS-EN 4701-002:2016
Hind 5,62 EUR
Identne EN 4701-002:2016
Aerospace series - Connectors, optical, rectangular, modular, operating temperature 125 °C, for EN 4531-101 contacts - Part 002: Specification of performance
This European Standard defines the material used in the manufacturing of EN 4701 optical modules.

EVS-EN 4644-002:2016
Hind 13,22 EUR
Identne EN 4644-002:2016
Aerospace series - Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Part 002: Specification of performance and contact arrangements
This European Standard specifies the common conditions for rectangular electrical modular connectors for receptacles and plugs with interchangeable modules and a continuous operating temperature of 175 °C (or 125 °C). Contact arrangements for fibre optic contacts are described in EN 4639-002.

EVS-EN 4644-142:2016
Hind 7,38 EUR
Identne EN 4644-142:2016
Aerospace series - Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Part 142: Size 4 receptacle for rack and panel application, class C and D - Product standard
This European Standard specifies the size 4 receptacle for rack and panel application used in the family of modular rectangular electrical and optical connector with rectangular inserts. The plug corresponding to this receptacle is defined in EN 4644-141.

EVS-EN 6059-202:2016
Hind 5,62 EUR
Identne EN 6059-202:2016
Aerospace series - Electrical cables, installation - Protection sleeves - Test methods - Part 202: Dimensions and mass
No scope available

ISO 7718-1:2016
Hind 35,48 EUR
Aircraft -- Passenger doors interface requirements for connection of passenger boarding bridge or passenger transfer vehicle -- Part 1: Main deck doors
ISO 7718-1:2016 specifies minimum requirements for dimensions and unobstructed space around main deck passenger doors of future types of civil-passenger transport aircraft when they are intended to be compatible with the thousands of passenger boarding bridges and passenger transfer vehicles existing, or being planned, in airports worldwide. ISO 7718-1:2016 is not applicable to existing models of civil transport aircraft, or derivative models with entry into service up to year 2000 with the same fuselage, for which the aircraft-mating section of passenger boarding bridges or passenger transfer vehicles is expected to be compatible with ISO 16004. It is not the intent of this document to restrict in any way the basic design of any future types of civil-passenger transport aircraft. However, it aims at clarifying, for aircraft-design engineers, the design characteristics which would make it difficult or impossible for a new type of aircraft to adequately connect with existing airport passenger boarding bridges or passenger transfer vehicles. If basic aircraft-design requirements impose on a future model certain dimensional characteristics not complying with this document, note that: - either alternative methods of embarking/disembarking passengers will need to be implemented, such as integral aircraft stairs, etc.; - or existing passenger boarding bridges and/or passenger transfer vehicles in the airports where such a new type of aircraft is to operate will require some degree of modification/reworking; - or additional interface devices/equipment will be required in order to connect such a new type of aircraft with existing passenger boarding bridges and passenger transfer vehicles. Each case results in increased aircraft-handling constraints and operating cost.
Asendab ISO 7718-1:2009

ISO 7718-2:2016
Hind 35,48 EUR
Aircraft -- Passenger doors interface requirements for connection of passenger boarding bridge or passenger transfer vehicle -- Part 2: Upper deck doors
ISO 7718-2:2016 specifies the minimum dimensional and unobstructed space requirements around future civil-passenger transport aircraft upper deck passenger doors when they are intended to be compatible with passenger boarding bridges planned in airports worldwide. This document is not applicable to existing models of civil transport aircraft, or derivative models with entry into service up to year 2000 with the same fuselage, for which the aircraft-mating section of passenger boarding bridges or passenger transfer vehicles is expected to be compatible with ISO 16004. However, it is expected that the design of such aircraft types may be taken into account for design of passenger boarding bridges capable of upper deck servicing, in addition to this document. It is not the intent of this document to restrict in any way the basic design of any future types of civil-passenger transport aircraft. It aims, however, at clarifying for aircraft design engineers the design characteristics which would make it difficult or impossible for a new type of aircraft to adequately connect with airport passenger boarding bridges. Should basic aircraft design requirements impose on a future model certain dimensional characteristics not complying with this document, note that: - either alternative methods of embarking/disembarking passengers will need to be implemented, such as using the internal aircraft stairs, etc.; - or upper deck passenger boarding bridges in the airports where such a new type of aircraft is to operate will require some degree of modification/reworking; - or additional interface devices/equipment will be required in order to connect such a new type of aircraft with existing upper deck passenger boarding bridges. Each case results in increased aircraft-handling constraints and operating cost.
Asendab ISO 7718-2:2009

Asendatud või tühistatud standardid


EVS-EN 3672:2008
Identne EN 3672:2008
Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated, for 30° swage - Classification: 1 210 MPa (at ambient temperature)/730 °C
This standard specifies the characteristics of self-locking shank nuts in NI-P101HT, silver plated, for use in 30° cone holes, for aerospace applications. Classification: 1 210 MPa1)/730 °C2)
Keel: Inglise
Asendatud EVS-EN 3672:2016

EVS-EN 4644-002:2012
Identne EN 4644-002:2012
Aerospace series - Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Part 002: Specification of performance and contact arrangements
This European Standard specifies the common conditions for rectangular electrical modular connectors for receptacles and plugs with interchangeable modules and a continuous operating temperature of 175 °C (or 125 °C). Contact arrangements for fibre optic contacts are described in EN 4639-002.
Keel: Inglise

EVS-EN 4644-142:2012
Identne EN 4644-142:2012
Aerospace series - Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175 °C (or 125 °C) continuous - Part 142: Size 4 receptacle for rack and panel application - Product standard
This European Standard specifies the size 4 receptacle for rack and panel application used in the family of modular rectangular electrical and optical connector with rectangular inserts, operating temperature 175 °C (or 125 °C) continuous. The plug corresponding to this receptacle is defined in EN 4644-141.
Keel: Inglise

EVS-EN 2714-002:2012
Identne EN 2714-002:2012
Aerospace series - Cables, electrical, single and multicore for general purpose - Operating temperatures between - 55 °C and 260 °C - Part 002: Screened and jacketed - General
This European Standard specifies the list of product standards and common characteristics of single and multicore screened and jacketed electrical cables for use in the on-board electrical systems of aircraft, at operating temperatures between - 55 °C and 260 °C (unless otherwise specified in product standards).
Keel: Inglise

EVS-EN 4701-002:2013
Identne EN 4701-002:2013
Aerospace series - Connectors, optical, rectangular, modular, operating temperature 125 °C, for EN 4531-101 contacts - Part 002: Material
This European Standard defines the material used in the manufacturing of EN 4701 optical modules.
Keel: Inglise

Kavandite arvamusküsitlus


FprEN 9110
Identne FprEN 9110
Tähtaeg 3.03.2017
Quality Management Systems - Requirements for Aviation Maintenance Organizations
This document standardizes quality management system requirements to the greatest extent possible and can be used at all levels of the supply chain by organizations around the world. Its use should result in improved quality, cost and delivery performance through the reduction or elimination of organization-unique requirements, effective implementation of the quality management system and wider application of good practice. While primarily developed for civil and military aviation industry organizations providing maintenance services, this standard can also be used in other industry sectors when a quality management system with additional requirements over an EN ISO 9001:2015 system is needed. This standard includes EN ISO 9001:20151) quality management system requirements and specifies additional civil and military aviation maintenance and continuing airworthiness industry requirements, definitions and notes as shown in bold, italic text.
Keel: Inglise

prEN 16603-31-02
Identne ECSS-E-ST-31-02C Rev.1; prEN 16603-31-02
Tähtaeg 3.03.2017
Space engineering - Two-phase heat transport equipment
This standard defines requirements for two-phase heat transportation equipment (TPHTE), for use in spacecraft thermal control. This standard is applicable to new hardware qualification activities. Requirements for mechanical pump driven loops (MPDL) are not included in the present version of this Standard. This standard includes definitions, requirements and DRDs from ECSS-E-ST-10-02, ECSS-E-ST-10-03, and ECSS-E-ST-10-06 applicable to TPHTE qualification. Therefore, these three standards are not applicable to the qualification of TPHTE. This standard also includes definitions and part of the requirements of ECSS-E-ST-32-02 applicable to TPHTE qualification. ECSS-E-ST-32-02 is therefore applicable to the qualification of TPHTE. This standard does not include requirements for acceptance of TPHTE. This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.
Keel: Inglise

prEN 16603-60-21
Identne ECSS-E-ST-60-21C DIR1; prEN 16603-60-21
Tähtaeg 3.03.2017
Space engineering - Gyros terminology and performance specification
This Standard specifies gyros functions and performances as part of a space project. This Standard covers aspects of functional and performance requirements, including nomenclature, definitions, functions and performance metrics for the performance specification of spaceborne gyros. The Standard focuses on functional and performance specifications with the exclusion of mass and power, TM/TC interface and data structures. When viewed from the perspective of a specific project context, the requirements defined in this Standard can be tailored to match the genuine requirements of a particular profile and circumstances of a project. The requirements verification by test can be performed at qualification level only or also at acceptance level. It is up to the Supplier, in agreement with the customer, to define the relevant verification approach in the frame of a specific procurement, in accordance with clause 5.2 of ECSS-E-ST-10-02. The present standard does not cover gyro use for launch vehicles. This standard can be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.
Keel: Inglise

FprEN 9100
Identne FprEN 9100
Tähtaeg 3.03.2017
Quality Management Systems - Requirements for Aviation, Space and Defense Organizations
This document standardizes quality management system requirements to the greatest extent possible and can be used at all levels of the supply chain by organizations around the world. Its use should result in improved quality, cost and delivery performance through the reduction or elimination of organization-unique requirements, effective implementation of the quality management system and wider application of good practice. While primarily developed for the aviation, space and defence industry, this standard can also be used in other industry sectors when a quality management system with additional requirements over an EN ISO 9001 system is needed.
Keel: Inglise

FprEN 9101
Identne FprEN 9101
Tähtaeg 3.03.2017
Quality Management Systems - Audit Requirements for Aviation, Space, and Defence Organisations
This document has been prepared by the IAQG and standardizes the requirements for conducting and reporting of QMS audits. It can be used at all levels of the supply chain by organizations around the world. It provides requirements for an audit and reporting process, based on the: • process and continual improvement approach defined in EN 9100-series standards; • specific aviation, space, and defence additions in EN 9100-series standards; • use of common audit tools; and • uniform, transparent, and standardized reporting of audit results.
Keel: Inglise

FprEN 9120
Identne FprEN 9120
Tähtaeg 3.03.2017
Quality Management Systems - Requirements for Aviation, Space and Defence Distributors
This document standardizes quality management system requirements to the greatest extent possible and can be used at all levels of the supply chain by organizations around the world. Its use should result in improved quality, cost and delivery performance through the reduction or elimination of organization-unique requirements, effective implementation of the quality management system and wider application of good practice. While primarily developed for the aviation, space and defence industry, this standard can also be used in other industry sectors when a quality management system with additional requirements over an EN ISO 9001 system is needed. This standard includes EN ISO 9001:2015 quality management system requirements and specifies additional aviation, space and defence industry requirements, definitions and notes as shown in bold, italic text.
Keel: Inglise