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49.030.99 - Other fasteners

ICS 49.030.99 Details

Other fasteners

Weitere Befestigungsmittel der Luft- und Raumfahrttechnik

Autres éléments de fixation

Drugi vezni elementi

General Information

Parent
49.030 - Fasteners for aerospace construction

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Standardization Organization
Technical Committee
Directive
Mandate
50
SIST
SIST EN 4114:2024(Main)
Aerospace series - Clamps, loop ("P" type) in aluminium alloy, with rubber cushioning - Dimensions, masses
EN 4114:2023

This document specifies the required characteristics of loop style clamps ("P" type) in aluminium alloy with various cushion materials.
These clamps are used for supporting aerospace pipe assemblies and electrical cable bundles.
They are used up to 80 °C max.
Usage at a higher temperature is at the option of the user.
For temperature range and environmental considerations, see the various cushion material standards.

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SIST
SIST EN 4113:2024(Main)
Aerospace series - Clamps, loop ("P" type) in corrosion resisting steel, passivated with rubber cushioning - Dimensions, masses
EN 4113:2023

This document specifies the required characteristics of loop style clamps ("P" type) in corrosion resisting steel, passivated with various cushion materials.
These clamps are used for supporting aerospace pipe assemblies and electrical cable bundles.
For temperature range and environmental considerations see the various cushion material standards.

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SIST
SIST EN 6095:2024(Main)
Aerospace series - Rotary fasteners - Structural and non-structural applications - Technical specification
EN 6095:2023

This document specifies the required characteristics, inspections, tests, quality assurance requirements, conditions for qualification acceptance and delivery of rotary fasteners for structural and non-structural applications.
This document applies to all rotary fasteners for structural and non-structural applications. It can be applied when referred to in the product standard or in a design specification.

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CEN
EN 4113:2023(Main)
Aerospace series - Clamps, loop ("P" type) in corrosion resisting steel, passivated with rubber cushioning - Dimensions, masses
SIST EN 4113:2024

This document specifies the required characteristics of loop style clamps ("P" type) in corrosion resisting steel, passivated with various cushion materials.
These clamps are used for supporting aerospace pipe assemblies and electrical cable bundles.
For temperature range and environmental considerations see the various cushion material standards.

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CEN
EN 4114:2023(Main)
Aerospace series - Clamps, loop ("P" type) in aluminium alloy with rubber cushioning - Dimensions, masses
SIST EN 4114:2024

This document specifies the required characteristics of loop style clamps ("P" type) in aluminium alloy with various cushion materials.
These clamps are used for supporting aerospace pipe assemblies and electrical cable bundles.
They are used up to 80 °C max.
Usage at a higher temperature is at the option of the user.
For temperature range and environmental considerations, see the various cushion material standards.

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CEN
EN 6095:2023(Main)
Aerospace series - Rotary fasteners - Structural and non-structural applications - Technical specification
SIST EN 6095:2024

This document specifies the required characteristics, inspections, tests, quality assurance requirements, conditions for qualification acceptance and delivery of rotary fasteners for structural and non-structural applications.
This document applies to all rotary fasteners for structural and non-structural applications. It can be applied when referred to in the product standard or in a design specification.

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    13 pages
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SIST
SIST EN 2287:2022(Main)
Aerospace series - Bush, plain, in corrosion resisting steel with self-lubricating liner - Dimensions and loads
EN 2287:2022

This European Standard specifies the characteristics of plain bushes in corrosion resisting steel with self lubricating liner and the design recommendation of shafts and housings.
The bushes are intended for operation within the temperature range of −55 C to 163 C and assembly with an interference fit into fixed and moving aerospace parts.

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CEN
EN 2287:2022(Main)
Aerospace series - Bush, plain, in corrosion resisting steel with self-lubricating liner - Dimensions and loads
SIST EN 2287:2022

This European Standard specifies the characteristics of plain bushes in corrosion resisting steel with self lubricating liner and the design recommendation of shafts and housings.
The bushes are intended for operation within the temperature range of −55 C to 163 C and assembly with an interference fit into fixed and moving aerospace parts.

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CEN
CEN/TR 17603-32-22:2022(Main)
Space engineering - Insert design handbook
SIST-TP CEN/TR 17603-32-22:2022

This handbook recommends engineering inserts and practices for European programs and projects. It may be cited in contracts and program documents as a reference for guidance to meet specific program/project needs.
The target users of this handbook are engineers involved in the design, analysis and verification of launchers and spacecraft in relation to insert usage. The current know‐how is documented in this handbook in order to make expertise to all European developers of space systems.
It is a guidelines document, therefore it includes advisory information rather than requirements.

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CEN
CEN/TR 17603-32-21:2022(Main)
Space engineering - Adhesive bonding handbook
SIST-TP CEN/TR 17603-32-21:2022

This handbook is an acceptable way of meeting the requirements of adhesive materials in bonded
joints of EN 16603-32 (equivalent to ECSS‐E‐ST‐32).

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SIST
SIST EN 3077:2022(Main)
Aerospace series - Clamps worm drive - Technical specification
EN 3077:2022

This document specifies the required characteristics, inspections, test methods, quality assurance,
qualification, acceptance and delivery conditions of clamps worm drive designed for use with suitable
rubber hoses to form joints in fluid system pipelines.
The clamps worm drive are intended to be used as specified in the product standards.

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ISO
ISO 23887:2021(Main)
Aerospace — Blind fasteners, threaded type, self-locking — Test method for locking torque

This document describes the locking torque test method for blind fasteners, threaded type. This test method is used to measure the locking torque of blind fasteners with internal thread and external sleeve. It is applicable to blind fasteners consisting out of four elements (drive nut, nut, sleeve and corebolt) having a cross recess at the top of the nut.

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    4 pages
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    4 pages
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ISO
ISO 23886:2021(Main)
Aerospace — Collar, threaded, self-locking — Test method for torque and preload

This document describes torque and preload test method for threaded collars. This test method is used to measure the locking torque, breakaway torque, torque off and preload of threaded collars.

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    5 pages
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    5 pages
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    5 pages
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CEN
EN 4234:2020(Main)
Aerospace series - Clamps, worm drive - Dimensions, masses
SIST EN 4234:2020

This document specifies the characteristics of worm drive clamps designed for use with suitable rubber
hoses to form joints in fluid system pipelines for aerospace applications.

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SIST
SIST EN 4234:2020(Main)
Aerospace series - Clamps, worm drive - Dimensions, masses
EN 4234:2020

This document specifies the characteristics of worm drive clamps designed for use with suitable rubber
hoses to form joints in fluid system pipelines for aerospace applications.

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CEN
EN 3278:2019(Main)
Aerospace series - Sleeves, tubular, protruding head, in corrosion resisting steel, passivated (0,25 mm wall thickness)
SIST EN 3278:2020

This European standard specifies the characteristics and technical requirements for protruding head tubular sleeves, in corrosion resisting steel, which may be plain or provided with a series of annular grooves.
Passivated sleeves are for use in aerospace assemblies whose maximum operating temperature does not exceed 650 °C. The operating temperatures for aluminium pigmented sleeves should not exceed 230 °C.

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SIST
SIST EN 3278:2020(Main)
Aerospace series - Sleeves, tubular, protruding head, in corrosion resisting steel, passivated (0,25 mm wall thickness)
EN 3278:2019

This document specifies the characteristics and technical requirements for protruding head tubular sleeves, in corrosion resisting steel, which may be plain or provided with a series of annular grooves.
Passivated sleeves are for use in aerospace assemblies whose maximum operating temperature does not exceed 650 °C. The operating temperatures for aluminium pigmented sleeves should not exceed 230 °C.

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CEN
EN 2288:2019(Main)
Aerospace series - Bush, flanged, corrosion resisting steel, with self-lubricating liner - Dimensions and loads
SIST EN 2288:2019

This document specifies the characteristics of flanged bushes in corrosion resisting steel with self lubricating liner and the design recommendation of shafts and housings.
The bushes are intended for operation within the temperature range of −55 °C to 163 °C and assembly with an interference fit into fixed and moving aerospace parts.

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SIST
SIST EN 2288:2019(Main)
Aerospace series - Bush, flanged, corrosion resisting steel, with self-lubricating liner - Dimensions and loads
EN 2288:2019

This document specifies the characteristics of flanged bushes in corrosion resisting steel with self lubricating liner and the design recommendation of shafts and housings.
The bushes are intended for operation within the temperature range of −55 °C to 163 °C and assembly with an interference fit into fixed and moving aerospace parts.

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    9 pages
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CEN
EN 6128:2017(Main)
Aerospace series - Blind bolt, 100° flush head, high strength
SIST EN 6128:2017

This European Standard specifies the configuration, dimension, tolerances and mass of a stainless steel blind bolt with 100° flush head for aerospace application.

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CEN
EN 2286:2017(Main)
Aerospace series - Bushes, flanged aluminium alloy, with self-lubricating liner - Dimensions and loads
SIST EN 2286:2017

This document specifies the characteristics of flanged bushes in aluminium alloy with self lubricating liner and the design recommendation of shafts and housings.
The bushes are intended for operation within the temperature range of −55 °C to 121 °C and assembly with an interference fit into fixed and moving aerospace parts.

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CEN
EN 2285:2017(Main)
Aerospace series - Bushes, plain, aluminium alloy, with self-lubricating liner - Dimensions and loads
SIST EN 2285:2017

This document specifies the characteristics of plain bushes in aluminium alloy with self lubricating liner and the design recommendation of shafts and housings.
The bushes are intended for operation within the temperature range of −55 °C to 121 °C and assembly with an interference fit into fixed and moving aerospace parts.

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SIST
SIST EN 4702-04:2018(Main)
Aerospace series - Quick release fastening systems for non-structural and lining applications - Part 04: Spring clamp
EN 4702-04:2017

This standard describes the dimensions, mass, tolerances and static values of quick-release and
locking – clamps for use in fuselage interior equipment and non-structural or secondary structural area.

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CEN
EN 2311:2017(Main)
Aerospace series - Bushes with self-lubricating liner - Technical specification
SIST EN 2311:2017

This document specifies the required characteristics, inspections and tests, quality assurance and qualification, acceptance and delivery conditions for bushes, designed to be subjected under load, to slow sliding movements, rotations and small oscillations only for aerospace applications.
This standard applies to all bushes when referred to in the respective product standards or in a design documentation.
The liner is designed to be used in the temperature range of −50 °C to 163 °C. Aluminium bushes are limited to −55 °C to 121 °C.

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SIST
SIST EN 2285:2017(Main)
Aerospace series - Bushes, plain, aluminium alloy, with self-lubricating liner - Dimensions and loads
EN 2285:2017

This document specifies the characteristics of plain bushes in aluminium alloy with self-lubricating liner and
the design recommendation of shafts and housings.
The bushes are intended for operation within the temperature range of −55 °C to 121 °C and assembly with
an interference fit into fixed and moving aerospace parts.

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    10 pages
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SIST
SIST EN 2286:2017(Main)
Aerospace series - Bushes, flanged aluminium alloy, with self-lubricating liner - Dimensions and loads
EN 2286:2017

This document specifies the characteristics of flanged bushes in aluminium alloy with self-lubricating liner
and the design recommendation of shafts and housings.
The bushes are intended for operation within the temperature range of −55 °C to 121 °C and assembly with
an interference fit into fixed and moving aerospace parts.

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    10 pages
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SIST
SIST EN 2311:2017(Main)
Aerospace series - Bushes with self-lubricating liner - Technical specification
EN 2311:2017

This document specifies the required characteristics, inspections and tests, quality assurance and
qualification, acceptance and delivery conditions for bushes, designed to be subjected under load, to slow
sliding movements, rotations and small oscillations only for aerospace applications.
This standard applies to all bushes when referred to in the respective product standards or in a design
documentation.
The liner is designed to be used in the temperature range of −50 °C to 163 °C. Aluminium bushes are limited
to −55 °C to 121 °C.

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CEN
EN 4534-2:2016(Main)
Aerospace series - Bushes, plain in aluminium alloy with self-lubricating liner, elevated load - Part 2: Dimensions and loads - Inch series
SIST EN 4534-2:2016

This European Standard specifies the characteristics of plain bushes in aluminium alloy with self-lubricating liner, elevated load for aerospace applications.
The bushes are intended for use in fixed or moving parts of the aircraft structure and control mechanisms.
They shall be used in the temperature range - 55 °C to 121 °C.

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CEN
EN 6092:2016(Main)
Aerospace series - Receptacle, floating, double lug
SIST EN 6092:2016

This European Standard specifies the dimensions, tolerances, required characteristics and mass of a receptacle for use in fuselage interior equipment and structural applications. This standard shall be used in conjunction with studs per EN 6088 or EN 6105.

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SIST
SIST EN 6092:2016(Main)
Aerospace series - Receptacle, floating, double lug
EN 6092:2016

This European Standard specifies the dimensions, tolerances, required characteristics and mass of a
receptacle for use in fuselage interior equipment and structural applications. This standard shall be used in
conjunction with studs per EN 6088 or EN 6105.

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    9 pages
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CEN
EN 3238:2010(Main)
Aerospace series - Metallic materials - Test method - Shear test for wires and rivets
SIST EN 3238:2011

This standard specifies the requirements for shear testing rivet wire and rivets in metallic materials for aerospace applications.
It shall be applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or inspection schedule.

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    10 pages
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CEN
EN 4115:2010(Main)
Aerospace series - Cushion, rubber for clamps - Dimensions, masses
SIST EN 4115:2010

This standard specifies the required characteristics for rubber cushions used on clamps according to EN 3730, EN 4113, EN 4114.
For temperature range and environmental conditions see Table 1.

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    9 pages
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SIST
SIST EN 3427:2009(Main)
Aerospace series - Groove dimensions for radial mounting retaining rings
EN 3427:2006

This standard defines the definitions of groove for radial mounting retaining rings.

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    5 pages
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SIST
SIST EN 3426:2009(Main)
Aerospace series - Groove dimensions for axial mounting external type retaining rings
EN 3426:2006

This standard defines the dimensions of grooves for axial mounting, external type, retaining rings.

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    6 pages
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SIST
SIST EN 3425:2009(Main)
Aerospace series - Groove dimensions for axial mouting internal type retaining rings
EN 3425:2006

This standard defines the dimensions of grooves for axial mounting, internal type, retaining rings.

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    6 pages
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SIST
SIST EN 3709:2009(Main)
Aerospace series - Wrenches and sockets, bi-hexagonal - Technical specification
EN 3709:2006

This standard specifies the requirements to be complied with by wrenches and double-hex sockets intended for aerospace products.

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    9 pages
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SIST
SIST EN 4111:2009(Main)
Aerospace series - Wrenches, splined, socket for pipe fittings - Technical specification
EN 4111:2006

This standard specifies the requirements which must be met by hand-operated splined wrenches and sockets for aerospace applications.

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    8 pages
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SIST
SIST EN 4358:2009(Main)
Aerospace series - Six lobe recess - Drivers, double ended, 90°
EN 4358:2006

This standard specifies the characteristics of drivers, double ended, 90°, six lobe recess, for aerospace applications.

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    7 pages
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SIST
SIST EN 4357:2009(Main)
Aerospace series - Six lobe recess - Drivers, handle
EN 4357:2006

This standard specifies the characteristics of drivers, handle, six lobe recess, for aerospace applications.

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    6 pages
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SIST
SIST EN 4354:2009(Main)
Aerospace series - Six lobe recess - Drivers, relieved
EN 4354:2006

This standard specifies the characteristics of drivers, relieved, six lobe recess, for aerospace applications.

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    8 pages
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SIST
SIST EN 4356:2009(Main)
Aerospace series - Six lobe recess - Drivers, short
EN 4356:2006

This standard specifies the characteristics of drivers, short, six lobe recess, for aerospace applications.

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    7 pages
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SIST
SIST EN 4359:2009(Main)
Aerospace series - Six lobe recess - Drivers - Technical specification
EN 4359:2006

This standard specifies the characteristics, qualification and acceptance requirements for drivers for installing and removing screws and bolts having six lobe recess internal drive.

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    10 pages
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CEN
EN 3916:2008(Main)
Aerospace series - Insert, thin wall - Salvage procedure for components
SIST EN 3916:2008

1.1   This specification covers the accepted methods for the reclamation of installation holes for standard thin wall inserts, within assemblies.
1.2   To enable rectification when defects or damage occur to the standard insert tapped installation hole, or to rectify any out of position of the hole within the specified parameters of use.
1.3   To control the machining of the existing insert hole and the installation requirements of the replacement oversize thin wall insert.

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CEN
EN 3729:2008(Main)
Aerospace series - Rings, threaded, self-locking, left-hand thread, in heat resisting steel FE-PA92HT (A286), silver plated
SIST EN 3729:2008

This standard specifies the characteristics of threaded, self-locking rings, with left-hand threads, in FE PA92HT, silver plated, chiefly used for axial location of bearing outer rings.
Maximum test temperature of the parts: 450 °C.
NOTE   These parts are designed to be used with 4H6H internal threads.

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CEN
EN 3915:2008(Main)
Aerospace series - Insert, thin wall, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), for salvage of components - Classification: 1 275 MPa (at ambient temperature) / 550 °C - Technical specification
SIST EN 3915:2008

This standard specifies the characteristics, qualification and acceptance requirements for self-locking thin wall salvage inserts with MJ threads in NI-PH2601 (NI P100HT).
Classification: 1 275 MPa  ) / 550 °C  ).

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    19 pages
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CEN
EN 4302:2008(Main)
Aerospace series - Open ring insert tool, square drive
SIST EN 4302:2008

This standard specifies the characteristics of open ring insert tools for splined nuts, metric for aerospace applications.

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    7 pages
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CEN
EN 4355:2008(Main)
Aerospace series - Six lobe recess - Drivers, socket
SIST EN 4355:2008

This standard specifies the characteristics of drivers, socket, six lobe recess, for aerospace applications.

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SIST
SIST EN 3916:2008(Main)
Aerospace series - Insert, thin wall - Salvage procedure for components
EN 3916:2008

1.1   This specification covers the accepted methods for the reclamation of installation holes for standard thin wall inserts, within assemblies.
1.2   To enable rectification when defects or damage occur to the standard insert tapped installation hole, or to rectify any out of position of the hole within the specified parameters of use.
1.3   To control the machining of the existing insert hole and the installation requirements of the replacement oversize thin wall insert.

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    15 pages
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SIST
SIST EN 3729:2008(Main)
Aerospace series - Rings, threaded, self-locking, left-hand thread, in heat resisting steel FE-PA92HT (A286), silver plated
EN 3729:2008

This standard specifies the characteristics of threaded, self-locking rings, with left-hand threads, in FE PA92HT, silver plated, chiefly used for axial location of bearing outer rings.
Maximum test temperature of the parts: 450 °C.
NOTE   These parts are designed to be used with 4H6H internal threads.

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    7 pages
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SIST
SIST EN 3915:2008(Main)
Aerospace series - Insert, thin wall, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), for salvage of components - Classification: 1 275 MPa (at ambient temperature) / 550 °C - Technical specification
EN 3915:2008

This standard specifies the characteristics, qualification and acceptance requirements for self-locking thin wall salvage inserts with MJ threads in NI-PH2601 (NI P100HT).
Classification: 1 275 MPa  ) / 550 °C  ).

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    19 pages
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