49.030.99 - Other fasteners
Other fasteners
Weitere Befestigungsmittel der Luft- und Raumfahrttechnik
Autres éléments de fixation
Drugi vezni elementi
General Information
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.
- Standard11 pagesEnglish language
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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.
- Standard7 pagesEnglish language
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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.
- Standard7 pagesEnglish language
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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.
- Standard9 pagesEnglish language
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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.
- Standard9 pagesEnglish language
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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.
- Standard8 pagesEnglish language
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This European Standard specifies the configuration, dimension, tolerances and mass of a stainless steel blind bolt with 100° flush head for aerospace application.
- Standard14 pagesEnglish language
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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.
- Standard9 pagesEnglish language
sale 10% off- e-Library read for1 day
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.
- Standard9 pagesEnglish language
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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.
- Standard10 pagesEnglish language
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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.
- Standard10 pagesEnglish language
sale 10% off- e-Library read for1 day
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.
- Standard10 pagesEnglish language
sale 10% off- e-Library read for1 day
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.
- Standard10 pagesEnglish language
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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. Alumin...view more
- Standard28 pagesEnglish language
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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...view more
- Standard28 pagesEnglish language
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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.
- Standard9 pagesEnglish language
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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.
- Standard15 pagesEnglish language
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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.
- Standard9 pagesEnglish language
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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.
- Standard10 pagesEnglish language
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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.
- Standard9 pagesEnglish language
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