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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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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This standard specifies the characteristics of spanner face wrenches for splined nuts for aerospace applications.

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

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

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

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

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This standard specifies the characteristics of open end box wrenches for splined nuts for aerospace applications.

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This standard specifies the characteristics of crow foot wrenches for splined nuts for aerospace applications.

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

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

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

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

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

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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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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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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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This standard defines the minimum clearance area required around nuts and bolt heads when using either double hexagon box or socket wrenches defined in AECMA standard.

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This standard defines the minimum clearance area required around nuts and bolt heads when using either double hexagon box or socket wrenches defined in AECMA standard.

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This standard specifies the properties of the following types of double end box wrenches: double head flat, double head offset and double end modified offset.

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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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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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This standard specifies the properties of double-hex sockets for aerospace use.

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

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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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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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