ASD/MECH - Mechanical

This standard specifies the characteristics of the thread end for 8°30' pipe couplings, nominal pressure up to 28 000 kPa, for aerospace applications.

This standard specifies the characteristics of elbows 45°, for pipe couplings 8°30', in titanium alloy, for aerospace
applications.
Nominal pressure: up to 28 000 kPa
Temperature range:   55 °C to 135 °C

This standard specifies the characteristics of elbows 45°, bulkhead, for pipe couplings 8°30', in titanium alloy, for aerospace
applications.
Nominal pressure: up to 28 000 kPa
Temperature range:   55 °C to 135 °C

This standard specifies the characteristics of thrust wire nuts for pipe couplings 8°30', in titanium alloy, for aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range: - 55 °C to 135 °C

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.

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

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 tempera-ture is at the option of the user.
For temperature range and environmental considerations see the various cushion material standards.

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.

This standard specifies the required characteristics of saddle clamps in aluminium alloy with various cushion materials.
These clamps, fixed version (type 1) or sliding version (type 2), are used for supporting pipe assemblies.
They are used up to 80 °C max. .
Usage at a higher tempera-ture is at the option of the user.
For temperature range and environmental considerations see the various cushion material standards.

This standard specifies the characteristics of bolts, normal hexagonal head, close tolerance normal shank, short thread, in heat and corrosion resisting steel, passivated, classification 1 100 MPa/425°C.

This standard specifies the characteristics of elbows 45°, welded end, with thrust wire nut, for pipe couplings 8°30', in
titanium alloy, for aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range:   55 °C to 135 °C

This standard specifies the characteristics of elbows 90°, with thrust wire nut, for pipe couplings 8°30', in titanium alloy, for
aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range:   55 °C to 135 °C

This standard specifies the characteristics of elbows 90°, welded end, with thrust wire nut, for pipe couplings 8°30', in
titanium alloy, for aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range:   55 °C to 135 °C

This standard specifies the rules for the marking of aerospace products. It is applicable whenever referenced in the definition document of the product.

This standard specifies the conditions of installation and removal (hole serration profile, tools, swaging procedure) of self-locking thin wall inserts defined by EN standards, for aerospace applications.

This standard specifies the characteristics, qualification and acceptance requirements for O-rings in fluorosilicone rubber FVMQ to EN 3825, EN 3826 and EN 3827.

This standard specifies the characteristics of O-rings in fluorosilicone rubber (FVMQ), hardness 80 IRHD for aerospace applications.

This standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank, short thread, in alloy steel, cadmium plated. Classification: 900 MPa / 235 degrees C.

This standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank, short thread, in corrosion resisting steel, passivated. Classification: 600 MPa / 425 degrees C.

This standard specifies the characteristics of bolts, normal hexagonal head, close tolerance normal shank, short thread, in alloy steel, cadmium plated. Classification: 1100 MPa / 235 degrees C.

This standard specifies the characteristics of self-locking hexagonal nuts with ball seat in alloy steel, cadmium plated, MoS2 lubricated. Classification: 900 MPa / 235 °C. They are intended to be used with washers to EN 2648 or suitable parts, see annex A.

This standard specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for plain spherical bearings designed to withstand static loads and loads with slight swivelling. It is applicable whenever referenced.

This standard specifies the characteristics of bolts, normal hexagonal head, close tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated. Classification: 1100 MPA / 315 degrees C.

This standard specifies the characteristics of inner clips, three parts, spring tension, in FE-PA92HT for applications at a maximum temperature of 260 °C.
They shall be assembled with parts from EN 4166 and EN 4168.

This standard specifies the characteristics of PTFE bushes for three part clips, spring tension for applications at a maximum temperature of 260 °C.
They shall be assembled with parts from EN 4167 and EN 4168.

This standard specifies the characteristics of outer clips, three parts, spring tension, in FE-PA92HT for applications at a maximum temperature of 260 °C.
They shall be assembled with parts from EN 4166 and EN 4167.

This standard specifies the characteristics of double hexagon headed bolts with relieved shank and long thread, in titanium alloy TI-P63, MoS2 coated, for aerospace applications. Classification: 1 100 MPa.

This standard specifies the characteristics, qualification and acceptance requirements for bolts with MJ threads in TI-P63.
Classification : 1 100 MPa
It is applicable whenever referenced.

This standard specifies the characteristics of screws with 100° countersunk head with six lobe recess, threaded to head, in TI-P63, anodized, MoS2 coated, for aerospace applications.
Classification: 900 MPa  )  / 350 °C

This standard specifies the characteristics of self-locking bihexagonal nuts in NI-P100HT, silver plated, for aerospace applications.
Classification : 1 550 MPa/600 °C

This standard specifies the characteristics of double hexagon headed bolts with lockwire holes, relieved shank and long thread, in TI-P63, anodized, MoS2 coated, for aerospace applications.
Strength class: 1 100 MPa

This standard specifies the characteristics of self-locking shank nuts in NI-P100HT, silver plated, for aerospace applications.
Classification: 1 550 MPa/600 °C

This standard specifies the characteristics of self-locking shank nuts in NI-P100HT, silver plated on thread, for aerospace applications.
Classification: 1 550 MPa  ) / 600 °C

This standard specifies the characteristics of pan head bolts with six lobe recess, normal shank and long thread, in TI-P63, MoS2 coated, for aerospace applications.
Strength class: 1 100 MPa
NOTE Taking account of the recess geometry, the strength class to be used for the seating torque calculation shall not be greater than 900 MPa.

This standard specifies the characteristics of self-locking bihexagonal nuts in NI-P100HT, silver plated on thread, for aerospace applications.
Classification: 1 550 MPa/600 °C

This standard specifies the characteristics of self-locking bihexagonal nuts in NI-P1 01 HT, silver plated on thread, for aerospace applications.
Classification: 1 210 MPa / 730 °C

This standard specifies the characteristics of self-locking shank nuts in NI-P101 HT, silver plated on thread, for use in 60° cone holes, for aerospace applications.
Classification: 1 210 MPa  ) / 730 °C