This document specifies the characteristics of externally threaded fasteners, pan head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated, for aerospace applications.
Classification: 1 100 MPa /315 °C .

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This document specifies the characteristics of externally threaded fasteners, 100° countersunk normal
head, Spiral Drive Recess, threaded to head, in heat and corrosion resisting steel, passivated, for
aerospace applications.

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This document specifies the characteristics of externally threaded fasteners, 100° countersunk normal
head, Spiral Drive Recess, short thread, in heat resisting steel FE-PA2601, passivated, for aerospace
applications.
Classification: 900 MPa
1/650 °C2.

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This document specifies the characteristics of externally threaded fasteners, 100° countersunk normal head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated, for aerospace applications.
Classification: 1 100 MPa /235 °C .

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This document specifies the characteristics of externally threaded fasteners, 100° countersunk normal head, Spiral Drive Recess, close tolerance normal shank, short thread, in titanium alloy, aluminium IVD coated, for aerospace applications.
Classification: 1 100 MPa /425 °C

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This document specifies the characteristics of externally threaded fasteners, 100° countersunk normal head, Spiral Drive Recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated, for aerospace applications.
Classification: 1 100 MPa /235 °C .

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This document specifies the characteristics of externally threaded fasteners, pan head, Spiral Drive
Recess, threaded to head, in heat and corrosion resisting steel, passivated, for aerospace applications.
Classification: 1 100 MPa1/425 °C2.

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This document specifies the characteristics of externally threaded fasteners, pan head, Spiral Drive
Recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated, for
aerospace applications.
Classification: 1 100 MPa1/235 °C2.

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This document specifies the dimensions of normal bihexagonal head bolts, with close or large tolerance normal shank and short or medium length MJ threads, in metallic material, coated or uncoated, with strength classes less than or equal to 1 100 MPa. This document is applicable to the compilation of aerospace product standards.

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The following documents are referred to in the text in such a way that some or all of their content constitutes requirements of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. ISO 7500‑1, Metallic materials — Calibration and verification of static uniaxial testing machines — Part 1: Tension/compression testing machines — Calibration and verification of the force-measuring system

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EN 2575 specifies the characteristics, qualification and acceptance requirements for bolts with MJ threads in heat resisting steel FE-PA2601, for aerospace applications.Classification: 900 MPa1/ 650 °C2.It is applicable whenever referenced.
Details

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This European Standard specifies the characteristics, qualification and acceptance requirements for helical coil screw thread inserts. It is applicable whenever referenced.

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This document specifies the characteristics of screws, pan head, offset cruciform recess, normal shank, long thread, in alloy steel, cadmium plated.
Classification: 1 100 MPa )/235 °C ).

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This document specifies the characteristics of bolts, shouldered, thin hexagonal head, close tolerance shank, short thread, in titanium alloy, anodized, MoS2 dryfilm coated, for aerospace applications. Classification: 1 100 MPa1/315 °C2. These bolts are intended to be used with washers according to EN 2414 and nuts according to EN 3230.

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This European Standard specifies dimensions, tolerances, characteristics and qualification requirements for MORTORQ Spiral Drive Recesses .
[MORTORQ® is the trade name of a product supplied by licensees of the Phillips Screw Company. This information is given for the convenience of users of this European Standard and does not constitute an endorsement by ASD-STAN nor CEN of the product named. Equivalent products may be used if they can be shown to lead to the same results.]

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This European standard specifies the characteristics of bolts, shouldered, thin hexagonal head, close tolerance shank, short thread, in titanium alloy, anodized, MoS2 dryfilm coated, for aerospace applications.
Classification: 1 100 MPa /315 °C .
These bolts are intended to be used with washers according to EN 2414 and nuts according to EN 3230.

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This European standard specifies the characteristics of screws, pan head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated, for aerospace applications.
Classification: 1 100 MPa /235 °C .

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This document specifies the technical, qualification and quality assurance requirements for bolts in material FE-PA2601 (A286) of tensile strength class 1 100 MPa at room temperature, maximum test temperature of material 650 °C.
Primarily for aerospace applications it is applicable to such bolts when referenced on the product standard or definition document.

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This document specifies the technical, qualification and quality assurance requirements for bolts in material FE-PA2601 (A286) of tensile strength class 1 100 MPa at room temperature, maximum test temperature of material 650 °C.
Primarily for aerospace applications it is applicable to such bolts when referenced on the product standard or definition document.

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This European standard specifies dimensions and gauging system for external MORTORQ super bolt
head spiral drive system1.

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This European standard specifies dimensions and gauging system for external MORTORQ super bolt
head spiral drive system1.

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This European standard specifies the characteristics, qualification and acceptance requirements for
bolts with MJ threads in TI-P64001, for aerospace applications.
Strength class: 1 100 MPa1.
It is applicable whenever referenced.

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This standard specifies the characteristics, qualification and acceptance requirements for bolts with MJ
threads in NI-PH2601.
Classification: 1 275 MPa1/650 °C2.
It is applicable whenever referenced.

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This document specifies the technical, qualification and quality assurance requirements for sensor based clamp load measurement systems for high tensile bolts and other clamp load sensitive elements. Primarily for aerospace applications, it is applicable to such products when referenced on the product standard or drawing.

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This European standard specifies the characteristics, qualification and acceptance requirements for
bolts with MJ threads in TI-P64001, for aerospace applications.
Strength class: 1 100 MPa1.
It is applicable whenever referenced.

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This standard specifies the characteristics, qualification and acceptance requirements for bolts with MJ threads in NI-PH2601.
Classification: 1 275 MPa /650 °C .
It is applicable whenever referenced.

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This European standard specifies the characteristics, qualification and acceptance requirements for
bolts with MJ threads in NI-PH2601, passivated, for aerospace applications.
Classification: 1 550 MPa1/650 °C2.
It is applicable whenever referenced.

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This European standard specifies the characteristics, qualification and acceptance requirements for bolts with MJ threads in NI-PH2601, passivated, for aerospace applications.
Classification: 1 550 MPa1/650 °C2.
It is applicable whenever referenced.

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This document specifies the technical, qualification and quality assurance requirements for sensor based clamp load measurement systems for high tensile bolts and other clamp load sensitive elements. Primarily for aerospace applications, it is applicable to such products when referenced on the product standard or drawing.

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This European standard specifies the characteristics of inserts, self locking, helical coil, tanged insertion drive, screw thread in NI-PH2801, for aerospace applications.
Maximum test temperature: 350 °C

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This European Standard describes the compilation of the component system the spring clip pin family
for use in fuselage interior equipment and in non-structural or secondary structural area for aerospace
applications.

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This standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal
shank, short thread, in titanium alloy, anodized, MoS2 lubricated.
Classification: 1 100 MPa1) / 315 °C2).

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This European Standard specifies the dimensions, mass, tolerances and static values of stud – quickrelease
and locking 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 standard specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated.
Classification: 1 100 MPa / 315 °C.

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This European Standard specifies the technical, qualification and quality assurance requirements for bolts in material FE-PM1708 (FV535) of tensile strength class 1 000 MPa at room temperature, maximum test temperature of material 550 °C.
Primarily for aerospace applications it is applicable to such bolts when referenced on the product standard or drawing.

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This European Standard specifies the technical, qualification and quality assurance requirements for bolts in material FE PM1708 (FV535) of tensile strength class 1 000 MPa at room temperature, maximum test temperature of material 550 °C.
Primarily for aerospace applications it is applicable to such bolts when referenced on the product standard or drawing.

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TC - mistake in drawing

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This European Standard specifies the characteristics of screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated.
Classification: 1 100 MPa  ) / 315 °C  ).

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TC - mistake in drawing

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This standard specifies the configuration, dimension, tolerances and mass of a stainless steel blind bolt with protruding head, for aerospace application.

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This standard specifies the dimensions, tolerances, required characteristics and mass of a stud for use in fuselage interior equipment and structural applications. This standard shall be used in conjunction with retaining washer per EN6090A01 (conform to EN 6090) and receptacles per EN 6092 or EN 6093.

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This standard specifies the dimensions, tolerances, required characteristics and mass of a stud for use in fuselage interior equipment and structural applications. This standard shall be used in conjunction with retaining washer per EN6090A01 (conform to EN 6090) and receptacles per EN 6092 or EN 6093.

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This standard specifies the configuration, dimension, tolerances and mass of a stainless steel blind bolt with protruding head, for aerospace application.

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ISO 8168:2016 the characteristics and quality assurance requirements for MJ thread bolts made of heat and corrosion resisting steel, of strength class 1 100 MPa, for aerospace construction. It is applicable whenever it is referenced in a definition document.

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  • Standard
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This European Standard specifies the characteristics of screws, pan head, six lobe recess, coarse
tolerance shank, medium length thread, in alloy steel, cadmium plated.
Classification: 1 100 MPa 1) / 235 °C 2).

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