iTeh StandardsiTeh Standards
EURUSD
Your shopping cart is empty.

49.030 - Fasteners for aerospace construction

ICS 49.030 Details

Fasteners for aerospace construction

Befestigungsmittel der Luft- und Raumfahrttechnik

Elements de fixation pour la construction aeronautique

Vezni elementi za letalsko in vesoljsko gradnjo

General Information

Parent
49 - AIRCRAFT AND SPACE VEHICLE ENGINEERING
Sub-Items
49.030.01 - Fasteners in general
49.030.10 - Screw threads
49.030.20 - Bolts, screws, studs
49.030.30 - Nuts
49.030.40 - Pins, nails
49.030.50 - Washers and other locking elements
49.030.60 - Rivets
49.030.99 - Other fasteners

e-Library Subscription

Create subscription and get permanent access to documents within 49.030 - Fasteners for aerospace construction

Type
Monthly Subscription
for
seat
×
$ 227.19
$ 227.19

Currently subscription includes documents marked with .We are working on making all documents available within the subscription.

Standardization Organization
Technical Committee
Directive
Mandate
50
SIST
SIST EN 3637:2023(Main)
Aerospace series - Nut, self-locking, bi-hexagonal (double reduced), in heat resisting nickel base alloy - NI-P101HT (Waspaloy), silver plated, Classification: 1 210 MPa/730 °C
EN 3637:2023

This document specifies the dimensions of self-locking, silver-coated bi-hexagonal nuts with MJ-thread in heat resisting nickel base alloy NI-P101HT for aerospace applications.
Maximum test temperature of the material 730 °C.

  • Standard
    8 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 4269:2023(Main)
Aerospace series - Nuts, anchor, self-locking, floating, two lug, reduced series, with counterbore, in steel, cadmium plated, MoS2 lubricated - Classification: 1 110 MPa (at ambient temperature)/235 °C
EN 4269:2023

This document specifies the characteristics of self-locking, floating, two lug anchor nuts, reduced series,
with counterbore, in steel, cadmium plated, MoS 2 lubricated.
Classification: 1 100 MPa1/235 °C2

  • Standard
    9 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 3637:2023(Main)
Aerospace series - Nut, self-locking, bi-hexagonal (double reduced), in heat resisting nickel base alloy - NI-P101HT (Waspaloy), silver plated, Classification: 1 210 MPa/730 °C
SIST EN 3637:2023

This document specifies the dimensions of self-locking, silver-coated bi-hexagonal nuts with MJ-thread in heat resisting nickel base alloy NI-P101HT for aerospace applications.
Maximum test temperature of the material 730 °C.

  • Standard
    8 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 4269:2023(Main)
Aerospace series - Nuts, anchor, self-locking, floating, two lug, reduced series, with counterbore, in steel, cadmium plated, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/235 °C
SIST EN 4269:2023

This document specifies the characteristics of self-locking, floating, two lug anchor nuts, reduced series,
with counterbore, in steel, cadmium plated, MoS 2 lubricated.
Classification: 1 100 MPa1/235 °C2

  • Standard
    9 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 2886:2023(Main)
Aerospace series - Screw, pan head, offset cruciform recess, close tolerance normal shank, short thread, in alloy steel, cadmium plated - Classification: 900 MPa (at ambient temperature)/235 °C
EN 2886:2023

This document specifies the characteristics of screws, pan head, offset cruciform recess, close tolerance
normal shank, short thread, in alloy steel, cadmium plated.
Classification: 900 MPa1/ 235 °C2.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 2885:2023(Main)
Aerospace series - Screw, pan head, offset cruciform recess, coarse tolerance normal shank, short thread, in alloy steel, cadmium plated - Classification: 900 MPa (at ambient temperature)/235 °C
EN 2885:2023

This document specifies the characteristics of screws, pan head, offset cruciform recess, coarse tolerance
normal shank, short thread, in alloy steel, cadmium plated.
Classification: 900 MPa1/235 °C2.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 2885:2023(Main)
Aerospace series - Screw, pan head, offset cruciform recess, coarse tolerance normal shank, short thread, in alloy steel, cadmium plated - Classification: 900 MPa (at ambient temperature)/235 °C
SIST EN 2885:2023

This document specifies the characteristics of screws, pan head, offset cruciform recess, coarse tolerance
normal shank, short thread, in alloy steel, cadmium plated.
Classification: 900 MPa1/235 °C2.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 2886:2023(Main)
Aerospace series - Screw, pan head, offset cruciform recess, close tolerance normal shank, short thread, in alloy steel, cadmium plated - Classification: 900 MPa (at ambient temperature)/235 °C
SIST EN 2886:2023

This document specifies the characteristics of screws, pan head, offset cruciform recess, close tolerance
normal shank, short thread, in alloy steel, cadmium plated.
Classification: 900 MPa1/ 235 °C2.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 6081:2023(Main)
Aerospace series - Rivet, universal head, close tolerance - Inch series
EN 6081:2022

This document specifies the dimensions, tolerances and mass of rivets with universal head, close tolerance, inch series, for aerospace application.

  • Standard
    14 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    15 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 6069:2023(Main)
Aerospace series - Rivet, 100° reduced flush head, close tolerance - Inch series
EN 6069:2022

This document specifies the dimensions, tolerances and mass of rivets with 100° reduced flush head, close tolerance, inch series, for aerospace application.

  • Standard
    14 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    16 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 6080:2023(Main)
Aerospace series - Rivet, 100° normal flush head, close tolerance - Inch series
EN 6080:2022

This document specifies the dimensions, tolerances and masses of rivets with 100° normal flush head, close tolerance, inch series, for aerospace application.

  • Standard
    14 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    16 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 3434:2023(Main)
Aerospace series - Nuts, hexagon, slotted/castellated, self-locking, in steel, cadmium plated, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/235 °C
EN 3434:2022

This standard specifies characteristics of self-locking hexagonal slotted/castellated nuts, in steel, cadmium plated, MoS2 lubricated, for aerospace applications.
Classification: 900 MPa /235 °C .

  • Standard
    8 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    8 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 6101:2023(Main)
Aerospace series - Rivet, 100° medium flush head, close tolerance - Inch series
EN 6101:2022

This document specifies the dimensions, tolerances and mass of rivets with 100° medium flush head, close tolerance, inch series, for aerospace application.

  • Standard
    15 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    17 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 6101:2022(Main)
Aerospace series - Rivet, 100° medium flush head, close tolerance - Inch series
SIST EN 6101:2023

This document specifies the dimensions, tolerances and mass of rivets with 100° medium flush head, close tolerance, inch series, for aerospace application.

  • Standard
    15 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    17 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 6080:2022(Main)
Aerospace series - Rivet, 100° normal flush head, close tolerance - Inch series
SIST EN 6080:2023

This document specifies the dimensions, tolerances and masses of rivets with 100° normal flush head, close tolerance, inch series, for aerospace applications.

  • Standard
    14 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    16 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 3434:2022(Main)
Aerospace series - Nuts, hexagon, slotted/castellated, self-locking, in steel, cadmium plated, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/235 °C
SIST EN 3434:2023

This standard specifies characteristics of self-locking hexagonal slotted/castellated nuts, in steel, cadmium plated, MoS2 lubricated, for aerospace applications.
Classification: 900 MPa /235 °C .

  • Standard
    8 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    8 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 6081:2022(Main)
Aerospace series - Rivet, universal head, close tolerance - Inch series
SIST EN 6081:2023

This document specifies the dimensions, tolerances and mass of rivets with universal head, close tolerance, inch series, for aerospace application.

  • Standard
    14 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    15 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 6069:2022(Main)
Aerospace series - Rivet, 100° reduced flush head, close tolerance - Inch series
SIST EN 6069:2023

This document specifies the dimensions, tolerances and mass of rivets with 100° reduced flush head, close tolerance, inch series, for aerospace applications.

  • Standard
    14 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    16 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 6052:2022(Main)
Aerospace series - Rivet-collar-system, aluminium alloy, shear type, inch series - Technical Specification
EN 6052:2022

This document defines the requirements for qualification, acceptance, delivery and inspection of 100° countersunk head, 100° countersunk reduced head and protruding head close tolerance pins, shear type in aluminium alloy 7050T73 and collars of aluminium alloy 3003 and of aluminium alloy 6061T7 for use as permanent fasteners in aerospace applications.

  • Standard
    22 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    24 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 6052:2022(Main)
Aerospace series - Rivet-collar-system, aluminium alloy, shear type, inch series - Technical Specification
SIST EN 6052:2022

This document defines the requirements for qualification, acceptance, delivery and inspection of 100° countersunk head, 100° countersunk reduced head and protruding head close tolerance pins, shear type in aluminium alloy 7050-T73 and collars of aluminium alloy 3003 and of aluminium alloy 6061-T7 for use as permanent fasteners in aerospace applications.

  • Standard
    22 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    24 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 3228:2022(Main)
Aerospace series - Nuts, hexagonal, plain, reduced height, normal across flats, in steel, cadmium plated - Classification: 900 MPa (at ambient temperature)/235 °C
SIST EN 3228:2022

This document specifies the characteristics of plain hexagonal nuts, reduced height, normal across flats, in steel, cadmium plated, for aerospace applications.
Classification: 900 MPa/235 °C.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 4846:2022(Main)
Aerospace series - Screws, pan head, Spiral Drive Recess, threaded to head, in heat and corrosion resisting steel, passivated - Classification : 1 100 MPa (at ambient temperature) / 425 °C
SIST EN 4846:2022

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.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 4845:2022(Main)
Aerospace series - Screw, 100° countersunk normal head, Spiral Drive Recess, short thread, in heat resisting steel FE-PA2601 (A286), passivated - Classification: 900 MPa (at ambient temperature)/650 °C
SIST EN 4845:2022

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.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 4847:2022(Main)
Aerospace series - Screw, pan head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambient temperature)/235 °C
SIST EN 4847:2022

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.

  • Standard
    11 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 4848:2022(Main)
Aerospace series - Screw, pan head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C
SIST EN 4848:2022

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 .

  • Standard
    11 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 4844:2022(Main)
Aerospace series - Screws, 100° countersunk normal head, Spiral Drive Recess, threaded to head, in heat and corrosion resisting steel, passivated - Classification : 1 100 MPa (at ambient temperature) / 425 °C
SIST EN 4844:2022

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.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 4853:2022(Main)
Aerospace series - Externally threaded fastener, 100° countersunk normal head, Spiral Drive Recess - Classification: 1 100 MPa (at ambient temperature)/425 °C
SIST EN 4853:2022

This document specifies the characteristics of externally threaded fasteners, 100° countersunk normal head, Spiral Drive Recess, for aerospace applications.
Classification: 1 100 MPa /425 °C .

  • Standard
    19 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 4849:2022(Main)
Aerospace series - Screw, 100° countersunk normal head, Spiral Drive Recess, close tolerance normal shank, short thread, in titanium alloy, aluminium IVD coated - Classification: 1 100 MPa (at ambient temperature)/425 °C
SIST EN 4849:2022

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

  • Standard
    12 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 4851:2022(Main)
Aerospace series - Screw, 100° countersunk normal head, Spiral Drive Recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambient temperature)/235 °C
SIST EN 4851:2022

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 .

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 4850:2022(Main)
Aerospace series - Screw, 100° countersunk normal head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambient temperature)/235 °C
SIST EN 4850:2022

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 .

  • Standard
    13 pages
    English language
    sale 10% off
    e-Library read for
    1 day
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.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
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.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST-TP CEN/TR 17603-32-23:2022(Main)
Space engineering - Threaded fasteners handbook
CEN/TR 17603-32-23:2022

The users of this document are engineers involved in design, analysis or verification of joints on structures used for space missions. It is a guidelines document; therefore it includes advisory information rather than requirements.This document is intended to be applicable to any type of joint that is mechanically connected by threaded fasteners (e.g. bolts, screws, etc). It is written for joints made from metallic materials. However, subject to the engineering judgement of the user, many of the procedures presented herein may be applicable to joints made from composite materials.

  • Technical report
    234 pages
    English language
    sale 10% off
    e-Library read for
    1 day
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).

  • Technical report
    458 pages
    English language
    sale 10% off
    e-Library read for
    1 day
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.

  • Technical report
    488 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
CEN/TR 17603-32-23:2022(Main)
Space engineering - Threaded fasteners handbook
SIST-TP CEN/TR 17603-32-23:2022

2021-07-08: This TR is based on ECSS-E-HB-32-23A Rev.1
Exception XML - No CEN template.

  • Technical report
    234 pages
    English language
    sale 10% off
    e-Library read for
    1 day
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.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 3228:2022(Main)
Aerospace series - Nuts, hexagonal, plain, reduced height, normal across flats, in steel, cadmium plated - Classification: 900 MPa (at ambient temperature)/235 °C
EN 3228:2022

This document specifies the characteristics of plain hexagonal nuts, reduced height, normal across flats,
in steel, cadmium plated, for aerospace applications.
Classification: 900 MPa/235 °C1.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
  • Draft
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 4848:2022(Main)
Aerospace series - Screw, pan head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C
EN 4848:2022

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 .

  • Standard
    11 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 4847:2022(Main)
Aerospace series - Screw, pan head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambient temperature)/235 °C
EN 4847:2022

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.

  • Standard
    11 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 4850:2022(Main)
Aerospace series - Screw, 100° countersunk normal head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambient temperature)/235 °C
EN 4850:2022

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 .

  • Standard
    13 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 4851:2022(Main)
Aerospace series - Screw, 100° countersunk normal head, Spiral Drive Recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambient temperature)/235 °C
EN 4851:2022

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 .

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 4846:2022(Main)
Aerospace series - Screws, pan head, Spiral Drive Recess, threaded to head, in heat and corrosion resisting steel, passivated - Classification : 1 100 MPa (at ambient temperature) / 425 °C
EN 4846:2022

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.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 4845:2022(Main)
Aerospace series - Screw, 100° countersunk normal head, Spiral Drive Recess, short thread, in heat resisting steel FE-PA2601 (A286), passivated - Classification: 900 MPa (at ambient temperature)/650 °C
EN 4845:2022

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.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 4853:2022(Main)
Aerospace series - Externally threaded fastener, 100° countersunk normal head, Spiral Drive Recess - Classification: 1 100 MPa (at ambient temperature)/425 °C
EN 4853:2022

This document specifies the characteristics of externally threaded fasteners, 100° countersunk normal head, Spiral Drive Recess, for aerospace applications.
Classification: 1 100 MPa /425 °C .

  • Standard
    19 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 4844:2022(Main)
Aerospace series - Screws, 100° countersunk normal head, Spiral Drive Recess, threaded to head, in heat and corrosion resisting steel, passivated - Classification : 1 100 MPa (at ambient temperature) / 425 °C
EN 4844:2022

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.

  • Standard
    10 pages
    English language
    sale 10% off
    e-Library read for
    1 day
SIST
SIST EN 4849:2022(Main)
Aerospace series - Screw, 100° countersunk normal head, Spiral Drive Recess, close tolerance normal shank, short thread, in titanium alloy, aluminium IVD coated - Classification: 1 100 MPa (at ambient temperature)/425 °C
EN 4849:2022

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

  • Standard
    12 pages
    English language
    sale 10% off
    e-Library read for
    1 day
ISO
ISO 4579:2021(Main)
Aerospace — Drives, internal, TORX® PARALOBE® drive — Geometrical definition, gaging and technical requirements

This document specifies basic dimensions, characteristics and engineering requirements for TORX® PARALOBE® recesses in aerospace fasteners.

  • Standard
    7 pages
    English language
    sale 15% off
  • Draft
    7 pages
    English language
    sale 15% off
ISO
ISO 4580:2021(Main)
Aerospace — Drives, internal, TORX® PARALOBE® driver bit — Geometrical definition, gaging and technical requirements

This document specifies basic dimensions, characteristics and engineering requirements for TORX® PARALOBE® driver bits used with aerospace fasteners.

  • Standard
    9 pages
    English language
    sale 15% off
  • Draft
    9 pages
    English language
    sale 15% off
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.

  • Standard
    5 pages
    English language
    sale 15% off
  • Standard
    5 pages
    French language
    sale 15% off
  • Draft
    5 pages
    English language
    sale 15% off
  • Draft
    5 pages
    French language
    sale 15% off
50