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49.030.10 - Screw threads

ICS 49.030.10 Details

Screw threads

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49.030 - Fasteners for aerospace construction

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Standardization Organization
Technical Committee
Directive
Mandate
50
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
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ISO
ISO 3353-1:2020(Main)
Aerospace — Lead and runout threads — Part 1: Rolled external threads

This document specifies the lead and runout requirements for rolled external threads for aerospace construction, and the inspection method to be used in case of dispute. It is applicable whenever it is referenced in a definition document.

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    10 pages
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  • Draft
    10 pages
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ISO
ISO 3353-2:2020(Main)
Aerospace — Lead and runout threads — Part 2: Internal threads

This document specifies the lead and runout thread and undercut requirements for internal threads (blind tapped holes) for aerospace construction. It is applicable whenever it is referenced in a definition document.

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    5 pages
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  • Draft
    5 pages
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CEN
EN 4178:2017(Main)
Aerospace series - Screws, pan head, six lobe 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 4178:2017

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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ISO
ISO 15872:2017(Main)
Aerospace — UNJ threads — Gauging

ISO 15872:2017 provides methods for the gauging of ISO UNJ threads complying with ISO 3161. Other methods of ensuring that the product is within the specified limits can be used, provided that correlation with the specified gauges is established.

  • Standard
    22 pages
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SIST
SIST EN 4178:2017(Main)
Aerospace series - Screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C
EN 4178:2017

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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CEN
EN 4163:2016(Main)
Aerospace series - Screws 100° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated - Classification: 1 100 MPa (at ambient temperature) / 235 °C
SIST EN 4163:2016

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

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ISO
ISO 10959:2016(Main)
Aerospace — MJ threads — Gauging

ISO 10959:2016 contains information for the gauging of ISO MJ threads in accordance with ISO 5855‑1, ISO 5855‑2, and ISO 5855‑3. Other methods of ensuring that the product is within the specified limits may be used provided correlation with the specified gauges is established [see 8.2, e)].

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SIST
SIST EN 3274:2011(Main)
Aerospace series - Pipe coupling 8°30' - Thread end - Geometric configuration
EN 3274:2010

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

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CEN
EN 4624:2010(Main)
Aerospace series - Inserts, MJ threads, self-locking, with self-broaching keys, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plate
SIST EN 4624:2010

This standard specifies the characteristics of self-locking, MJ thread inserts, self-broaching keys, in NI PH1302, silver plated, for aerospace applications.
Classification: 1 200 MPa / 800 °C

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CEN
EN 4622:2010(Main)
Aerospace series - Inserts, MJ threads, self-locking, with self-broaching keys, in heat resisting steel FE-PA2601 (A286), MoS2 coated
SIST EN 4622:2010

This standard specifies the characteristics of self-locking, MJ thread inserts, self-broaching keys, in FE PA2601, MoS2 coated, for aerospace applications.
Classification: 1 100 MPa / 315 °C

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CEN
EN 4623:2010(Main)
Aerospace series - Inserts, MJ threads, self-locking, with self-broaching keys, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated
SIST EN 4623:2010

This standard specifies the characteristics of self-locking, MJ thread inserts, self-broaching keys, in NI PH2601, silver plated, for aerospace applications.
Classification: 1 550 MPa / 600 °C

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SIST
SIST EN 4623:2010(Main)
Aerospace series - Inserts, MJ threads, self-locking, with self-broaching keys, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated
EN 4623:2010

This standard specifies the characteristics of self-locking, MJ thread inserts, self-broaching keys, in NI-PH2601, silver plated, for aerospace applications. Classification: 1 550 MPa/600 °C.

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SIST
SIST EN 4624:2010(Main)
Aerospace series - Inserts, MJ threads, self-locking, with self-broaching keys, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plate
EN 4624:2010

This standard specifies the characteristics of self-locking, MJ thread inserts, self-broaching keys, in NI-PH1302, silver plated, for aerospace applications. Classification: 1 200 MPa/800 °C).

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    9 pages
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SIST
SIST EN 4622:2010(Main)
Aerospace series - Inserts, MJ threads, self-locking, with self-broaching keys, in heat resisting steel FE-PA2601 (A286), MoS2 coated
EN 4622:2010

This standard specifies the characteristics of self-locking, MJ thread inserts, self-broaching keys, in FE-PA2601, MoS2 coated, for aerospace applications. Classification: 1 100 MPa/ 315 °C).

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    9 pages
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CEN
EN 4636:2009(Main)
Aerospace series - Screws, 100° countersunk head, six lobe recess, short thread, in titanium alloy TI-P64001, with aluminium pigmented coating - Classification: 1 100 MPa (at ambient temperature) / 315 °C
SIST EN 4636:2009

This standard specifies the characteristics of screws with 100° countersunk head, with six lobe recess, short
thread, in titanium alloy TI-P64001, aluminium pigmented coating, for aerospace applications.

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    7 pages
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CEN
EN 4493:2008(Main)
Aerospace series - Inserts, screw thread, helical coil, self-locking, in heat resisting nickel base alloy NI-PH1801 (NI-P96HT, Nimonic 90), silver plated
SIST EN 4493:2008

This standard specifies the characteristics of self-locking, helical coil, screw thread inserts in NI-PH1801 (NI P96HT), silver plated, for aerospace applications.
Maximum test temperature: 550 °C.

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    8 pages
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SIST
SIST EN 4493:2008(Main)
Aerospace series - Inserts, screw thread, helical coil, self-locking, in heat resisting nickel base alloy NI-PH1801 (NI-P96HT, Nimonic 90), silver plated
EN 4493:2008

This standard specifies the characteristics of self-locking, helical coil, screw thread inserts in NI-PH1801 (NI P96HT), silver plated, for aerospace applications.
Maximum test temperature: 550 °C.

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ISO
ISO 3161:1999(Main)
Aerospace — UNJ threads — General requirements and limit dimensions

This International Standard specifies the general requirements and limit dimensions of inch series UNJ threads with controlled root radius for aerospace construction. It determines the basic triangular profile for this type of thread and gives a system for designating the diameter and number of threads per inch combinations. For all diameters 0,060 in (1,524 mm) to 6,000 in (152,4 mm), it offers in the form of tables the basic dimensions and tolerances for a selection of diameter and number of threads per inch combinations. It also provides the method of calculation for the dimensions and tolerances for any diameter and number of threads per inch combination not given in the tables, including threads with a diameter in excess of 6,000 in.

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    40 pages
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ISO
ISO 5855-2:1999(Main)
Aerospace — MJ threads — Part 2: Limit dimensions for bolts and nuts

This part of ISO 5855 specifies limit dimensions of MJ threads for bolts and nuts of nominal diameter 1,6 mm to 39 mm for aerospace construction.

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    6 pages
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ISO
ISO 5855-3:1999(Main)
Aerospace — MJ threads — Part 3: Limit dimensions for fittings for fluid systems

This part of ISO 5855 specifies limit dimensions of MJ threads for fluid systems fittings for aerospace construction.

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    6 pages
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    6 pages
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ISO
ISO 5855-1:1999(Main)
Aerospace — MJ threads — Part 1: General requirements

This part of ISO 5855 specifies the general requirements for MJ threads used in aerospace construction. It determines the basic triangular profile for this type of thread and gives a system for designating the diameter and pitch combinations. For all diameters 1,6 mm to 300 mm, it offers in the form of tables the basic dimensions and tolerances for a selection of diameter and pitch combinations. It also provides the method of calculation for the dimensions and tolerances for any diameter and pitch combination not given in the tables, including threads with a diameter in excess of 300 mm. For limit dimensions for bolts and nuts of nominal diameter 1,6 mm to 39 mm, see ISO 5855-2. For limit dimensions for fittings for fluid systems, see ISO 5855-3.

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    36 pages
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SIST
SIST EN 4178:2010(Main)
Aerospace series - Screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - 1100 MPa (at ambient temperature)/315 °C
EN 4178:2009

This 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 1) / 315 °C 2)

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CEN
EN 4178:2009(Main)
Aerospace series - Screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - 1 100 MPa (at ambient temperature) / 315 °C
SIST EN 4178:2010

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.

  • Standard
    8 pages
    English language
    sale 10% off
    e-Library read for
    1 day
CEN
EN 4163:2009(Main)
Aerospace series - Screws 100° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated - 1 100 MPa (at ambient temperature) / 235 °C
SIST EN 4163:2010

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

  • Standard
    8 pages
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SIST
SIST EN 3274:2004(Main)
Aerospace series - Pipe coupling 8°30' - Thread end - Geometric configuration
EN 3274:2001

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

  • Standard
    10 pages
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CEN
EN 3274:2001(Main)
Aerospace series - Pipe coupling 8°30' - Thread end - Geometric configuration
SIST EN 3274:2004

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

  • Standard
    10 pages
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ISO
ISO 15872:2002(Main)
Aerospace — UNJ threads — Gauging

ISO 15872:2002 gives information for the gauging of ISO UNJ threads complying with ISO 3161. Other methods of ensuring that the product is within the specified limits may be used, provided correlation with the specified gauges is established.

  • Standard
    27 pages
    English language
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  • Standard
    27 pages
    French language
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ISO
ISO 3353-1:2002(Main)
Aerospace — Lead and runout threads — Part 1: Rolled external threads

ISO 3353-1:2002 specifies the lead and runout requirements for rolled external threads for aerospace construction, and the inspection method to be used in case of dispute. It is applicable whenever it is referenced in a definition document.

  • Standard
    11 pages
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    11 pages
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ISO
ISO 3353-2:2002(Main)
Aerospace — Lead and runout threads — Part 2: Internal threads

ISO 3353-2:2002 specifies the lead and runout thread and undercut requirements for internal threads (blind tapped holes) for aerospace construction. It is applicable whenever it is referenced in a definition document.

  • Standard
    4 pages
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    4 pages
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ISO
ISO 10959:2000(Main)
Aerospace — MJ threads — Gauging
  • Standard
    19 pages
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  • Standard
    20 pages
    French language
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ISO
ISO 3161:1996(Main)
Aerospace — UNJ threads, with controlled root radius, for aerospace — Inch series
  • Standard
    36 pages
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  • Standard
    36 pages
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ISO
ISO 3353:1992(Main)
Aerospace — Rolled threads for bolts — Lead and runout requirements

Specifies appropriate dimensions and the inspection method to be used in case of dispute.

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    9 pages
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    9 pages
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    9 pages
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ISO
ISO 5855-2:1988(Main)
Aerospace — MJ threads — Part 2: Limit dimensions for bolts and nuts
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    5 pages
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    5 pages
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ISO
ISO 5855-1:1988(Main)
Aerospace — MJ threads — Part 1: General requirements
  • Standard
    7 pages
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    7 pages
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ISO
ISO 5855-3:1988(Main)
Aerospace — MJ threads — Part 3: Limit dimensions for fittings for fluid systems
  • Standard
    6 pages
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    6 pages
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ISO
ISO 5855-2:1981(Main)
Aerospace construction — MJ threads — Part 2: Dimensions for bolts and nuts
  • Standard
    6 pages
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ISO
ISO 5855-1:1981(Main)
Aerospace construction — MJ threads — Part 1: Basic profile
  • Standard
    2 pages
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    2 pages
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ISO
ISO 3161:1977(Main)
UNJ threads, with controlled root radius, for aerospace — Inch series
  • Standard
    43 pages
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    43 pages
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ISO
ISO 3353:1976(Main)
Aerospace construction — Rolled threads — Runout and lead threads
  • Standard
    4 pages
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    4 pages
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