Aerospace — Nuts, anchor, self-locking, sealing, floating, two-lug, with counterbore, with MJ threads, classifications: 900 MPa (at ambient temperature)/120 degrees C, 900 MPa (at ambient temperature)/175 degrees C and 900 MPa (at ambient temperature)/235 degrees C — Dimensions

ISO 8940:2002 specifies the dimensions of self-locking, sealing, floating, two-lug anchor nuts, with counterbore, with MJ threads, for classifications: 900 MPa/120 °C, 900 MPa/175 °C and 900 MPa/235 °C. ISO 8940:2002 is only applicable for the compilation of aerospace product standards.

Aéronautique et espace — Écrous à river, à freinage interne, étanches, flottants, double patte, avec chambrage, à filetage MJ, classifications: 900 MPa (à température ambiante)/120 degrés C, 900 MPa (à température ambiante)/175 degrés C et 900 MPa (à température ambiante)/235 degrés C — Dimensions

L'ISO 8940:2002 spécifie les dimensions des écrous à river, à freinage interne, étanches, flottants, double patte, avec chambrage, à filetage MJ, de classifications: 900 MPa/120 °C, 900 MPa/175 °C et 900 MPa/235 °C. L'ISO 8940:2002 est uniquement destinée à l'élaboration de normes de produit applicables aux constructions aérospatiales.

General Information

Status
Published
Publication Date
28-Aug-2002
Current Stage
9093 - International Standard confirmed
Start Date
19-Oct-2021
Completion Date
14-Feb-2026

Relations

Effective Date
06-Jun-2022
Effective Date
15-Apr-2008

Overview

ISO 8940:2002 specifies the dimensions and basic characteristics of self-locking, sealing, floating, two-lug anchor nuts with counterbore and metric MJ threads for the aerospace industry. Developed by the International Organization for Standardization (ISO), this standard targets the compilation of aerospace product standards and addresses nuts classified by their performance under specific conditions: 900 MPa at ambient temperature with temperature ratings of 120°C, 175°C, and 235°C.

Complying with ISO 8940:2002 helps ensure compatibility, performance, and reliability of critical fastener components in demanding aerospace applications.

Key Topics

  • Product Scope: Defines anchor nuts that are self-locking, sealed, floating, and feature two lugs as well as a counterbore, using standardized MJ threads.
  • Classification: Details classifications based on tensile strength (900 MPa at ambient temperature) and three maximum temperature ratings (120°C, 175°C, 235°C).
  • Dimensions and Configuration: Specifies dimensions in millimetres and covers design features such as shell, seal, retainer, and threaded element. All tolerances are referenced to ISO 8788.
  • Compatibility: Ensures that parts manufactured according to this standard align with procurement specifications and interface seamlessly with other aerospace fastener standards, specifically ISO 5858 and ISO 5855-2.
  • Manufacturing Considerations: Allows manufacturers discretion in certain form details where not explicitly defined, enabling flexibility while maintaining interchangeability.

Applications

ISO 8940:2002 is essential in the design, manufacture, and specification of anchor nuts for aerospace fastener systems, particularly where high performance and operational reliability are critical. Practical applications include:

  • Aircraft and Spacecraft Assembly: Providing secure, vibration-resistant joints in primary and secondary structures.
  • Component Integration: Used in situations requiring floating nuts that accommodate minor misalignment, frequent disassembly, or tight sealing requirements.
  • Maintenance and Repair: Allowing for consistent replacement or retrofit in line with international aerospace product standards.
  • Product Standardization: Serving as a reference for drafting and evaluating technical requirements in aerospace procurement documentation.

Using anchor nuts that comply with ISO 8940:2002 ensures standardization, which simplifies logistics, improves safety, and supports international collaboration among aerospace manufacturers and suppliers.

Related Standards

Organizations following ISO 8940:2002 should also consider these relevant standards:

  • ISO 5855-2:1999: Aerospace - MJ threads - Part 2: Limit dimensions for bolts and nuts
  • ISO 8788:2000: Aerospace - Nuts, metric - Tolerances of form and position
  • ISO 5858:1999: Aerospace - Nuts, self-locking, with maximum operating temperature less than or equal to 425°C - Procurement specification
  • ISO 13715:2000: Technical drawings - Edges of undefined shape - Vocabulary and indications

Conclusion

Implementing ISO 8940:2002 for anchor nuts in aerospace projects supports the highest levels of product quality, consistency, and safety. By adhering to internationally recognized dimensions and classifications, manufacturers and suppliers facilitate better integration, streamlined procurement, and enhanced reliability in the demanding aerospace sector.

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Standard

ISO 8940:2002 - Aerospace — Nuts, anchor, self-locking, sealing, floating, two-lug, with counterbore, with MJ threads, classifications: 900 MPa (at ambient temperature)/120 degrees C, 900 MPa (at ambient temperature)/175 degrees C and 900 MPa (at ambient temperature)/235 degrees C — Dimensions Released:8/29/2002

English language (4 pages)
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Standard

ISO 8940:2002 - Aéronautique et espace — Écrous a river, a freinage interne, étanches, flottants, double patte, avec chambrage, a filetage MJ, classifications: 900 MPa (a température ambiante)/120 degrés C, 900 MPa (a température ambiante)/175 degrés C et 900 MPa (a température ambiante)/235 degrés C — Dimensions Released:8/29/2002

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Frequently Asked Questions

ISO 8940:2002 is a standard published by the International Organization for Standardization (ISO). Its full title is "Aerospace — Nuts, anchor, self-locking, sealing, floating, two-lug, with counterbore, with MJ threads, classifications: 900 MPa (at ambient temperature)/120 degrees C, 900 MPa (at ambient temperature)/175 degrees C and 900 MPa (at ambient temperature)/235 degrees C — Dimensions". This standard covers: ISO 8940:2002 specifies the dimensions of self-locking, sealing, floating, two-lug anchor nuts, with counterbore, with MJ threads, for classifications: 900 MPa/120 °C, 900 MPa/175 °C and 900 MPa/235 °C. ISO 8940:2002 is only applicable for the compilation of aerospace product standards.

ISO 8940:2002 specifies the dimensions of self-locking, sealing, floating, two-lug anchor nuts, with counterbore, with MJ threads, for classifications: 900 MPa/120 °C, 900 MPa/175 °C and 900 MPa/235 °C. ISO 8940:2002 is only applicable for the compilation of aerospace product standards.

ISO 8940:2002 is classified under the following ICS (International Classification for Standards) categories: 49.030.30 - Nuts. The ICS classification helps identify the subject area and facilitates finding related standards.

ISO 8940:2002 has the following relationships with other standards: It is inter standard links to ISO 4628-8:2012, ISO 8940:1988. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

ISO 8940:2002 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.

Standards Content (Sample)


INTERNATIONAL ISO
STANDARD 8940
Second edition
2002-08-01
Aerospace — Nuts, anchor, self-locking,
sealing, floating, two-lug, with counterbore,
with MJ threads, classifications: 900 MPa
(at ambient temperature)/120 °C, 900 MPa
(at ambient temperature)/175 °C and
900 MPa (at ambient temperature)/235 °C —
Dimensions
Aéronautique et espace — Écrous à river, à freinage interne, étanches,
flottants, double patte, avec chambrage, à filetage MJ, classifications:
900 MPa (à température ambiante)/120 °C, 900 MPa (à température
ambiante)/175 °C et 900 MPa (à température ambiante)/235 °C —
Dimensions
Reference number
©
ISO 2002
PDF disclaimer
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©  ISO 2002
All rights reserved. Unless otherwise specified, no part of this publication may be reproduced or utilized in any form or by any means, electronic
or mechanical, including photocopying and microfilm, without permission in writing from either ISO at the address below or ISO's member body
in the country of the requester.
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ii © ISO 2002 – All rights reserved

Foreword
ISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO
member bodies). The work of preparing International Standards is normally carried out through ISO technical
committees. Each member body interested in a subject for which a technical committee has been established has
the right to be represented on that committee. International organizations, governmental and non-governmental, in
liaison with ISO, also take part in the work. ISO collaborates closely with the International Electrotechnical
Commission (IEC) on all matters of electrotechnical standardization.
International Standards are drafted in accordance with the rules given in the ISO/IEC Directives, Part 3.
The main task of technical committees is to prepare International Standards. Draft International Standards adopted
by the technical committees are circulated to the member bodies for voting. Publication as an International
Standard requires approval by at least 75 % of the member bodies casting a vote.
Attention is drawn to the possibility that some of the elements of this International Standard may be the subject of
patent rights. ISO shall not be held responsible for identifying any or all such patent rights.
ISO 8940 was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 4,
Aerospace fastener systems.
This second edition cancels and replaces the first edition (ISO 8940:1988), which has been technically revised.

Introduction
The dimensions specified in this International Standard have been determined to allow production of a part which
will satisfy the requirements of the procurement specification ISO 5858.

iv © ISO 2002 – All rights reserved

INTER
...


NORME ISO
INTERNATIONALE 8940
Deuxième édition
2002-08-01
Aéronautique et espace — Écrous à river, à
freinage interne, étanches, flottants, double
patte, avec chambrage, à filetage MJ,
classifications: 900 MPa (à température
ambiante)/120 °C, 900 MPa (à température
ambiante)/175 °C et 900 MPa (à température
ambiante)/235 °C — Dimensions
Aerospace — Nuts, anchor, self-locking, sealing, floating, two-lug, with
counterbore, with MJ threads, classifications: 900 MPa (at ambient
temperature)/120 °C, 900 MPa (at ambient temperature)/175 °C and
900 MPa (at ambient temperature)/235 °C — Dimensions

Numéro de référence
©
ISO 2002
PDF – Exonération de responsabilité
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©  ISO 2002
Droits de reproduction réservés. Sauf prescription différente, aucune partie de cette publication ne peut être reproduite ni utilisée sous quelque
forme que ce soit et par aucun procédé, électronique ou mécanique, y compris la photocopie et les microfilms, sans l'accord écrit de l’ISO à
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Tel. + 41 22 749 01 11
Fax. + 41 22 749 09 47
E-mail copyright@iso.ch
Web www.iso.ch
Imprimé en Suisse
ii © ISO 2002 – Tous droits réservés

Avant-propos
L'ISO (Organisation internationale de normalisation) est une fédération mondiale d'organismes nationaux de
normalisation (comités membres de l'ISO). L'élaboration des Normes internationales est en général confiée aux
comités techniques de l'ISO. Chaque comité membre intéressé par une étude a le droit de faire partie du comité
technique créé à cet effet. Les organisations internationales, gouvernementales et non gouvernementales, en
liaison avec l'ISO participent également aux travaux. L'ISO collabore étroitement avec la Commission
électrotechnique internationale (CEI) en ce qui concerne la normalisation électrotechnique.
Les Normes internationales sont rédigées conformément aux règles données dans les Directives ISO/CEI,
Partie 3.
La tâche principale des comités techniques est d'élaborer les Normes internationales. Les projets de Normes
internationales adoptés par les comités techniques sont soumis aux comités membres pour vote. Leur publication
comme Normes internationales requiert l'approbation de 75 % au moins des comités membres votants.
L'attention est appelée sur le fait que certains des éléments de la présente Norme internationale peuvent faire
l'objet de droits de propriété intellectuelle ou de droits analogues. L'ISO ne saurait être tenue pour responsable de
ne pas avoir identifié de tels droits de propriété et averti de leur existence.
L'ISO 8940 a été élaborée par le comité technique ISO/TC 20, Aéronautique et espace, sous-comité SC 4,
Éléments de fixation pour constructions aérospatiales.
Cette deuxième édition annule et remplace la première édition (ISO 8940:1988), dont elle constitue une révision
technique.
Introduction
Les dimensions spécifiées dans la présente Norme internationale ont été définies pour permettre la production
d’une pièce satisfaisant aux exigences de la spécification d’approvisionnement ISO 5858.

iv © ISO 2002 – Tous
...

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