Aerospace series - Nuts, anchor, self-locking, one lug, fixed, with counterbore, in heat resisting steel, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C

This standard specifies the characteristics of one lug counterbored fixed anchor nuts, with a self locking feature achieved by forming the upper portion out-of-round, in heat resisting steel, MoS2 lubricated.
Classification: 1 100 MPa / 315 °C.

Luft- und Raumfahrt - Annietmuttern, selbstsichernd, einseitiger Flansch, mit zylindrischer Aussenkung, aus hochwarmfestem Stahl, MoS2-geschmiert - Klasse: 1100 MPa (bei Raumtemperatur)/315 °C

Diese Norm legt die Merkmale von Annietmuttern mit zylindrischer Aussenkung und einseitigem Flansch, selbstsichernd durch ovale Formgebung des oberen Teils, aus hochwarmfestem Stahl, MoS2-geschmiert, fest.
Klasse: 1 100 MPa )/ 315 °C )

Série aérospatiale - Écrous à river, à freinage interne, fixes, simple patte, avec chambrage, en acier résistant à chaud, lubrifiés MoS2 - Classification: 1100 MPa (à température ambiante)/315 °C

Aeronavtika - Zakovne matice, samovarovalne, enostranske, fiksne, z izvrtino za valjaste vijake, iz toplotnoodpornega jekla, mazane z MoS2 - Klasifikacija: 1100 MPa (pri temperaturi okolice)/315 °C

Ta standard določa značilnosti enostranskih fiksnih zakovnih matic, z izvrtino za vijake, s samozapiranjem, ki je omogočeno tako, da je zgornji del oblikovan ovalno, iz toplotnoodpornega jekla, mazanih z MoS2. Klasifikacija: 1.100 MPa (pri temperaturi okolice)/315 °C.

General Information

Status
Published
Publication Date
07-Mar-2010
ICS
49.030.30 - Nuts
Technical Committee
I13 - Imaginarni 13
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
01-Mar-2010
Due Date
06-May-2010
Completion Date
08-Mar-2010
Ref Project
EN 3539:2010 - Aerospace series - Nuts, anchor, self-locking, one lug, fixed, with counterbore, in heat resisting steel, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature) / 315 °C

Overview

SIST EN 3539:2010 is a European standard developed by CEN, specifying requirements for aerospace series anchor nuts that are self-locking, fixed, and feature a one lug design with a counterbore. These nuts are manufactured from heat resisting steel and are lubricated with molybdenum disulphide (MoS2) to withstand elevated temperatures. The standard classifies these nuts for strength at 1,100 MPa at ambient temperature and operational temperature resistance up to 315 °C.

This standard is critical in aerospace and defense industries for ensuring the reliability and safety of threaded fasteners that operate under demanding mechanical and thermal conditions. It harmonizes specifications, dimensions, materials, and performance criteria for these specialized nuts, supporting international compatibility and quality assurance.

Key Topics

  • Scope and Application
    Defines characteristics, materials, lubrication, and performance for one lug counterbored fixed anchor nuts designed with a self-locking feature via an out-of-round upper portion.

  • Material Specifications
    Utilizes heat resisting steels complying with EN 2398, EN 2399, EN 3638, or EN 3639, providing high tensile strength and thermal resistance.

  • Lubrication
    MoS2 (molybdenum disulphide) coating ensures reduced friction and wear at high temperatures, maintaining locking performance.

  • Mechanical Classification
    Nuts are capable of withstanding 1,100 MPa tensile strength at room temperature, aligning with aerospace bolt strength classes.

  • Temperature Rating
    Certified to endure up to 315 °C without losing mechanical or locking properties, critical for aerospace environments.

  • Dimensional and Form Tolerances
    Follows ISO 3168 and ISO 8788 standards for geometric accuracy, thread dimensions, and form tolerances to ensure compatibility and performance.

  • Marking and Traceability
    Requires standardized marking per EN 2424 for product identification and quality control.

  • Compliance and Quality Management
    Manufacturers must meet EN 9100 quality management system requirements and product qualification rules under EN 9133.

Applications

SIST EN 3539:2010 nuts are specifically designed for:

  • Aerospace Fastening Systems
    Used in aircraft, spacecraft, and related defense equipment where high mechanical loads and thermal exposure occur.

  • High-Temperature Environments
    Suitable for assembly points experiencing sustained temperatures up to 315 °C, such as engine mounts and exhaust systems.

  • Self-Locking Assembly
    Ensures secure fastening in vibration-intensive and harsh service conditions without additional locking components.

  • Maintenance and Repair
    Conforms to international aerospace standards, enabling interchangeability and maintenance efficiency in aviation platforms.

Related Standards

  • EN 2398 / EN 2399 / EN 3638 / EN 3639
    Define the heat resisting steel materials used for fasteners.

  • EN 2491
    Specifies MoS2 dry lubricant coating methods for aerospace parts.

  • ISO 3168
    Provides dimensions and thread specifications for similar aerospace nuts.

  • EN 2424
    Covers marking standards for aerospace products to ensure traceability.

  • EN 9100 / EN 9133
    Standards for quality management systems and qualification procedures for aerospace standard parts.

  • ISO 5855-2 / ISO 5858 / ISO 8788
    Govern thread dimensions, procurement specifications, and tolerances for aerospace nuts and bolts.

By adhering to SIST EN 3539:2010, aerospace manufacturers and suppliers guarantee the delivery of high-quality, durable, and precisely engineered self-locking nuts that meet stringent thermal and mechanical requirements essential for safe and reliable aerospace assemblies.

Frequently Asked Questions

SIST EN 3539:2010 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Nuts, anchor, self-locking, one lug, fixed, with counterbore, in heat resisting steel, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C". This standard covers: This standard specifies the characteristics of one lug counterbored fixed anchor nuts, with a self locking feature achieved by forming the upper portion out-of-round, in heat resisting steel, MoS2 lubricated. Classification: 1 100 MPa / 315 °C.

This standard specifies the characteristics of one lug counterbored fixed anchor nuts, with a self locking feature achieved by forming the upper portion out-of-round, in heat resisting steel, MoS2 lubricated. Classification: 1 100 MPa / 315 °C.

SIST EN 3539:2010 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.

SIST EN 3539:2010 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)


2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aeronavtika - Zakovne matice, samovarovalne, enostranske, fiksne, z izvrtino za valjaste vijake, iz toplotnoodpornega jekla, mazane z MoS2 - Klasifikacija: 1100 MPa (pri temperaturi okolice)/315 °CLuft- und Raumfahrt - Annietmuttern, selbstsichernd, einseitiger Flansch, mit zylindrischer Aussenkung, aus hochwarmfestem Stahl, MoS2-geschmiert - Klasse: 1100
MPa (bei Raumtemperatur)/315 °CSérie aérospatiale - Écrous à river, à freinage interne, fixes, simple patte, avec chambrage, en acier résistant à chaud, lubrifiés MoS2 - Classification: 1100 MPa (à température ambiante)/315 °CAerospace series - Nuts, anchor, self-locking, one lug, fixed, with counterbore, in heat resisting steel, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C49.030.30MaticeNutsICS:Ta slovenski standard je istoveten z:EN 3539:2010SIST EN 3539:2010en,de01-april-2010SIST EN 3539:2010SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 3539
February 2010 ICS 49.030.30 English Version
Aerospace series - Nuts, anchor, self-locking, one lug, fixed, with counterbore, in heat resisting steel,
MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature) / 315 °C
Série aérospatiale - Écrous à river, à freinage interne, fixes, simple patte, avec chambrage, en acier résistant à chaud, lubrifiés MoS2 - Classification : 1 100 MPa (à température ambiante) / 315 °C
Luft- und Raumfahrt - Annietmuttern, selbstsichernd, einseitiger Flansch, mit zylindrischer Aussenkung, aus hochwarmfestem Stahl,
MoS2-geschmiert - Klasse: 1 100
MPa (bei Raumtemperatur) / 315 °C This European Standard was approved by CEN on 18 December 2009.
CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN Management Centre or to any CEN member.
This European Standard exists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN Management Centre has the same status as the official versions.
CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre:
Avenue Marnix 17,
B-1000 Brussels © 2010 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3539:2010: ESIST EN 3539:2010
...

Questions, Comments and Discussion

Ask us and Technical Secretary will try to provide an answer. You can facilitate discussion about the standard in here.

Loading comments...