Aerospace series - Inserts, screw threads, helical coil, self-locking, tanged insertion drive, in heat resisting nickel base alloy NI-PH2801 (Inconel X750)

This document specifies the characteristics of inserts, self-locking, helical coil, tanged insertion drive, with MJ screw threads in NI-PH2801 material, for aerospace applications.
Maximum test temperature: 550 °C.

Luft- und Raumfahrt - Draht-Gewindeeinsätze, MJ-Gewinde, spriralförmig gewunden, selbstsichernd, Einsteckantrieb mit Zapfen, aus hochwarmfester Nickelbasislegierung NI-PH2801 (Inconel X750)

Série aérospatiale - Inserts, filets de vis MJ, bobine hélicoïdale, autobloquants, entraînement par insertion à brides, en alliage à base de nickel résistant à la chaleur NI-PH2801 (Inconel X750)

Aeronavtika - Vložki s spiralnim navojem, samozapiralni, za ročno vstavljanje, iz toplotno odporne zlitine na nikljevi osnovi Ni-PH2801 (Inconel X750)

General Information

Status
Not Published
Public Enquiry End Date
28-Feb-2022
Technical Committee
I13 - Imaginarni 13
Current Stage
4020 - Public enquire (PE) (Adopted Project)
Start Date
15-Dec-2021
Due Date
04-May-2022
Completion Date
01-Mar-2022

Relations

Effective Date
18-Jan-2023
Effective Date
01-Feb-2022

Overview

The oSIST prEN 3542:2022 standard specifies requirements for aerospace-grade inserts featuring self-locking, helical coil screw threads with a tanged insertion drive. These inserts are manufactured from the heat-resistant nickel base alloy NI-PH2801 (Inconel X750), known for its superior mechanical properties at elevated temperatures. Designed primarily for aerospace applications, these inserts support thread locking and durability under demanding conditions, with a maximum test temperature rating of 550 °C.

Produced and maintained by CEN through the Aerospace and Defence Industries Association of Europe (ASD-STAN), oSIST prEN 3542:2022 updates and supersedes EN 3542:2018, reflecting the latest technical advancements and requirements in aerospace fastening technology.

Key Topics

  • Insert Characteristics: The standard details configuration, dimensions, tolerances, and mass for inserts with MJ screw threads, ensuring consistent shape and performance.
  • Material Specification: Inserts must be made from NI-PH2801, a nickel-chromium-based heat-resistant alloy compliant with EN 3018, guaranteeing excellent high-temperature resistance and mechanical strength.
  • Self-locking Feature: The helical coil design includes an out-of-round zone to achieve self-locking without the use of additional locking elements, enhancing assembly reliability.
  • Tanged Insertion Drive: Inserts feature a tang as part of the installation drive, facilitating secure placement and ease of installation.
  • Marking and Designation: Compliance with EN 2424 for aerospace product marking ensures traceability and identification, using styles G and optionally F.
  • Technical Specifications: The inserts conform to EN 2943 for technical requirements and EN 3044 for installation hole design.
  • Quality Management: Manufacturers must operate under aerospace-approved quality management systems (e.g., EN 9100) and document qualification procedures as per EN 9133 or equivalent.

Applications

The oSIST prEN 3542:2022 standard applies to inserts used in critical aerospace components where high strength, heat resistance, and secure thread locking are essential. Typical applications include:

  • Engine and airframe assemblies requiring maintenance-friendly yet robust threaded connections.
  • High-temperature zones within aerospace components exposed to temperatures up to 550 °C.
  • Structures where vibration and thermal cycling require self-locking threads to prevent loosening.
  • Aerospace manufacturing and repair processes demanding standardized, certified fastening inserts.
  • Components requiring heat-resistant nickel alloy inserts for enhanced durability and reliability.

By adhering to oSIST prEN 3542:2022, aerospace manufacturers and suppliers can ensure consistent quality and performance of critical fastening elements that meet rigorous safety and performance standards.

Related Standards

oSIST prEN 3542:2022 references and aligns with several key aerospace standards to ensure comprehensive application and conformity:

  • EN 3018 – Defines the chemical and mechanical characteristics of the NI-PH2801 alloy used in insert manufacturing.
  • EN 2943 – Technical specifications for inserts with MJ and M screw threads, critical for ensuring insert compatibility and function.
  • EN 3044 – Provides guidelines for designing installation holes for self-locking, helical coil inserts.
  • EN 2424 – Specifies aerospace marking standards for product traceability and compliance.
  • EN 9100 – Aerospace quality management system requirements to ensure production reliability.
  • ISO 5855-2 – Dimensioning limits for MJ threads, aiding in specification consistency for bolts and nuts used with these inserts.
  • EN 9133 – Procedures for aerospace standard product qualification testing.

Summary

oSIST prEN 3542:2022 establishes a rigorous framework for the design, production, marking, and quality assurance of self-locking, helical coil aerospace inserts made from Inconel X750. This standard is essential for aerospace manufacturers seeking proven fastening solutions that withstand high temperatures and meet strict quality and safety requirements. Implementing oSIST prEN 3542:2022 supports reliability in critical aerospace assemblies, aligning with international best practices and ensuring compatibility across the aerospace supply chain.

Frequently Asked Questions

oSIST prEN 3542:2022 is a draft published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Inserts, screw threads, helical coil, self-locking, tanged insertion drive, in heat resisting nickel base alloy NI-PH2801 (Inconel X750)". This standard covers: This document specifies the characteristics of inserts, self-locking, helical coil, tanged insertion drive, with MJ screw threads in NI-PH2801 material, for aerospace applications. Maximum test temperature: 550 °C.

This document specifies the characteristics of inserts, self-locking, helical coil, tanged insertion drive, with MJ screw threads in NI-PH2801 material, for aerospace applications. Maximum test temperature: 550 °C.

oSIST prEN 3542:2022 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.

oSIST prEN 3542:2022 has the following relationships with other standards: It is inter standard links to SIST EN 3542:2018, SIST EN 3542:2018. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

You can purchase oSIST prEN 3542:2022 directly from iTeh Standards. The document is available in PDF format and is delivered instantly after payment. Add the standard to your cart and complete the secure checkout process. iTeh Standards is an authorized distributor of SIST standards.

Standards Content (Sample)


SLOVENSKI STANDARD
01-februar-2022
Aeronavtika - Vložki s spiralnim navojem, samozapiralni, vgrajeni pogon s tangenti
(tanged insertion drive ), iz toplotnoodporne zlitine na nikljevi osnovi Ni-PH2801
(Inconel X750)
Aerospace series - Inserts, screw threads, helical coil, self-locking, tanged insertion
drive, in heat resisting nickel base alloy NI-PH2801 (Inconel X750)
Luft- und Raumfahrt - Draht-Gewindeeinsätze, MJ-Gewinde, spriralförmig gewunden,
selbstsichernd, Einsteckantrieb mit Zapfen, aus hochwarmfester Nickelbasislegierung
NI-PH2801 (Inconel X750)
Série aérospatiale - Inserts, filets de vis MJ, bobine hélicoïdale, autobloquants,
entraînement par insertion à brides, en alliage à base de nickel résistant à la chaleur NI-
PH2801 (Inconel X750)
Ta slovenski standard je istoveten z: prEN 3542
ICS:
49.030.30 Matice Nuts
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

DRAFT
EUROPEAN STANDARD
NORME EUROPÉENNE
EUROPÄISCHE NORM
December 2021
ICS 49.030.30 Will supersede EN 3542:2018
English Version
Aerospace series - Inserts, screw threads, helical coil, self-
locking, tanged insertion drive, in heat resisting nickel
base alloy NI-PH2801 (Inconel X750)
Série aérospatiale - Inserts, filets de vis MJ, bobine Luft- und Raumfahrt - Draht-Gewindeeinsätze, MJ-
hélicoïdale, autobloquants, entraînement par insertion Gewinde, spriralförmig gewunden, selbstsichernd,
à brides, en alliage à base de nickel résistant à la Einsteckantrieb mit Zapfen, aus hochwarmfester
chaleur NI-PH2801 (Inconel X750) Nickelbasislegierung NI-PH2801 (Inconel X750)
This draft European Standard is submitted to CEN members for enquiry. It has been drawn up by the Technical Committee ASD-
STAN.
If this draft becomes a European Standard, 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.

This draft European Standard was established by CEN 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-CENELEC
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, Republic of North Macedonia, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and
United Kingdom.
Recipients of this draft are invited to submit, with their comments, notification of any relevant patent rights of which they are
aware and to provide supporting documentation.

Warning : This document is not a European Standard. It is distributed for review and comments. It is subject to change without
notice and shall not be referred to as a European Standard.

EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION

EUROPÄISCHES KOMITEE FÜR NORMUNG

CEN-CENELEC Management Centre: Rue de la Science 23, B-1040 Brussels
© 2021 CEN All rights of exploitation in any form and by any means reserved Ref. No. prEN 3542:2021 E
worldwide for CEN national Members.

Contents Page
European foreword . 3
Introduction . 4
1 Scope . 5
2 Normative references . 5
3 Terms and definitions . 5
4 Required characteristics . 5
4.1 Configuration — Dimensions — Tolerances — Masses . 5
4.2 Material . 7
4.3 Material identification . 7
5 Designation . 9
6 Marking . 9
7 Technical specification . 9
8 Quality management systems . 9
Bibliography . 10

European foreword
This document (prEN 3542:2021) has been prepared by the Aerospace and Defence Industries
Association of Europe — Standardization (ASD-STAN).
After enquiries and votes carried out in accordance with the rules of this Association, this document has
received the approval of the Nation
...

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