oSIST prEN 4131:2025
(Main)Aerospace series - Bolt, normal hexagonal head, coarse tolerance normal shank, medium length thread, in heat resisting nickel base alloy, aluminium IVD coated - Classification: 1 250 MPa (at ambient temperature) / 425 °C
Aerospace series - Bolt, normal hexagonal head, coarse tolerance normal shank, medium length thread, in heat resisting nickel base alloy, aluminium IVD coated - Classification: 1 250 MPa (at ambient temperature) / 425 °C
This document specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in heat resisting nickel base alloy, aluminium IVD coated.
Classification: 1 250 MPa / 425 °C
Luft- und Raumfahrt - Sechskantschraube, mittlere Gewindelänge, aus hochwarmfester Nickelbasislegierung, Aluminium‑IVD‑beschichtet - Klasse: 1 250 MPa (bei Raumtemperatur)/425 °C
Dieses Dokument legt Eigenschaften von Sechskantschrauben mit mittlerer Gewindelänge aus hochwarmfester Nickelbasislegierung, Aluminium IVD-beschichtet, fest.
Klasse: 1 250 MPa /425 °C .
Série aérospatiale - Vis à tête hexagonale normale, tige normale à tolérance large, filetage moyen, en alliage résistant à chaud à base de nickel, revêtues aluminium IVD - Classification: 1 250 MPa (à température ambiante) / 425 °C
Le présent document spécifie les caractéristiques des vis à tête hexagonale normale, tige à tolérance large, filetage moyen, en alliage résistant à chaud base nickel, revêtues d'aluminium IVD.
Classification : 1 250 MPa /425 °C.
Aeronavtika - Sorniki, normalna šestroba glava, široka toleranca, srednja navojna dolžina, iz toplotnoodporne zlitine na nikljevi osnovi, prevlečene z aluminijem IVD - Klasifikacija: 1 250 MPa (pri temperaturi okolice)/425 °C
General Information
- Status
- Not Published
- Public Enquiry End Date
- 22-Oct-2025
- Technical Committee
- I13 - Imaginarni 13
- Current Stage
- 4020 - Public enquire (PE) (Adopted Project)
- Start Date
- 19-Aug-2025
- Due Date
- 06-Jan-2026
- Completion Date
- 23-Oct-2025
Relations
- Effective Date
- 12-Feb-2025
- Effective Date
- 12-Feb-2025
Overview
prEN 4131:2025 (draft) specifies requirements for an aerospace-series bolt: normal hexagonal head, coarse tolerance normal shank, medium length MJ thread, manufactured from a heat-resisting nickel‑base alloy and aluminium IVD coated. The fastener classification is 1 250 MPa (minimum tensile strength at ambient temperature) with an elevated temperature capability up to 425 °C (maximum service temperature influenced by surface treatment). This document is intended for use in aerospace applications where high strength and heat resistance are required.
Key topics and technical requirements
- Material and strength
- Material to comply with EN 2952, EN 3219 or TR 3775 (heat‑resisting nickel‑base alloys, classification 1 250 MPa).
- Mechanical classification
- Minimum tensile strength: 1 250 MPa at ambient temperature.
- Maximum temperature capability: 425 °C (surface treatment dependent).
- Dimensions and threads
- Dimensions and masses according to ISO 3193 (MJ threads), with sizes and length codes listed in the standard’s tables.
- Thread form and lead/runout conform to ISO 3353‑1; MJ thread limits per ISO 5855‑2.
- Tolerances and form
- Tolerances of form and position per ISO 7913.
- Dimensions specified apply after surface treatment.
- Surface treatment
- Aluminium IVD coating in accordance with MIL‑DTL‑83488D, Type II, Class 3, with deposit thickness 7–20 µm.
- Post‑treatment: mechanical blasting, chromate conversion coating within 24 h, optional lubrication using cethylic alcohol (code E).
- Configuration, marking and holes
- Hex head configuration, hole codes (lockwire, split pin, etc.) and product marking per EN 2424 and the standard’s tables.
- Quality and qualification
- Manufacturer approval: approved aerospace production organization with an aerospace quality management system (e.g., EN 9100).
- Product qualification per aerospace procedures (e.g., EN 9133); technical specification aligned with EN 2583.
Applications and users
- Designed for aerospace structural and engine components requiring high strength and high‑temperature performance.
- Primary users:
- Aerospace design and structural engineers
- Fastener manufacturers and heat‑treatment suppliers
- Procurement and quality managers in aviation, space and defence
- Certification and maintenance organizations specifying approved hardware
- Typical applications: turbine housings, high‑temperature brackets, airframe locations exposed to elevated temperatures where nickel‑base alloy bolts and aluminium IVD coating are specified.
Related standards
- EN 2952, EN 3219, TR 3775 (materials)
- ISO 3193, ISO 3353‑1, ISO 5855‑2, ISO 7913 (dimensions, threads, tolerances)
- MIL‑DTL‑83488D (aluminium coating)
- EN 2424 (marking), EN 2583 (technical specification), EN 9100, EN 9133 (quality/qualification)
Keywords: prEN 4131, aerospace bolt, nickel base alloy, aluminium IVD coated, hexagonal head bolt, MJ thread, 1250 MPa, 425 °C, aerospace fasteners, MIL‑DTL‑83488D.
Frequently Asked Questions
oSIST prEN 4131:2025 is a draft published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Bolt, normal hexagonal head, coarse tolerance normal shank, medium length thread, in heat resisting nickel base alloy, aluminium IVD coated - Classification: 1 250 MPa (at ambient temperature) / 425 °C". This standard covers: This document specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in heat resisting nickel base alloy, aluminium IVD coated. Classification: 1 250 MPa / 425 °C
This document specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in heat resisting nickel base alloy, aluminium IVD coated. Classification: 1 250 MPa / 425 °C
oSIST prEN 4131:2025 is classified under the following ICS (International Classification for Standards) categories: 49.025.20 - Aluminium; 49.030.20 - Bolts, screws, studs. The ICS classification helps identify the subject area and facilitates finding related standards.
oSIST prEN 4131:2025 has the following relationships with other standards: It is inter standard links to SIST EN 4131:2009, SIST EN 4131:2009/AC:2010. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
oSIST prEN 4131:2025 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)
SLOVENSKI STANDARD
01-oktober-2025
Aeronavtika - Sorniki, normalna šestroba glava, široka toleranca, srednja navojna
dolžina, iz toplotnoodporne zlitine na nikljevi osnovi, prevlečene z aluminijem IVD -
Klasifikacija: 1 250 MPa (pri temperaturi okolice)/425 °C
Aerospace series - Bolt, normal hexagonal head, coarse tolerance normal shank,
medium length thread, in heat resisting nickel base alloy, aluminium IVD coated -
Classification: 1 250 MPa (at ambient temperature) / 425 °C
Luft- und Raumfahrt - Sechskantschraube, mittlere Gewindelänge, aus hochwarmfester
Nickelbasislegierung, Aluminium‑IVD‑beschichtet - Klasse: 1 250 MPa (bei
Raumtemperatur)/425 °C
Série aérospatiale - Vis à tête hexagonale normale, tige normale à tolérance large,
filetage moyen, en alliage résistant à chaud à base de nickel, revêtues aluminium IVD -
Classification: 1 250 MPa (à température ambiante) / 425 °C
Ta slovenski standard je istoveten z: prEN 4131
ICS:
49.025.20 Aluminij Aluminium
49.030.20 Sorniki, vijaki, stebelni vijaki Bolts, screws, studs
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
DRAFT
EUROPEAN STANDARD
NORME EUROPÉENNE
EUROPÄISCHE NORM
July 2025
ICS 49.030.20 Will supersede EN 4131:2009
English Version
Aerospace series - Bolt, normal hexagonal head, coarse
tolerance normal shank, medium length thread, in heat
resisting nickel base alloy, aluminium IVD coated -
Classification: 1 250 MPa (at ambient temperature) / 425
°C
Série aérospatiale - Vis à tête hexagonale normale, tige Luft- und Raumfahrt - Sechskantschraube, mittlere
normale à tolérance large, filetage moyen, en alliage Gewindelänge, aus hochwarmfester
résistant à chaud à base de nickel, revêtues aluminium Nickelbasislegierung, Aluminium-IVD-beschichtet -
IVD - Classification: 1 250 MPa (à température Klasse: 1 250 MPa (bei Raumtemperatur)/425 °C
ambiante) / 425 °C
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, Türkiye 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
© 2025 CEN All rights of exploitation in any form and by any means reserved Ref. No. prEN 4131:2025 E
worldwide for CEN national Members.
Contents Page
European foreword . 3
1 Scope . 4
2 Normative references . 4
3 Terms and definitions . 4
4 Required characteristics . 4
4.1 Configuration — Dimensions — Masses . 4
4.2 Tolerances of form and position . 5
4.3 Materials . 5
4.4 Surface treatment . 5
5 Designation . 8
6 Marking . 8
7 Technical specification . 9
7.1 General. 9
7.2 Approval of manufacturers . 9
7.3 Qualification of bolts. 9
Bibliography . 10
European foreword
This document (prEN 4131:2025) has been prepared by ASD-STAN.
After enquiries and votes carried out in accordance with the rules of this Association, this document has
received the approval of the National Associations and the Official Services of the member countries of
ASD-STAN, prior to its presentation to CEN.
This document is currently submitted to the CEN Enquiry.
This document will supersede EN 4131:2009/AC:2010.
EN 4131:2009/AC:2010:
— Clause 2, Normative references, has been updated;
— Clause 3, Terms and definitions, added;
— Table 3 has been updated with new drive code references;
— the technical specification has been changed to EN 2583;
— subclause 7.4, Other modified requirement, has been updated.
1 Scope
This document specifies the characteristics of bolts, normal hexagonal head, coarse tolerance normal
shank, medium length thread, in heat resisting nickel base alloy, aluminium IVD coated.
1 2
Classification: 1 250 MPa / 425 °C
2 Normative references
The following documents are referred to in the text in such a way that some or all of their content
...










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