SIST EN 4128:2026
(Main)Aerospace series - Bolt, normal hexagonal head, coarse tolerance shank, short 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 shank, short 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 shank, short thread, in heat resisting nickel base alloy, aluminium IVD coated.
Classification: 1 250 MPa/425 °C.
Luft- und Raumfahrt - Sechskantschrauben, kurzes Gewinde, aus hochwarmfester Nickelbasislegierung, Aluminium-IVD-beschichtet - Klasse: 1 250 MPa (bei Raumtemperatur)/425 °C
Série aérospatiale - Vis à tête hexagonale normale, fût à tolérance large, filetage court, 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, fût à tolérance large, filetage court, en alliage résistant à chaud base nickel, revêtues d'aluminium IVD.
Classification : 1 250 MPa/425 °C.
Aeronavtika - Sornik, normalna šestroba glava, široka toleranca, kratek navoj, iz toplotnoodporne zlitine na nikljevi osnovi, prevlečeni z aluminijem IVD - Klasifikacija: 1250 MPa (pri temperaturi okolice)/425 °C
General Information
- Status
- Published
- Public Enquiry End Date
- 05-May-2024
- Publication Date
- 15-Mar-2026
- Technical Committee
- I13 - Imaginarni 13
- Current Stage
- 6060 - National Implementation/Publication (Adopted Project)
- Start Date
- 05-Mar-2026
- Due Date
- 10-May-2026
- Completion Date
- 16-Mar-2026
Relations
- Effective Date
- 19-Jan-2023
Overview
FprEN 4128 is a draft CEN/AeroSpace standard that specifies the characteristics of aerospace series bolts with a normal hexagonal head, coarse-tolerance shank and short thread, manufactured from a heat‑resisting nickel‑base alloy and aluminium IVD coated. The bolts are classified for a minimum tensile strength of 1 250 MPa (ambient) and rated to 425 °C (maximum temperature determined by the surface treatment). This standard defines geometry, materials, surface treatment, marking, and qualification requirements for fasteners used in high‑temperature aerospace applications.
Key topics and technical requirements
- Configuration & dimensions: Dimensions, tolerances and masses conform to ISO 3193 and ISO 5855‑2; sizes use MJ thread codes and are expressed in millimetres (values apply after surface treatment but before lubrication).
- Material: Heat‑resisting nickel‑base alloy per TR 3775, strength class 1 250 MPa.
- Surface treatment: Aluminium IVD coating requirements are referenced to prEN 6118; optional lubrication with cetyl alcohol per prEN 6117 (code E).
- Mechanical properties: Minimum hardness 36 HRC; detailed tensile, shear and fatigue performance by diameter are specified (see Table 5 in the standard).
- Roughness limits: Threads Ramax = 0.8 µm; bearing surfaces Ramax = 1.6 µm; other surfaces Ramax = 3.2 µm (values before surface treatment).
- Marking & holes: Marking follows EN 2424; hole codes for lockwire/split pin options are defined.
- Manufacturer & qualification: Producers must be an approved aerospace production organization with a quality management system (e.g. EN 9100) and follow qualification/testing protocols (ISO 9154 / EN 9133 guidance).
Applications and who uses this standard
- Primary use: High‑temperature aerospace structures and propulsion systems where fasteners must retain strength and corrosion resistance up to 425 °C.
- Typical users: Aerospace design engineers, procurement/specification specialists, fastener manufacturers, quality and certification teams, MRO organisations and OEM supply chain managers.
- Benefits: Ensures interchangeability, consistent mechanical performance, traceability and compatibility with aerospace quality systems for critical high‑temperature bolting applications.
Related standards
- ISO 3193, ISO 5855‑2 (dimensions/threads)
- TR 3775 (materials)
- prEN 6118, prEN 6117 (surface protection and lubrication)
- ISO 9154 (procurement of nickel‑alloy bolts)
- EN 2424 (marking)
- EN 9100, EN 9133 (quality and qualification procedures)
- ISO 3353‑1, ISO 7913, MIL‑DTL‑83488 (coatings/threads/quality references)
Keywords: FprEN 4128, aerospace bolts, hexagonal head bolt, nickel base alloy, aluminium IVD coating, 1250 MPa, 425 °C, aerospace standard, short thread bolt.
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Frequently Asked Questions
SIST EN 4128:2026 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Bolt, normal hexagonal head, coarse tolerance shank, short 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 shank, short 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 shank, short thread, in heat resisting nickel base alloy, aluminium IVD coated. Classification: 1 250 MPa/425 °C.
SIST EN 4128:2026 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.
SIST EN 4128:2026 has the following relationships with other standards: It is inter standard links to SIST EN 4128:2016. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
SIST EN 4128:2026 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-april-2026
Aeronavtika - Sornik, normalna šestroba glava, široka toleranca, kratek navoj, iz
toplotnoodporne zlitine na nikljevi osnovi, prevlečeni z aluminijem IVD -
Klasifikacija: 1250 MPa (pri temperaturi okolice)/425 °C
Aerospace series - Bolt, normal hexagonal head, coarse tolerance shank, short thread,
in heat resisting nickel base alloy, aluminium IVD coated - Classification: 1 250 MPa (at
ambient temperature)/425 °C
Luft- und Raumfahrt - Sechskantschrauben, kurzes Gewinde, aus hochwarmfester
Nickelbasislegierung, Aluminium-IVD-beschichtet - Klasse: 1 250 MPa (bei
Raumtemperatur)/425 °C
Série aérospatiale - Vis à tête hexagonale normale, fût à tolérance large, filetage court,
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: EN 4128:2026
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.
EN 4128
EUROPEAN STANDARD
NORME EUROPÉENNE
February 2026
EUROPÄISCHE NORM
ICS 49.030.20 Supersedes EN 4128:2016
English Version
Aerospace series - Bolt, normal hexagonal head, coarse
tolerance shank, short 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, fût à Luft- und Raumfahrt - Sechskantschraube, kurzes
tolérance large, filetage court, en alliage résistant à Gewinde, aus hochwarmfester Nickelbasislegierung,
chaud base nickel, revêtue d'aluminium IVD - Aluminium-IVD-beschichtet - Klasse: 1 250 MPa (bei
Classification : 1 250 MPa (à température Raumtemperatur)/425 °C
ambiante)/425 °C
This European Standard was approved by CEN on 25 May 2025.
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-CENELEC 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-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.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
CEN-CENELEC Management Centre: Rue de la Science 23, B-1040 Brussels
© 2026 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4128:2026 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 . 5
4.1 Configuration – Dimensions – Masses . 5
4.2 Materials . 5
4.3 Surface treatment . 5
5 Designation . 7
6 Marking . 7
7 Technical specification . 7
7.1 General. 7
7.2 Approval of manufacturers . 7
7.3 Qualification of bolts. 8
Bibliography . 9
European foreword
This document (EN 4128:2026) 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 European Standard shall be given the status of a national standard, either by publication of an
identical text or by endorsement, at the latest by August 2026, and conflicting national standards shall be
withdrawn at the latest by August 2026.
Attention is drawn to the possibility that some of the elements of this document may be the subject of
patent rights. CEN shall not be held responsible for identifying any or all such patent rights.
This document supersedes EN 4128:2016.
This document includes the following significant technical changes with respect to EN 4128:2016:
— normative references updated;
— Clause 3 “Terms and definitions” added;
— Figure 1, roughness deleted;
— 7.2 and 7.3 revised;
— Bibliography updated.
Any feedback and questions on this document should be directed to the users’ national standards body.
A complete listing of these bodies can be found on the CEN website.
According to the CEN-CENELEC Internal Regulations, the national standards organizations of the
following countries are bound to implement this European Standard: 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 the United
Kingdom.
1 Scope
This document specifies the characteristics of bolts, normal hexagonal head, coarse tolerance shank,
short 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
constitutes requirements of this document. For d
...




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