Aerospace series - Bolt, normal hexagon head, relieved shank, long thread, in heat resisting steel FE-PA2601 (A286), silver plated - Classification: 1 100 MPa/650 °C

This document specifies the characteristics of silver-plated Bolts normal Hexagon Head with relieved shank and long thread, in heat resisting steel FE-PA92HT (A286), tensile strength class 1 100 MPa at room temperature. The maximum test temperature of the material is 650 °C.

Luft- und Raumfahrt - Sechskantschraube, Dünnschaft, langes Gewinde, aus hochwarmfestem Stahl FE-PA2601 (A286), versilbert - Klasse: 1 100 MPa/650 °C

Dieses Dokument legt die Eigenschaften von Sechskantschrauben mit Dünnschaft und langem Gewinde aus hochwarmfestem Stahl FE-PA2601 (A286), versilbert, Zugfestigkeitsklasse 1 100 MPa bei Raumtemperatur, fest. Die maximale Prüftemperatur des Werkstoffes beträgt 650 °C.

Série aérospatiale - Vis à tête hexagonale normale, tige dégagée, filetage long, en acier résistant à chaud FE-PA2601 (A286), argentées - Classification : 1 100 MPa/650 °C

Le présent document spécifie les caractéristiques des vis argentées, à tête hexagonale normale, tige dégagée, filetage long, en acier résistant à chaud FE-PA2601 (A286), de classe de résistance à la traction de 1 100 MPa à température ambiante. La température maximale d’essai du matériau est de 650 °C.

Aeronavtika - Sorniki, normalna šestroba glava, tanko steblo, dolg navoj, iz toplotno odpornega jekla FE-PA2601 (A286), posrebreni - Klasifikacija: 1100 MPa/650 °C

Ta dokument določa lastnosti srebrno prevlečenih vijakov z običajno šesterokotno glavo, z razbremenjenim steblom in dolgim navojem, iz toplotno odpornega jekla FE-PA92HT (A286), z natezno trdnostjo razreda 1 100 MPa pri sobni temperaturi. Najvišja preskusna temperatura materiala je 650 °C.

General Information

Status
Published
Publication Date
10-Mar-2026
Technical Committee
ASD-STAN - Aerospace
Drafting Committee
ASD-STAN/D 3/S 2 - Fasteners
Current Stage
6060 - Definitive text made available (DAV) - Publishing
Start Date
11-Mar-2026
Completion Date
11-Mar-2026

Relations

Effective Date
11-Oct-2023
Effective Date
11-Oct-2023
Effective Date
25-Mar-2026
Effective Date
25-Mar-2026
Effective Date
25-Mar-2026
Effective Date
25-Mar-2026
Effective Date
25-Mar-2026
Effective Date
25-Mar-2026
Effective Date
25-Mar-2026
Effective Date
28-Jan-2026

Overview

EN 3687:2026 establishes the requirements for aerospace bolts featuring a normal hexagon head, relieved shank, and long thread, made from heat resisting steel FE-PA2601 (A286) with silver plating. This European standard is part of the Aerospace series developed by CEN, tailored specifically for high-strength fasteners used in demanding aerospace environments. The bolts covered under this standard are classified for a tensile strength of 1,100 MPa at room temperature and their material is validated for operating temperatures up to 650 °C.

The standard supersedes previous versions (EN 3687:2010 and EN 3687:2010/AC:2011), introducing precise updates on surface roughness requirements and dimensional tolerances, further enhancing reliability and performance in critical aerospace applications.

Key Topics

  • Product Characteristics

    • Normal hexagon head for standard wrenching
    • Relieved (thin) shank and extended thread to support specific assembly designs
    • Manufactured from FE-PA2601 (A286) heat resisting steel, ideal for high temperature and high stress
    • Silver plating for improved corrosion resistance and galling prevention
  • Performance Classification

    • Tensile strength: 1,100 MPa at room temperature
    • Maximum operating/test temperature: 650 °C
  • Surface and Dimensional Requirements

    • Surface roughness:
      • Bearing areas (head, shank, thread): Ra max 0.8 µm
      • Other surfaces: Ra max 3.2 µm
    • All edges are to be free from sharpness (0.1 mm to 0.4 mm removed)
    • Dimensional envelopes specified by size code and length for design reliability
  • Marking and Traceability

    • Each bolt is marked in compliance with EN 2424 for aerospace product identification

Applications

EN 3687:2026 bolts are engineered for use in:

  • Aircraft Structural Assemblies
    The combination of high tensile strength and heat resistance ensures reliability in critical airframe connections, engine components, and other load-bearing structures exposed to extreme thermal cycles.

  • Aerospace Engine Mounting
    The relieved shank and long thread designs accommodate precise torque requirements in jet engines and propulsion systems.

  • Spacecraft and Satellites
    Silver plating improves electrical conductivity and galling resistance, making these bolts suitable for high-reliability electrical and mechanical junctions in space applications.

  • High-Temperature Fastening
    Ideal for parts subjected to elevated temperatures, such as exhaust systems or turbine assemblies, where sustained mechanical strength and corrosion resistance are essential.

Related Standards

For complete conformity and integration in aerospace manufacturing, EN 3687:2026 should be used alongside:

  • EN 2424: Aerospace marking of products, ensuring proper identification and traceability.
  • EN 2786: Defines requirements for electrolytic silver plating of fasteners.
  • EN 3685: Comprehensive technical specification for bolts in heat resisting steel FE-PA2601 (A286).
  • EN 3761: Material requirements for FE-PA2601 (A286) alloy bar for forged fasteners.
  • ISO 3353-1: Aerospace lead and runout threads.
  • ISO 5855-1 and ISO 5855-2: Specifies MJ threads and their tolerances for aerospace fasteners.
  • ASME B46.1: Surface texture and roughness standards, referenced for finish quality.

EN 3687:2026 provides a robust framework for the selection and use of high-performance, silver-plated, high-temperature bolts in aerospace industries, ensuring longevity, safety, and consistent quality in demanding applications. For further guidance, always consult the relevant related standards to ensure comprehensive compliance in aerospace engineering projects.

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Frequently Asked Questions

EN 3687:2026 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Bolt, normal hexagon head, relieved shank, long thread, in heat resisting steel FE-PA2601 (A286), silver plated - Classification: 1 100 MPa/650 °C". This standard covers: This document specifies the characteristics of silver-plated Bolts normal Hexagon Head with relieved shank and long thread, in heat resisting steel FE-PA92HT (A286), tensile strength class 1 100 MPa at room temperature. The maximum test temperature of the material is 650 °C.

This document specifies the characteristics of silver-plated Bolts normal Hexagon Head with relieved shank and long thread, in heat resisting steel FE-PA92HT (A286), tensile strength class 1 100 MPa at room temperature. The maximum test temperature of the material is 650 °C.

EN 3687:2026 is classified under the following ICS (International Classification for Standards) categories: 49.030.20 - Bolts, screws, studs. The ICS classification helps identify the subject area and facilitates finding related standards.

EN 3687:2026 has the following relationships with other standards: It is inter standard links to EN 3687:2010/AC:2011, EN 3687:2010, ISO 5855-2:1999, ISO 5855-1:1999, ISO 3353-1:2020, EN 3685:2019, EN 2786:2008, EN 2424:2008, EN 3761:2020, EN 14439:2025. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

EN 3687:2026 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-maj-2026
Aeronavtika - Sorniki, normalna šestroba glava, tanko steblo, dolg navoj, iz
toplotno odpornega jekla FE-PA2601 (A286), posrebreni - Klasifikacija: 1100
MPa/650 °C
Aerospace series - Bolts, normal hexagon head, relieved shank, long thread, in heat
resisting steel FE-PA2601 (A286), silver plated - Classification: 1 100 MPa/650 °C
Luft- und Raumfahrt - Sechskantschrauben, Dünnschaft, langes Gewinde, aus
hochwarmfestem Stahl FE-PA2601 (A286), versilbert - Klasse: 1 100 MPa/650 °C
Série aérospatiale - Vis à tête hexagonale normale, tige dégagée, filetage long, en acier
résistant à chaud FE-PA2601 (A286), argentées - Classification : 1 100 MPa/650 °C
Ta slovenski standard je istoveten z: EN 3687:2026
ICS:
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 3687
EUROPEAN STANDARD
NORME EUROPÉENNE
March 2026
EUROPÄISCHE NORM
ICS 49.030.20 Supersedes EN 3687:2010
English Version
Aerospace series - Bolt, normal hexagon head, relieved
shank, long thread, in heat resisting steel FE-PA2601
(A286), silver plated - Classification: 1 100 MPa/650 °C
Série aérospatiale - Vis à tête hexagonale normale, tige Luft- und Raumfahrt - Sechskantschraube, Dünnschaft,
dégagée, filetage long, en acier résistant à chaud FE- langes Gewinde, aus hochwarmfestem Stahl FE-
PA2601 (A286), argentées - Classification : 1 100 PA2601 (A286), versilbert - Klasse: 1 100 MPa/650 °C
MPa/650 °C
This European Standard was approved by CEN on 19 January 2026.

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 3687:2026 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 . 4
4.1 Configuration – Dimensions – Tolerances . 4
4.2 Surface roughness . 4
4.3 Material . 5
4.4 Surface treatment . 5
5 Designation . 11
6 Marking . 11
7 Technical specification . 11
Bibliography . 12

European foreword
This document (EN 3687:2026) 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 September 2026, and conflicting national standards
shall be withdrawn at the latest by September 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 3687:2010 and EN 3687:2010/AC:2011.
This document includes the following significant technical changes with respect to EN 3687:2010 and
EN 3687:2010/AC:2011:
— the surface roughness requirements have been replaced from Figure 1 to the text;
— values for S at diameter code 050 in Table 1 have been corrected.
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 silver-plated bolts with normal hexagon head, relieved
shank and long thread, in heat resisting steel FE-PA2601 (A286), tensile strength class 1 100 MPa at
room temperature. The maximum test temperature of the material is 650 °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 dated references, only the edition cited applies. For
undated references, the latest edition of the referenced document (including any amendments) applies.
EN 2424:2008, Aerospace series — Marking of aerospace products
EN 2786, Aerospace series — Electrolytic silver plating of fasteners
EN 3685, Aerospace series — Bolts in heat resisting steel FE-PA2601 (A286) — Classification:
1 100 MPa/650 °C — Technical specification
EN 3761, Aerospace series — Heat resisting alloy FE-PA2601 — Softened and cold worked — Bar for
forged fasteners — D ≤ 50 mm — 1 100 MPa ≤ R ≤ 1 300 MPa
m
ISO 3353-1, Aerospace — Lead and runout threads — Part 1: Rolled external threads
ISO 5855-1, Aerospace — MJ threads — Part 1: General requirements
ISO 5855-2, Aerospace — MJ threads — Part 2: Limit dimensions for bolts and nuts
3 Terms and definitions
No terms and definitions are listed in this document.
ISO and IEC maintain terminology databases for use in standardization at th
...

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