SIST EN 3687:2012
(Main)Aerospace series - Bolts, normal hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated - Classification: 1100 MPa/650°C
Aerospace series - Bolts, normal hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated - Classification: 1100 MPa/650°C
This standard 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 - Sechskantschrauben, Dünnschaft, langes Gewinde, aus hochwarmfesten Stahl FE-PA92HT (A286) versilbert - Klasse: 1100MPa/650°C
Diese Norm legt die Eigenschaften von Sechskantschrauben mit Dünnschaft und langem Gewinde aus hochwarmfestem Stahl FE-PA92HT (A286), versilbert, Zugfestigkeitsklasse 1 100 MPa bei Raumtemperatur, fest. Die maximale Prüftemperatur des Werkstoffes beträgt 650 °C.
Série aérospatiale - Vis à tête hexagonale normale, fût dégagé filetage long, en acier résistant à chaud FE-PA92HT (A286), argentées - Classification: 1100 MPa/650°C
Aeronavtika - Sorniki, normalna šestroba glava, tanko steblo, dolg navoj, iz toplotnoodpornega jekla FE-PA92HT (A286), posrebreni - Klasifikacija: 1100 MPa/650 °C
Ta standard določa značilnosti posrebrenih sornikov z normalno šestrobo glavo, tankim steblom in dolgim navojem iz toplotnoodpornega jekla FE-PA92HT (A286), razreda natezne trdnosti 1100 MPa pri sobni temperaturi. Maksimalna preskusna temperatura materiala je 650 °C.
General Information
- Status
- Published
- Publication Date
- 30-Nov-2011
- Technical Committee
- I13 - Imaginarni 13
- Current Stage
- 6060 - National Implementation/Publication (Adopted Project)
- Start Date
- 24-Nov-2011
- Due Date
- 29-Jan-2012
- Completion Date
- 01-Dec-2011
Relations
- Effective Date
- 06-Aug-2011
- Effective Date
- 11-Oct-2023
Overview
EN 3687:2010 defines requirements for a specific class of aerospace fasteners: bolts with a normal hexagon head, relieved shank and long thread made from heat‑resisting steel FE‑PA92HT (A286). The standard covers bolts silver‑plated by electrolytic plating and classified for a tensile strength of 1 100 MPa (room temperature) with a maximum test temperature of 650 °C. EN 3687:2010 is aimed at consistent performance, interchangeability and traceability of high‑temperature aerospace bolts.
Key topics and technical requirements
- Material: Heat‑resisting steel FE‑PA92HT (A286) per EN 3761.
- Mechanical classification: Tensile strength class 1 100 MPa at room temperature; material test up to 650 °C.
- Configuration and dimensions: Head, shank and long‑thread geometry, plus tolerances and masses, are specified in figures and tables (diameter/length codes). Dimensions conform to ISO thread standards.
- Threads: Rolled external threads and lead/runout details per ISO 3353‑1; MJ thread limits per ISO 5855‑1/2.
- Surface finish / roughness: Values specified (applicable before silver plating).
- Surface treatment:Electrolytic silver plating per EN 2786 Category A; coating thickness 3 µm to 6 µm measured on thread flanks at pitch diameter.
- Marking and designation: Marking conforms to EN 2424 Category A; example designation format - BOLT EN3687‑060030.
- Technical specification & procurement: Technical rules reference EN 3685 for bolt technical specification and EN 3761 for material bar requirements.
Applications
EN 3687:2010 is intended for aerospace applications where fasteners must withstand elevated temperatures and maintain high tensile strength and corrosion/thermal protection from silver plating. Typical uses include:
- Hot‑section assemblies and components in aircraft and propulsion systems
- Structural and mechanical aerospace joints exposed to high temperatures
- Situations requiring precise interchangeability, traceability and controlled plating for electrical conductivity or corrosion resistance
Who uses this standard
- Aerospace design and mechanical engineers specifying high‑temperature fasteners
- Fastener manufacturers and heat‑treat/finish suppliers producing FE‑PA92HT (A286) bolts
- Quality assurance, procurement and regulatory teams in aerospace OEMs and MRO providers
- Suppliers preparing technical specifications and inspection/test documentation
Related standards
- EN 2786 - Electrolytic silver plating of fasteners
- EN 2424 - Marking of aerospace products
- EN 3685 - Bolt technical specification (related heat‑resisting bolts)
- EN 3761 - Heat‑resisting alloy FE‑PA2601 / material bar requirements
- ISO 3353‑1, ISO 5855‑1/2 - Thread forms and limits
Keywords: EN 3687:2010, aerospace bolts, FE‑PA92HT, A286, silver plated bolts, heat resisting steel, 1100 MPa, 650 °C, hexagon head bolts, aerospace fasteners.
Frequently Asked Questions
SIST EN 3687:2012 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Bolts, normal hexagon head, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated - Classification: 1100 MPa/650°C". This standard covers: This standard 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 standard 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.
SIST EN 3687:2012 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.
SIST EN 3687:2012 has the following relationships with other standards: It is inter standard links to SIST EN 3687:2012/AC:2012, kSIST FprEN 3687:2025. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
SIST EN 3687:2012 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-januar-2012
Aeronavtika - Sorniki, normalna šestroba glava, tanko steblo, dolg navoj, iz
toplotnoodpornega jekla FE-PA92HT (A286), posrebreni - Klasifikacija: 1100
MPa/650 °C
Aerospace series - Bolts, normal hexagon head, relieved shank, long thread, in heat
resisting steel FE-PA92HT (A286), silver plated - Classification: 1100 MPa/650°C
Luft- und Raumfahrt - Sechskantschrauben, Dünnschaft, langes Gewinde, aus
hochwarmfesten Stahl FE-PA92HT (A286) versilbert - Klasse: 1100MPa/650°C
Série aérospatiale - Vis à tête hexagonale normale, fût dégagé filetage long, en acier
résistant à chaud FE-PA92HT (A286), argentées - Classification: 1100 MPa/650°C
Ta slovenski standard je istoveten z: EN 3687:2010
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.
EUROPEAN STANDARD
EN 3687
NORME EUROPÉENNE
EUROPÄISCHE NORM
December 2010
ICS 49.030.20
English Version
Aerospace series - Bolts, normal hexagon head, relieved shank,
long thread, in heat resisting steel FE-PA92HT (A286), silver
plated - Classification: 1 100 MPa/650 °C
Série aérospatiale - Vis à tête hexagonale normale, fût Luft- und Raumfahrt - Sechskantschrauben, Dünnschaft,
dégagé filetage long, en acier résistant à chaud FE- langes Gewinde, aus hochwarmfesten Stahl FE-PA92HT
PA92HT (A286), argentées - Classification: 1 100 MPa/650 (A286) versilbert - Klasse: 1 100 MPa/650 °C
°C
This European Standard was approved by CEN on 15 August 2010.
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, 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 Ref. No. EN 3687:2010: E
worldwide for CEN national Members.
Contents Page
Foreword .3
1 Scope .4
2 Normative references .4
3 Required characteristics .4
3.1 Configuration – Dimensions – Tolerances .4
3.2 Surface roughness .4
3.3 Material .4
3.4 Surface treatment .4
4 Designation . 11
5 Marking . 11
6 Technical specification . 11
Foreword
This document (EN 3687:2010) 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 Standard has
received the approval of the National Associations and the Official Services of the member countries of ASD,
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 June 2011, and conflicting national standards shall be withdrawn at
the latest by June 2011.
Attention is drawn to the possibility that some of the elements of this document may be the subject of patent
rights. CEN [and/or CENELEC] shall not be held responsible for identifying any or all such patent rights.
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, Romania, Slovakia, Slovenia, Spain,
Sweden, Switzerland and the United Kingdom.
1 Scope
This standard 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.
2 Normative references
The following referenced documents are indispensable for the application 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, 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
1)
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 t
...




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