Aerospace series - Bolts, normal hexagonal head, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated - Classification: 1 275 MPa/650 °C

This document specifies the characteristics of bolts normal hexagonal head with relieved shank and long thread in heat resisting nickel base alloy NI-PH2601 (Inconel 718), for aerospace applications.
Classification: 1 275 MPa /650 °C

Luft‑ und Raumfahrt - Sechskantschrauben, Dünnschaft, langes Gewinde, aus hochwarmfester Nickelbasislegierung NI‑PH2601 (Inconel 718), versilbert - Klasse: 1 275 MPa/650 °C

Dieses Dokument legt die Eigenschaften von üblichen Sechskantschrauben mit Dünnschaft und langem Gewinde aus hochwarmfester Nickelbasislegierung NI PH2601 (Inconel 718) für die Anwendung in der Luft- und Raumfahrt fest.
Klasse: 1 275 MPa /650 °C

Série aérospatiale - Vis à tête hexagonale normale, tige dégagée, filetage long, en alliage résistant à chaud base nickel NI-PH2601 (Inconel 718), argentées - Classification : 1 275 MPa/650 °C

Le présent document spécifie les caractéristiques des vis à tête hexagonale normale, tige dégagée, filetage long, en alliage résistant à chaud base nickel NI-PH2601 (Inconel 718), pour les applications aérospatiales.
Classification : 1 275 MPa /650 °C.

Aeronavtika - Sorniki, normalna šestroba glava, tanko steblo, dolg navoj, iz toplotnoodporne zlitine na nikljevi osnovi NI-PH2601 (Inconel 718), posrebreni - Klasifikacija: 1 275 MPa/650 °C

General Information

Status
Not Published
Publication Date
13-Dec-2026
Technical Committee
ASD-STAN - Aerospace
Drafting Committee
ASD-STAN/D 3/S 2 - Fasteners
Current Stage
4060 - Closure of enquiry - Enquiry
Start Date
11-Sep-2025
Completion Date
11-Sep-2025

Relations

Effective Date
12-Feb-2025

Overview

prEN 3613 defines the characteristics of aerospace bolts with a normal hexagonal head, relieved shank and long thread, manufactured from the heat‑resisting nickel‑base alloy NI‑PH2601 (Inconel 718) and silver plated. The draft European Standard (to supersede EN 3613:2009) classifies these fasteners as 1 275 MPa / 650 °C, and is intended for high‑temperature aerospace applications where standardised dimensions, materials and coatings are required.

Key Topics and Requirements

  • Scope and classification: Bolts in NI‑PH2601 (Inconel 718) for aerospace use; Classification: 1 275 MPa / 650 °C (minimum tensile class at ambient temperature and maximum test temperature).
  • Configuration, dimensions and tolerances: Detailed geometry, sizes (diameter codes 050–080), lengths and masses are specified in figures and tables. Dimensions apply after silver plating.
  • Surface roughness: Requirements given for the as‑manufactured surface (values apply after plating).
  • Material: Nickel alloy to comply with TR 3775; SAE AMS5662 is cited as an example material specification for NI‑PH2601 (Inconel 718).
  • Surface coating: Electrolytic silver plating per EN 2786, Category A, with coating thickness 3 µm to 6 µm on thread flanks measured at the pitch diameter.
  • Marking and designation: Marking per EN 2424, Category A. Example designation format: BOLT EN 3613 060 030 (document number + diameter code + length code).
  • Technical specification reference: Technical requirements referenced to EN 2583.
  • Standards coordination: Threads and form follow relevant ISO standards (e.g., ISO 3353‑1, ISO 5855‑1/2).

Applications and Users

Who uses prEN 3613:

  • Aerospace fastener manufacturers and suppliers producing Inconel 718 bolts
  • Aircraft engine and airframe design engineers specifying high‑temperature fasteners
  • Procurement, quality assurance and inspection teams requiring standardised marking, materials and plating
  • Maintenance, repair and overhaul (MRO) organisations and certification bodies that verify compliance

Practical applications:

  • Fastening components in high‑temperature aerospace environments where a heat‑resistant nickel‑base alloy is needed and standardised dimensions, thread forms and silver plating are specified.

Related Standards

  • EN 2583 - Bolts, MJ threads, in NI‑PH2601 (Inconel 718)
  • EN 2786 - Electrolytic silver plating of fasteners
  • EN 2424 - Marking of aerospace products
  • ISO 3353‑1, ISO 5855‑1/2 - Thread forms and limit dimensions
  • TR 3775, SAE AMS5662 - Material specifications for nickel alloys

Keywords: aerospace bolts, Inconel 718, NI‑PH2601, hexagonal head bolts, relieved shank, long thread, silver plated fasteners, high‑temperature aerospace fasteners, EN 3613.

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Frequently Asked Questions

prEN 3613 is a draft published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Bolts, normal hexagonal head, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated - Classification: 1 275 MPa/650 °C". This standard covers: This document specifies the characteristics of bolts normal hexagonal head with relieved shank and long thread in heat resisting nickel base alloy NI-PH2601 (Inconel 718), for aerospace applications. Classification: 1 275 MPa /650 °C

This document specifies the characteristics of bolts normal hexagonal head with relieved shank and long thread in heat resisting nickel base alloy NI-PH2601 (Inconel 718), for aerospace applications. Classification: 1 275 MPa /650 °C

prEN 3613 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.

prEN 3613 has the following relationships with other standards: It is inter standard links to EN 3613:2009. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

prEN 3613 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-september-2025
Aeronavtika - Sorniki, normalna šestroba glava, tanko steblo, dolg navoj, iz
toplotnoodporne zlitine na nikljevi osnovi NI-PH2601 (Inconel 718), posrebreni -
Klasifikacija: 1 275 MPa/650 °C
Aerospace series - Bolts, normal hexagonal head, relieved shank, long thread, in heat
resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated - Classification: 1 275
MPa/650 °C
Luft‑ und Raumfahrt - Sechskantschrauben, Dünnschaft, langes Gewinde, aus
hochwarmfester Nickelbasislegierung NI‑PH2601 (Inconel 718), versilbert - Klasse: 1
275 MPa/650 °C
Série aérospatiale - Vis à tête hexagonale normale, fût dégagé, filetage long, en alliage
base nickel, résistant à chaud NI-PH2601 (Inconel 718), argentées - Classification : 1
275 MPa/650 °C
Ta slovenski standard je istoveten z: prEN 3613
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.

DRAFT
EUROPEAN STANDARD
NORME EUROPÉENNE
EUROPÄISCHE NORM
June 2025
ICS 49.030.20 Will supersede EN 3613:2009
English Version
Aerospace series - Bolts, normal hexagonal head, relieved
shank, long thread, in heat resisting nickel base alloy NI-
PH2601 (Inconel 718), silver plated - Classification: 1 275
MPa/650 °C
Série aérospatiale - Vis à tête hexagonale normale, fût Luft- und Raumfahrt - Sechskantschrauben,
dégagé, filetage long, en alliage base nickel, résistant à Dünnschaft, langes Gewinde, aus hochwarmfester
chaud NI-PH2601 (Inconel 718), argentées - Nickelbasislegierung NI-PH2601 (Inconel 718),
Classification : 1 275 MPa/650 °C versilbert - Klasse: 1 275 MPa/650 °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 3613:2025 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, tolerances, masses . 4
4.2 Surface roughness . 4
4.3 Material . 5
4.4 Surface coating . 5
5 Designation . 8
6 Marking . 8
7 Technical specification . 8
European foreword
This document (prEN 3613:2025) 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 3613:2009.
This document includes the following significant technical changes with respect to EN 3613:2009:
— 4.2 “Material”: material standard SAE AMS5662 added;
— 4.4 “Thread surface” removed.
1 Scope
This document specifies the characteristics of bolts normal hexagonal head with relieved shank and long
thread in heat resisting nickel base alloy NI-PH2601 (Inconel 718), for aerospace applications.
1 2
Classification: 1 275 MPa /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, Aerospace series — Marking of aerospace products
EN 2583, Aerospace series — Bolts, MJ threads, in heat resisting nickel base
...

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