EN 2583:2019
(Main)Aerospace series - Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) - Classification: 1 275 MPa (at ambient temperature)/650°C - Technical specification
Aerospace series - Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) - Classification: 1 275 MPa (at ambient temperature)/650°C - Technical specification
This standard specifies the characteristics, qualification and acceptance requirements for bolts with MJ threads in NI-PH2601.
Classification: 1 275 MPa /650 °C .
It is applicable whenever referenced.
Luft- und Raumfahrt - Schrauben, MJ-Gewinde, aus hochwarmfester Nickelbasislegierung NI-PH2601 (Inconel 718) - Klasse: 1 275 MPa (bei Raumtemperatur)/650°C - Technische Lieferbedingungen
Diese Norm legt die Eigenschafts , Qualifizierungs und Abnahmeanforderungen für Schrauben mit MJ Gewinde aus NI PH2601 fest.
Klassifizierung: 1 275 MPa /650 °C .
Die Norm ist anwendbar, wenn darauf verwiesen wird.
Série aérospatiale - Vis à filetage MJ, en alliage résistant à chaud à base de nickel NI-PH2601 (Inconel 718) - Classification: 1 275 MPa (à température ambiante)/650°C - Spécification technique
La présente norme spécifie les caractéristiques, les exigences de qualification et de réception des vis à filetage MJ en NI-PH2601.
Classification : 1 275 MPa /650 °C .
Elle est applicable chaque fois qu'elle est citée en référence.
Aeronavtika - Sorniki, navoj MJ, iz toplotnoodporne zlitine na nikljevi osnovi NI-PH2601 (Inconel 718) - Klasifikacija: 1270 MPa (pri okoljski temperaturi)/650 °C - Tehnična specifikacija
Ta standard določa karakteristike ter zahteve glede kvalifikacije in sprejemljivosti za sornike z navojem MJ iz NI-PH2601.
Klasifikacija: 1 275 MPa1/650 °C2.
Uporablja se, kadar je naveden.
General Information
Relations
Standards Content (Sample)
SLOVENSKI STANDARD
01-julij-2019
Nadomešča:
SIST EN 2583:2001
Aeronavtika - Sorniki, navoj MJ, iz toplotnoodporne zlitine na nikljevi osnovi NI-
PH2601 (Inconel 718) - Klasifikacija: 1270 MPa (pri okoljski temperaturi)/650 °C -
Tehnična specifikacija
Aerospace series - Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601
(Inconel 718) - Classification: 1 275 MPa (at ambient temperature)/650°C - Technical
specification
Luft- und Raumfahrt - Schrauben, MJ-Gewinde, aus hochwarmfester
Nickelbasislegierung NI-PH2601 (Inconel 718) - Klasse: 1 275 MPa (bei
Raumtemperatur)/650°C - Technische Lieferbedingungen
Série aérospatiale - Vis à filetage MJ, en alliage résistant à chaud à base de nickel NI-
PH2601 (Inconel 718) - Classification: 1 275 MPa (à température ambiante)/350°C -
Spécification technique
Ta slovenski standard je istoveten z: EN 2583:2019
ICS:
21.060.10 Sorniki, vijaki, stebelni vijaki Bolts, screws, studs
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 2583
EUROPEAN STANDARD
NORME EUROPÉENNE
May 2019
EUROPÄISCHE NORM
ICS 49.030.20 Supersedes EN 2583:1997
English Version
Aerospace series - Bolts, MJ threads, in heat resisting
nickel base alloy NI-PH2601 (Inconel 718) - Classification:
1 275 MPa (at ambient temperature)/650°C - Technical
specification
Série aérospatiale - Vis à filetage MJ, en alliage résistant Luft- und Raumfahrt - Schrauben, MJ-Gewinde, aus
à chaud à base de nickel NI-PH2601 (Inconel 718) - hochwarmfester Nickelbasislegierung NI-PH2601
Classification: 1 275 MPa (à température (Inconel 718) - Klasse: 1 275 MPa (bei
ambiante)/650°C - Spécification technique Raumtemperatur)/650°C - Technische
Lieferbedingungen
This European Standard was approved by CEN on 10 December 2018.
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, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania,
Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland,
Turkey 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
© 2019 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 2583:2019 E
worldwide for CEN national Members.
Contents
Page
European foreword . 3
1 Scope . 4
2 Normative references . 4
3 Definitions . 4
4 Quality assurance . 6
5 Requirements . 7
Annex A (normative) Passivation treatment for bolts . 23
Bibliography . 24
European foreword
This document (EN 2583:2019) 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 November 2019, and conflicting national standards
shall be withdrawn at the latest by November 2019.
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 2583:1997.
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, Former Yugoslav Republic of Macedonia,
France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta,
Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland,
Turkey and the United Kingdom.
1 Scope
This standard specifies the characteristics, qualification and acceptance requirements for bolts with MJ
threads in NI-PH2601.
1 2
Classification: 1 275 MPa /650 °C .
It is applicable whenever referenced.
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.
ISO 2859-1, Sampling procedures for inspection by attributes — Part 1: Sampling schemes indexed by
acceptance quality limit (AQL) for lot-by-lot inspection
ISO 3452-1, Non-destructive testing — Penetrant testing — Part 1: General principles
ISO 3534:1977, Statistics — Vocabulary and symbols
ISO 4288, Geometrical Product Specifications (GPS) — Surface texture: Profile method — Rules and
procedures for the assessment of surface texture
ISO 5855-2, Aerospace — MJ threads — Part 2: Limit dimensions for bolts and nuts
ISO 6508-1, Metallic materials — Rockwell hardness test — Part 1: Test method
ISO 6892-1, Metallic materials — Tensile testing — Part 1: Method of test at room temperature
ISO 7961, Aerospace — Bolts — Test methods
ISO 9227, Corrosion tests in artificial atmospheres — Salt spray tests
ASTM E 112-13, Standard Test Methods for Determining Average Grain Size
3 Definitions
For the purposes of this document, the following terms and definitions apply.
ISO and IEC maintain terminological databases for use in standardization at the following addresses:
1 Minimum tensile strength of the material at ambient temperature.
2 Maximum test temperature of the parts.
3 Published by: American Society for Testing and Materials (ASTM), 100 Barr Harbor Drive, PO Box C700,
West Conshohoken, PA 19428-2959, USA.
IEC Electropedia: available at http://www.electropedia.org/
ISO Online browsing platform: available at http://www.iso.org/obp
3.1
batch
quantity of finished bolts, of the same type and same diameter, produced from a material obtained from
the same melt, manufactured in the course of the same production cycle, following the same
manufacturing route and having undergone all the relevant heat treatments and surface treatments
3.2
Surface discontinuities
3.2.1
crack
rupture in the material which may extend in any direction and which may be intercrystalline or
transcrystalline in character
3.2.2
seam
open surface defect
3.2.3
lap
surface defect caused by folding over metal fins or sharp corners and then compressing them into the
surface
3.2.4
inclusions
non-metallic particles originating from the material manufacturing process. These particles may be
isolated or arranged in strings
3.3
test temperature
ambient temperature, unless otherwise specified
3.4
simple random sampling
taking of n items from a population of N items in such a way that all possible combinations of n items
have the same probability of being chosen
[SOURCE: ISO 3534:1977]
3.5
critical defect
defect that, according to judgement and experience, is likely to result in hazardous or unsafe conditions
for individuals using, maintaining, or depending upon the considered product, or that is likely to
prevent performance of the function of a major end item
[SOURCE: ISO 3534:1977]
3.6
major defect
defect, other than critical, that is likely to result in a failure or to reduce materially the usability of the
considered product for its intended purpose
[SOURCE: ISO 3534:1977]
3.7
minor defect
defect that is not likely to reduce materially the usability of the considered product for its intended
purpose, or that is a departure from established specification having little bearing on the effective use
or operation of this product
[SOURCE: ISO 3534:1977]
3.8
sampling plan
plan according to which one or more samples are taken in order to obtain information and possibly to
reach a decision
[SOURCE: ISO 3534:1977]
3.9
limiting quality
in a sampling plan, the quality level which corresponds to the specified 10 % probability of acceptance
3.10
acceptable quality level
AQL
quality level which in a sampling plan corresponds to a specified but relatively high probability of
acceptance. It is the maximum per cent defective (or the maximum number of defects per hundred
units) that, for purposes of sampling inspection, can be considered satisfactory as a process average
[SOURCE: ISO 3534:1977]
3.11
finished bolt
bolt ready for use, inclusive of any possible treatments and/or surface coatings, as specified in the
product standard or definition document
3.12
definition document
document specifying all the requirements for finished bolts
4 Quality assurance
4.1 Qualification
The qualification procedure for aerospace standard products (e. g. according to EN 9133 or an
equivalent aerospace accepted and established qualification procedure) shall be used and documented
according to the specified tests if not otherwise agreed between customer and supplier.
Qualification inspections and tests (requirements, methods, numbers of bolts) are specified in Table 1.
They shall be carried out on:
each type and diameter of bolt;
25 bolts selected from a single batch by simple random sampling.
The test programme may possibly be reduced, or the qualification be granted without inspection or
testing: any such decision shall be based on the results obtained on similar types and diameters of bolts
provided that the design and manufacturing conditions are identical.
Table 2 indicates the allocation of bolt specimens for the inspections and tests.
4.2 Acceptance
4.2.1 Purpose
The purpose of acceptance inspections and tests is to check, as simply as possible, by a method
representative of actual use conditions, with the uncertainty inherent to statistical sampling, that the
bolts constituting the batch satisfy the requirements of this standard.
4.2.2 Conditions
Acceptance inspections and tests (requirements, methods, numbers of bolts) are specified in Table 1.
They shall be carried out on each batch. Bolts from the batch to be tested shall be selected by simple
random sampling.
Each nut may be submitted to several inspections or tests.
If a more stringent inspection is deemed necessary, all or part of the qualification inspections and tests
may be performed during the acceptance inspection and testing. In this case, the number of bolts
submitted to these inspections and tests is the same as that submitted for qualification inspection and
tests.
4.2.3 Responsibility
Acceptance inspections and tests shall be carried out by the manufacturer, or under his responsibility.
4.2.4 Inspection and test report
A test report showing actual numerical values shall be provided if specified in the purchase order.
5 Requirements
See Table 1.
Table 1 — Technical requirements and test methods
Inspection and test
a
Clause Characteristic Requirement Sample size
Q/A
method
5.1 Material In accordance with the product Chemical analysis or Q
standard or definition document. certificate of compliance
A
issued by the
manufacturer of the
semi-finished product
5.2 Dimensions, In accordance with the product Standard gauging Q 25
tolerances and standard or definition document.
A Table 3 and
tolerances of form
Table 4
and position
Inspection and test
a
Clause Characteristic Requirement Sample size
Q/A
method
5.3 Manufacturing
5.3.1 Forging The head of the bolts shall be The method of forging Q
formed by hot or cold forging. If shall be indicated.
hot forged, the forging
temperature shall not exceed
1 150 °C and they shall be air
cooled.
The equipment shall ensure a
uniform temperature throughout
the batch.
5.3.2 Heat treatment The heat treatment medium or Calibration of the heat Q
atmosphere shall not cause a
...
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