EN 2576:2020
(Main)Aerospace series - Bolts, MJ threads, in heat resisting steel FE-PA2601 (A286) - Classification: 900 MPa (at ambient temperature)/650 °C - Technical specification
Aerospace series - Bolts, MJ threads, in heat resisting steel FE-PA2601 (A286) - Classification: 900 MPa (at ambient temperature)/650 °C - Technical specification
This European standard specifies the characteristics, qualification and acceptance requirements for bolts with MJ threads in heat resisting steel FE-PA2601, for aerospace applications.
Classification: 900 MPa1/650 °C2.
It is applicable whenever referenced.
Luft- und Raumfahrt - Schrauben, MJ-Gewinde, aus hochwarmfestem Stahl FE-PA2601 (A286) - Klasse: 900 MPa (bei Raumtemperatur)/650 °C - Technische Lieferbedingungen
Dieses Dokument legt die Eigenschaften sowie die Qualifikations- und Annahmeanforderungen für Schrauben mit MJ-Gewinde aus hochwarmfestem Stahl FE PA2601 für Anwendungen in der Luft- und Raumfahrt fest.
Klasse: 900 MPa /650 °C .
Es gilt in allen Fällen, in denen darauf verwiesen wird.
Série aérospatiale - Vis à filetage MJ, en acier résistant à chaud FE-PA2601 (A286) - Classification : 900 MPa (à température ambiante)/650 °C - Spécification technique
La présente norme européenne spécifie les caractéristiques, les exigences de qualification et de réception des vis à filetage MJ en acier résistant à chaud FE-PA2601, pour applications aérospatiales.
Classification : 900 MPa1) 650 °C 2)
Elle est applicable chaque fois qu'elle est citée en référence.
Aeronavtika - Sorniki, navoj MJ, iz toplotno odpornega jekla FE‑PA2601 (A286) - Klasifikacija: 900 MPa (pri okoljski temperaturi)/650 °C - Tehnična specifikacija
General Information
Standards Content (Sample)
SLOVENSKI STANDARD
01-julij-2020
Aeronavtika - Sorniki, navoj MJ, iz toplotno odpornega jekla FE‑PA2601 (A286) -
Klasifikacija: 900 MPa (pri okoljski temperaturi)/650 °C - Tehnična specifikacija
Aerospace series - Bolts, MJ threads, in heat resisting steel FE‑PA2601 (A286) -
Classification: 900 MPa (at ambient temperature)/650 °C - Technical specification
Luft- und Raumfahrt - Schrauben, MJ-Gewinde, aus hochwarmfestem Stahl FE-PA2601
(A286) - Klasse: 900 MPa (bei Raumtemperatur)/650 °C - Technische
Lieferbedingungen
Série aérospatiale - Vis à filetage MJ, en acier résistant à chaud FE‑PA2601 (A286) -
Classification : 900 MPa (à température ambiante)/650 °C - Spécification technique
Ta slovenski standard je istoveten z: EN 2576:2020
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 2576
EUROPEAN STANDARD
NORME EUROPÉENNE
May 2020
EUROPÄISCHE NORM
ICS 49.030.20
English Version
Aerospace series - Bolts, MJ threads, in heat resisting steel
FE-PA2601 (A286) - Classification: 900 MPa (at ambient
temperature)/650 °C - Technical specification
Série aérospatiale - Vis à filetage MJ, en acier résistant Luft- und Raumfahrt - Schrauben, MJ-Gewinde, aus
à chaud FE-PA2601 (A286) - Classification : 900 MPa hochwarmfestem Stahl FE-PA2601 (A286) - Klasse:
(à température ambiante)/650 °C - Spécification 900 MPa (bei Raumtemperatur)/650 °C - Technische
technique Lieferbedingungen
This European Standard was approved by CEN on 30 September 2019.
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, 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
© 2020 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 2576:2020 E
worldwide for CEN national Members.
Contents
Page
European foreword . 3
1 Scope . 4
2 Normative references . 4
3 Terms and definitions . 4
4 Quality assurance . 6
4.1 Qualification . 6
4.2 Acceptance . 7
4.2.1 Purpose . 7
4.2.2 Conditions . 7
4.2.3 Responsibility . 7
4.2.4 Inspection and test report . 7
5 Requirements . 7
Annex A (normative) Passivation treatment for bolts . 25
A.1 Pre-treatment . 25
A.2 Passivation . 25
A.3 Water rinse . 25
A.4 Finish . 25
Annex B (informative) Tensile, stress rupture — Areas and loads formulae . 26
B.1 Cross sectional area values . 26
B.2 Formulae . 27
B.2.1 Cross sectional area . 27
B.2.2 Test load in kN . 27
Annex C (informative) Standard evolution form . 28
Bibliography . 29
European foreword
This document (EN 2576:2020) 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 2020, and conflicting national standards
shall be withdrawn at the latest by November 2020.
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 organisations 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, Turkey and the
United Kingdom.
1 Scope
This document specifies the characteristics, qualification and acceptance requirements for bolts with MJ
threads in heat resisting steel FE-PA2601, for aerospace applications.
1 2
Classification: 900 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.
EN ISO 3452-1, Non-destructive testing — Penetrant testing — Part 1: General principles
EN ISO 4288, Geometrical Product Specifications (GPS) — Surface texture: Profile method — Rules and
procedures for the assessment of surface texture
EN ISO 6508-1, Metallic materials — Rockwell hardness test — Part 1: Test method
EN ISO 6892-1, Metallic materials — Tensile testing — Part 1: Method of test at room temperature
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 5855-2, Aerospace — MJ threads — Part 2: Limit dimensions for bolts and nuts
ISO 7961, Aerospace — Bolts — Test methods
ASTM E 112, Standard Test Methods for Determining Average Grain Size
3 Terms and 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:
— ISO Online browsing platform: available at http://www.iso.org/obp
— IEC Electropedia: available at http://www.electropedia.org/
Minimum tensile strength of the material at ambient temperature.
Maximum test temperature of the parts.
3 Published by: ASTM International (http://www.astm.org/).
3.1
batch
quantity of finished parts, of the same type and same diameter, produced from the same 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
inspection lot
quantity of parts from a single production batch of the same part number which completely defines the
parts
3.3 Surface discontinuities
3.3.1
crack
rupture in the material which may extend in any direction and which may be intercrystalline or
transcrystalline in character
3.3.2
seam
longitudinal surface discontinuity in the form of an unwelded open fold in the material
3.3.3
lap
surface discontinuity caused by folding over metal fins or sharp corners and then rolling or forging
them into the surface
3.3.4
inclusion
non-metallic particles originating from the material manufacturing process
Note 1 to entry: These particles may be isolated or arranged in strings extending longitudinally.
3.4
test temperature
ambient temperature, unless otherwise specified
3.5
simple random sampling
the 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
3.6
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
3.7
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
3.8
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
3.9
sampling plan
plan according to which one or more samples are taken in order to obtain information and possibly to
reach a decision
3.10
limiting quality
LQ
quality level in a sampling plan which corresponds to a specified and relatively low probability of
acceptance, in this case 10 % probability of acceptance
Note 1 to entry: It is the limiting lot quality characteristic that a lot of this quality would occur.
3.11
acceptance quality limit
AQL
quality limit which in a sampling plan corresponds to a specified but relatively high probability of
acceptance
Note 1 to entry: 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.
3.12
finished bolt
bolt ready for use, inclusive of any possible treatments and/or surface coatings, as specified in the
product standard or definition document
3.13
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, number 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 inspection lot by simple random sampling.
The test programme may possibly be reduced, or the qualification of a bolt 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 manufact
...
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