SIST EN 4009:2005

SLOVENSKI STANDARD
SIST EN 4009:2005
01-junij-2005
1DGRPHãþD
SIST EN 4009:2004
Aerospace series - Bolts, double hexagon head, close tolerance shank, medium
length thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) -
Classification: 1 550 MPa (at ambient temperature) / 650 °C
Aerospace series - Bolts, double hexagon head, close tolerance shank, medium length
thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) - Classification: 1 550
MPa (at ambient temperature) / 650 °C
Luft- und Raumfahrt - Zwölfkant-Passschrauben, mittlere Gewindelänge, aus
hochwarmfester Nickelbasislegierung NI-PH2601 (Inconel 718) - Klasse: 1 550 MPa (bei
Raumtemperatur)/650 °C
Série aérospatiale - Vis a tete bihexagonale, fut a tolérance serrée, filetage moyen, en
alliage résistant a chaud a base de nickel NI-PH2601 (Inconel 718) - Classification : 1
550 MPa (a température ambiante) / 650 °C
Ta slovenski standard je istoveten z: EN 4009:2004
ICS:
49.030.20 Sorniki, vijaki, stebelni vijaki Bolts, screws, studs
SIST EN 4009:2005 en
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

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SIST EN 4009:2005

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SIST EN 4009:2005



EUROPEAN STANDARD
EN 4009

NORME EUROPÉENNE

EUROPÄISCHE NORM
November 2004
ICS 49.030.20 Supersedes EN 4009:2003
English version
Aerospace series - Bolts, double hexagon head, close tolerance
shank, medium length thread, in heat resisting nickel base alloy
NI-PH2601 (Inconel 718) - Classification: 1 550 MPa (at ambient
temperature) / 650° C
Série aérospatiale - Vis à tête bihexagonale, fût à tolérance Luft- und Raumfahrt - Zwölfkant-Paßschrauben, mittlere
serrée, filetage moyen, en alliage résistant à chaud à base Gewindelänge, aus hochwarmfester Nickelbasislegierung
de nickel NI-PH2601 (Inconel 718) - Classification : 1 550 NI-PH2601 (Inconel 718) - Klasse: 1 550 MPa (bei
MPa (à température ambiante) / 650° C Raumtemperatur) / 650° C
This European Standard was approved by CEN on 11 September 2003.

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 Central Secretariat 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 Central Secretariat has the same status as the official
versions.

CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France,
Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia,
Slovenia, Spain, Sweden, Switzerland and United Kingdom.




EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION

EUROPÄISCHES KOMITEE FÜR NORMUNG

Management Centre: rue de Stassart, 36  B-1050 Brussels
© 2004 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4009:2004: E
worldwide for CEN national Members.

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SIST EN 4009:2005

EN 4009:2004 (E)
Contents                                                                         Page

Foreword.3
1 Scope .4
2 Normative references .4
3 Required characteristics.4
4 Designation .8
5 Marking .8
6 Technical specification .8
2

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SIST EN 4009:2005

EN 4009:2004 (E)
Foreword
This document (EN 4009:2004) has been prepared by the European Association of Aerospace
Manufacturers - Standardization (AECMA-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
AECMA, 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 May 2005, and conflicting national standards shall be withdrawn at
the latest by May 2005.
This document supersedes EN 4009:2003.
According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following
countries are bound to implement this European Standard: Austria, Belgium, Cyprus, Czech Republic,
Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania,
Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland
and United Kingdom.
3

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SIST EN 4009:2005

EN 4009:2004 (E)
1 Scope
This standard specifies the characteristics of double hexagon headed bolts, with close tolerance shank and
medium length thread, in NI-PH2601, for aerospace applications.
1) 2)
Classification: 1 550 MPa / 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.
ISO 3353-1, Aerospace – Lead and runout threads – Part 1: Rolled external threads
ISO 4095, Aerospace – Bihexagonal drives – Wrenching configuration – Metric series
ISO 5855-2, Aerospace – MJ threads – Part 2: Limit dimensions for bolts and nuts
EN 2424, Aerospace series – Marking of aerospace products
EN 2952, Aerospace series – Heat resisting alloy NI-PH2601 – Solution treated and cold worked – Bar for
3)
forged fasteners – D ≤ 50 mm – 1 270 MPa ≤ R ≤ 1 550 MPa
m
EN 3666, Aerospace series – Heat resisting alloy NI-PH2601 – Solution treated and cold
...