SIST EN 3270:2004
(Main)Aerospace series - Pipe coupling 8°30' in titanium alloy - Blanking plugs with lockring
Aerospace series - Pipe coupling 8°30' in titanium alloy - Blanking plugs with lockring
This standard specifies the characteristics for blanking plugs with lockring for pipe couplings 8°30', in titanium alloy, for aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range: - 55 °C to + 135 °C
Luft- und Raumfahrt - Rohrverschraubung 8°30' aus Titanlegierung - Verschlußschrauben mit Sicherungsring
Série aérospatiale - Systeme de raccordement 8°30' en alliage de titane - Obturateurs filetés avec bague de freinage
Aerospace series - Pipe coupling 8°30' in titanium alloy - Blanking plugs with lockring
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Standards Content (Sample)
SLOVENSKI STANDARD
SIST EN 3270:2004
01-maj-2004
Aerospace series - Pipe coupling 8°30' in titanium alloy - Blanking plugs with
lockring
Aerospace series - Pipe coupling 8°30' in titanium alloy - Blanking plugs with lockring
Luft- und Raumfahrt - Rohrverschraubung 8°30' aus Titanlegierung -
Verschlußschrauben mit Sicherungsring
Série aérospatiale - Systeme de raccordement 8°30' en alliage de titane - Obturateurs
filetés avec bague de freinage
Ta slovenski standard je istoveten z: EN 3270:2001
ICS:
49.030.20 Sorniki, vijaki, stebelni vijaki Bolts, screws, studs
SIST EN 3270:2004 en
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
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SIST EN 3270:2004
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SIST EN 3270:2004
EUROPEAN STANDARD
EN 3270
NORME EUROPÉENNE
EUROPÄISCHE NORM
October 2001
ICS 49.030.20
English version
Aerospace series - Pipe coupling 8°30' in titanium alloy -
Blanking plugs with lockring
Série aérospatiale - Système de raccordement 8°30' en Luft- und Raumfahrt - Rohrverschraubung 8°30' aus
alliage de titane - Obturateurs filetés avec bague de Titanlegierung - Verschlußschrauben mit Sicherungsring
freinage
This European Standard was approved by CEN on 6 January 2001.
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 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 Management Centre has the same status as the official
versions.
CEN members are the national standards bodies of Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece,
Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, 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
© 2001 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 3270:2001 E
worldwide for CEN national Members.
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SIST EN 3270:2004
EN 3270:2001 (E)
Foreword
This European Standard has been prepared by the European Association of Aerospace Manufacturers
(AECMA).
After inquiries 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 April 2002, and conflicting national standards shall be withdrawn at
the latest by April 2002.
According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following
countries are bound to implement this European Standard: Austria, Belgium, Czech Republic, Denmark,
Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal,
Spain, Sweden, Switzerland and the United Kingdom.
2
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SIST EN 3270:2004
EN 3270:2001 (E)
1 Scope
This standard specifies the characteristics for blanking plugs with lockring for pipe couplings 830', in titanium
alloy, for aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range: – 55 C to + 135 C
2 Normative references
This European Standard inco
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