Aerospace series - Aluminium alloy AL-P7075 - T73511 - Extruded bar and section - a or D <or= 150 mm with peripheral coarse grain control

This standard specifies the requirements relating to:
Aluminium alloy AL-P7075-
T73511
Extruded bar and section
a or D with peripheral coarse grain control
for aerospace application.
This standard may also be used to supply material in the T73510 condition if specified by the purchaser on the order and the product is marked accordingly.

Luft- und Raumfahrt - Aluminiumlegierung AL-P7075 - T73511 - Stranggepresste Stange und Profile - a oder D <or= 150 mm mit Kontrolle der Grobkornrandzone

Diese Norm legt die Anforderungen an
Aluminiumlegierung AL-P7075-
T73511
stranggepresste Stangen und Profile
a oder D  150 mm
mit Kontrolle der Grobrandzone
für Anwendungen in der Luft- und Raumfahrt fest.
Diese Norm kann auch für die Lieferung des Werkstoffs im Zustand T73510 verwendet werden, wenn der Käufer dies in der Bestellung angibt und das Halbzeug entsprechend gekennzeichnet ist.

Série aérospatiale - Alliage d'aluminium AL-P7075 - T73511 - Barres et profilés filés - a ou D <or= 150 mm avec contrôle de la zone périphérique à gros grains

Aeronavtika – Aluminijeva zlitina AL-P7075 - T73511 – Iztiskane palice in profili - a ali D ? 150 mm s kontrolo debelozrnatega obrobja

General Information

Status
Published
Publication Date
25-Oct-2005
Withdrawal Date
29-Apr-2006
Technical Committee
Drafting Committee
Current Stage
6060 - Definitive text made available (DAV) - Publishing
Start Date
26-Oct-2005
Completion Date
26-Oct-2005

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Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Aluminium alloy AL-P7075 - T73511 - Extruded bar and section - a or D STANDARDSIST EN 2632:200601-julij-2006







EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 2632
October 2005 ICS 49.025.20 Supersedes EN 2632:1993 English Version
Aerospace series - Aluminium alloy AL-P7075 - T73511 - Extruded bar and section - a or D ≤ 150 mm with peripheral coarse grain control
Série aérospatiale - Alliage d'aluminium AL-P7075 - T73511 - Barres et profilés filés - a ou D ≤ 150 mm avec contrôle de la zone périphérique à gros grains
Luft- und Raumfahrt - Aluminiumlegierung AL-P7075 - T73511 - Stranggepreßte Stange und Profile - a oder D ≤ 150 mm mit Kontrolle der Grobkornrandzone This European Standard was approved by CEN on 26 September 2005.
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 © 2005 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2632:2005: E



EN 2632:2005 (E) 2 Contents Page Foreword.3 Introduction.4 1 Scope.4 2 Normative references.4



EN 2632:2005 (E) 3 Foreword This European Standard (EN 2632:2005) 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 April 2006, and conflicting national standards shall be withdrawn at the latest by April 2006. 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. This European Standard supersedes EN 2632:1993. 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 the United Kingdom.



EN 2632:2005 (E) 4 Introduction This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accord
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