EN 2702:2005
(Main)Aerospace series - Aluminium alloy AL-P6061 - T6 or T62 - Drawn or extruded bar and section - a or D
Aerospace series - Aluminium alloy AL-P6061 - T6 or T62 - Drawn or extruded bar and section - a or D <or= 200 mm
This standard specifies the requirements relating to:
Aluminium alloy AL-P6061-
T6 or T62
Drawn or extruded bar and section
a or D < or = 200 mm
for aerospace application.
Luft- und Raumfahrt - Aluminiumlegierung AL-P6061-T6 oder T62 - Gezogene oder stranggepresste Stangen und Profile - a oder D 200 mm
Diese Norm legt die Anforderungen an
Aluminiumlegierung AL-P6061
T6 oder T62
Gezogene oder stranggepresste Stangen und Profile
a oder D £ 200 mm
für Anwendungen in der Luft- und Raumfahrt fest.
Série aérospatiale - Alliage d'aluminium AL-P6061 - T6 ou T62 - Barres et profilés filés ou étirés - a ou D <or= 200 mm
Aeronavtika – Aluminijeva zlitina AL-P6061 - T6 ali T62 – Vlečene ali iztiskane palice in profili - a ali D ? 200 mm
General Information
- Status
- Published
- Publication Date
- 25-Oct-2005
- Withdrawal Date
- 29-Apr-2006
- Technical Committee
- ASD-STAN - Aerospace
- Drafting Committee
- ASD-STAN/D 4 - Metallic
- Current Stage
- 6060 - Definitive text made available (DAV) - Publishing
- Start Date
- 26-Oct-2005
- Completion Date
- 26-Oct-2005
Relations
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
Overview
EN 2702:2005 is a CEN/AECMA aerospace material standard that specifies requirements for Aluminium alloy AL-P6061 in the T6 or T62 tempers. It applies to drawn or extruded bar and section forms with dimensions a or D ≤ 200 mm, intended for aerospace applications. The standard is part of the EN metallic materials series and is prepared in accordance with EN 4500-2 and the general organization described in EN 4258.
EN 2702:2005 sets out delivery conditions, required mechanical characteristics and references to technical specification EN 4400-3 for bar and section products. It ensures consistent material properties, production control and inspection practices important to aircraft manufacturers and suppliers.
Key Topics
- Material designation: AL-P6061 with specified chemical composition ranges (Si, Fe, Cu, Mn, Mg, Cr, Zn, Ti, Al) as referenced in the standard.
- Tempers and delivery conditions: T6 and T62 are covered; delivery condition codes and heat treatment routes are specified (see EN 4400-3 for detailed technical specification).
- Forms and production: Applies to drawn or extruded bars and sections (a or D ≤ 200 mm).
- Mechanical requirements: Minimum characteristic values are given in the standard, including proof stress (Rp0.2 ≥ 245 MPa), tensile strength (Rm ≥ 270 MPa) and elongation (A ≥ 10 % for 50 mm gauge).
- Testing and inspection: Test sample rules, dimensional and marking inspections, and limits on external/internal defects are referenced to EN 4400-3.
- Qualification: Product qualification and a qualification programme are to be agreed between manufacturer and purchaser, per EN 4400-3.
Applications
EN 2702:2005 is targeted at aerospace component manufacturers, material suppliers and procurement teams who require certified aluminium wrought products for structural or secondary aircraft parts. Typical practical values of adopting this standard include:
- Assured mechanical performance for structural design and assembly.
- Consistent heat treatment and temper control to achieve repeatable properties across production batches.
- Clear inspection and acceptance criteria that facilitate supplier qualification and traceability.
Use cases include structural bars, machined components from extruded profiles, and other aerospace parts where AL-P6061 in T6 or T62 condition is appropriate and where the cross-section or diameter does not exceed 200 mm.
Related Standards
- EN 4400-3 - Aerospace series: Aluminium and aluminium alloy wrought products - Technical specification: Part 3: Bar and section (normative reference for tests and specifications).
- EN 4258 - General organization of standardization for aerospace metallic materials.
- EN 4500-2 - Rules for drafting and presentation of metallic material standards (specific rules for aluminium alloys).
For procurement and technical implementation, users should consult EN 4400-3 and the referenced EN documents to apply the full set of material, testing and inspection requirements mandated by EN 2702:2005.
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Frequently Asked Questions
EN 2702:2005 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Aluminium alloy AL-P6061 - T6 or T62 - Drawn or extruded bar and section - a or D <or= 200 mm". This standard covers: This standard specifies the requirements relating to: Aluminium alloy AL-P6061- T6 or T62 Drawn or extruded bar and section a or D < or = 200 mm for aerospace application.
This standard specifies the requirements relating to: Aluminium alloy AL-P6061- T6 or T62 Drawn or extruded bar and section a or D < or = 200 mm for aerospace application.
EN 2702:2005 is classified under the following ICS (International Classification for Standards) categories: 49.025.20 - Aluminium. The ICS classification helps identify the subject area and facilitates finding related standards.
EN 2702:2005 has the following relationships with other standards: It is inter standard links to EN 4258:2024, EN 3475-604:2010. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
EN 2702:2005 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.
Standards Content (Sample)
SLOVENSKI STANDARD
01-julij-2006
$HURQDYWLND±$OXPLQLMHYD]OLWLQD$/37DOL7±9OHþHQHDOLL]WLVNDQH
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Aerospace series - Aluminium alloy AL-P6061 - T6 or T62 - Drawn or extruded bar and
section - a or D
Luft- und Raumfahrt - Aluminiumlegierung AL-P6061-T6 oder T62 - Gezogene oder
stranggepresste Stangen und Profile - a oder D 200 mm
Série aérospatiale - Alliage d'aluminium AL-P6061 - T6 ou T62 - Barres et profilés filés
ou étirés - a ou D
Ta slovenski standard je istoveten z: EN 2702:2005
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EUROPEAN STANDARD EN 2702
NORME EUROPÉENNE
EUROPÄISCHE NORM
October 2005
ICS 49.025.20
English Version
Aerospace series - Aluminium alloy AL-P6061 - T6 or T62 -
Drawn or extruded bar and section - a or D ≤ 200 mm
Série aérospatiale - Alliage d'aluminium AL-P6061 - T6 ou Luft- und Raumfahrt - Aluminiumlegierung AL-P6061 - T6
oder T62 - Gezogene oder Stranggepreßte Stangen und
T62 - Barres et profilés filés ou étirés - a ou D ≤ 200 mm
Profile - a oder D ≤ 200 mm
This European Standard was approved by CEN on 19 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 Ref. No. EN 2702:2005: E
worldwide for CEN national Members.
Contents Page
Foreword .3
Introduction.4
1 Scope.4
2 Normative references.4
Foreword
This European Standard (EN 2702:2005) 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
right
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