EN 4313:2005

Aerospace series - Aluminium alloy AL-P6013-T6 - Sheet and strip - 0,5 mm <a <6 mm

This standard specifies the requirements relating to:
Aluminium alloy AL-P6013-
T6
Sheet and strip
0,5 mm < or = a < or = 6 mm
for aerospace application.

Luft- und Raumfahrt - Aluminiumlegierung AL-P6013-T6 - Bleche und Bänder - 0,5 mm <a <6 mm

Diese Norm legt die Anforderungen an
Aluminiumlegierung AL P6013-T6
Bleche und Bänder
0,5 mm £ a £ 6 mm
für Anwendungen in der Luft- und Raumfahrt fest.

Série aérospatiale - Alliage d'aluminium AL-P6013-T6 - Tôles et bandes - 0,5 mm <a <6 mm

Aerospace series - Aluminium alloy AL-P6013-T6 - Sheet and strip - 0,5 mm <a <6 mm

General Information

• Status: Published
• Publication Date: 21-Jun-2005
• Withdrawal Date: 30-Dec-2005
• ICS: 49.025.20 - Aluminium
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 4 - Metallic
• Current Stage: 6060 - Definitive text made available (DAV) - Publishing
• Start Date: 22-Jun-2005
• Completion Date: 22-Jun-2005
• Ref Project: SIST EN 4313:2005 - Aerospace series - Aluminium alloy AL-P6013-T6 - Sheet and strip - 0,5 mm <a <6 mm

Overview

EN 4313:2005 is a European standard developed by CEN that specifies the technical requirements for aluminium alloy AL-P6013-T6 in sheet and strip forms, with thickness ranging from 0.5 mm to 6 mm. Designed specifically for aerospace applications, this standard ensures consistent material quality, chemical composition, mechanical properties, and production methods to meet the stringent demands of the aerospace industry. This standard is part of the broader aerospace metallic materials series and aligns with other European standards for aluminum alloys to facilitate uniformity across manufacturers and users.

Key Topics

• Material Designation: Aluminium alloy AL-P6013-T6, a heat-treatable aluminum alloy known for its strength and corrosion resistance suitable for aerospace structures.
• Dimensions: Applies to sheets and strips with thickness between 0.5 mm and 6 mm, addressing commonly used dimensions in aerospace manufacturing.
• Chemical Composition: Includes precise limits for critical alloying elements such as silicon, iron, copper, manganese, magnesium, chromium, zinc, titanium, and aluminum to ensure performance and reliability.
• Heat Treatment: Specifies delivery conditions T4 (solution heat-treated) and T6 (solution heat-treated and artificially aged), with detailed temperature and duration requirements to achieve desired mechanical properties.
• Mechanical Properties: Defines proof stress (minimum 315 MPa in T6), tensile strength (minimum 360 MPa in T6), elongation (minimum 8% in T6), and other physical properties critical for structural applications.
• Manufacturing Processes: Sheets and strips are to be produced by rolling, with strict quality control for external defects, batch uniformity, and dimensional tolerances.
• Testing and Inspection: References EN 4400-2 for sampling, testing methodologies, marking, and dimensional inspections to maintain standard compliance.
• Standardization Compliance: Developed following EN 4500-2 guidelines and coordinated within the aerospace material standards framework described in EN 4258.

Applications

• Aerospace Structural Components: Ideal for manufacturer of aircraft fuselage, wing skins, and structural components that require lightweight, strong, and corrosion-resistant materials.
• Precision Sheet Metal Fabrication: Enables production of high-performance aerospace sheet metal parts with predictable mechanical characteristics for reliable operation in demanding environments.
• Aerospace Manufacturing: Supports suppliers and manufacturers in adhering to uniform quality and performance criteria, critical for safety, certification, and international collaboration.
• Material Qualification: Used by purchasing entities and manufacturers to define and verify aluminium alloy material quality through agreed qualification programs.

Related Standards

• EN 4258: Provides the general organization for metallic material standards within aerospace applications, establishing the framework for EN 4313.
• EN 4400-2: Specifies technical requirements for aluminium and aluminium alloy wrought products including sheet and strip materials which EN 4313 references for testing and inspection protocols.
• EN 4500-2: Details the rules for drafting and presenting material standards specifically related to aluminium alloys, ensuring clarity and consistency across EN 4313 and related documents.

By conforming to the EN 4313:2005 standard, aerospace manufacturers ensure the use of aluminium alloy AL-P6013-T6 sheets and strips that meet rigorous European aerospace industry requirements, thus promoting safety, interoperability, and quality in aircraft production.

Standards Content (Sample)

SLOVENSKI STANDARD
01-november-2005
Aerospace series - Aluminium alloy AL-P6013-T6 - Sheet and strip - 0,5 mm mm
Aerospace series - Aluminium alloy AL-P6013-T6 - Sheet and strip - 0,5 mm Luft- und Raumfahrt - Aluminiumlegierung AL-P6013-T6 - Bleche und Bänder - 0,5 mm
Série aérospatiale - Alliage d'aluminium AL-P6013-T6 - Tôles et bandes - 0,5 mm mm
Ta slovenski standard je istoveten z: EN 4313:2005
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD EN 4313
NORME EUROPÉENNE
EUROPÄISCHE NORM
June 2005
ICS 49.025.20
English version
Aerospace series - Aluminium alloy AL-P6013-T6 - Sheet and
strip - 0,5 mm ≤a ≤6 mm
Série aérospatiale - Alliage d'aluminium AL-P6013-T6 - Luft- und Raumfahrt - Aluminiumlegierung AL-P6013-T6 -
Tôles et bandes - 0,5 mm ≤a ≤6 mm Bleche und Bänder - 0,5 mm ≤a ≤6 mm
This European Standard was approved by CEN on 22 April 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,
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© 2005 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4313:2005: E
worldwide for CEN national Members.

Foreword
This document (EN 4313:2005) 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 December 2005, and conflicting national standards shall be withdrawn
at the latest by December 2005.
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 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, Ita
...