Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - Sheet and strip - 0,4 mm <a <6 mm

This standard specifies the requirements relating to:
Aluminium alloy AL-P2014A
T4 or T42
Sheet and strip
0,4 mm < or = a < or = 6 mm
for aerospace application.

Luft- und Raumfahrt - Aluminiumlegierung AL-P2014A-T4 oder T42 - Bleche und Bänder - 0,4 mm <a <6 mm

Diese Norm legt die Anforderungen an
Aluminiumlegierung AL-P2014A
T4 oder T42
Bleche und Bänder
0,4 mm >= a >= 6 mm
für Anwendungen in der Luft- und Raumfahrt fest.

Série aérospatiale - Alliage d'aluminium AL-P2014A-T4 ou T42 - Tôles et bandes - 0,4 mm <a <6 mm

Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - Sheet and strip - 0,4 mm <a <6 mm

General Information

Status
Published
Publication Date
31-Oct-2005
ICS
49.025.20 - Aluminium
Technical Committee
SS SPL - Technical Board for the general field
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
01-Nov-2005
Due Date
01-Nov-2005
Completion Date
01-Nov-2005
Ref Project
EN 2395:2005 - Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - Sheet and strip - 0,4 mm <a <6 mm

Relations

Replaces
SIST EN 2395:2001 - Aerospace series - Aluminium alloy AL-P2014A - T4 or T42 - Sheet and strip 0,4 mm <= a <= 6 mm
Effective Date
22-Dec-2008

Overview

SIST EN 2395:2005 is a European standard established by the European Committee for Standardization (CEN) focusing on aluminum alloy AL-P2014A in sheet and strip form. Specifically designed for aerospace applications, this standard covers the technical requirements for aluminum alloy sheets and strips with thickness ranging from 0.4 mm to 6 mm. The alloy is available in temper conditions T4 and T42, providing enhanced mechanical properties suitable for demanding aerospace environments.

This standard ensures uniformity and quality across aluminum products used in aerospace manufacturing, streamlining procurement and compliance for manufacturers and suppliers.

Key Topics

  • Material Scope:
    Aluminum alloy AL-P2014A in sheet and strip forms with thickness 0.4 mm ≤ a ≤ 6 mm.
  • Temper Conditions:
    • T4: Solution heat-treated and naturally aged.
    • T42: Heat treated with controlled artificial aging.
  • Chemical Composition:
    Specified limits on elements such as Si, Fe, Cu, Mn, Mg, Cr, Ni, Zn, Ti, and Zr to ensure alloy integrity and performance.
  • Mechanical Properties:
    • Minimum proof stress (Rp0.2) ≥ 255 MPa.
    • Tensile strength (Rm) ≥ 400 MPa.
    • Elongation at break (A50) ≥ 14%.
  • Manufacturing Processes:
    Rolled sheet and strip production with strict dimensional tolerances.
  • Testing and Inspection:
    Requirements for test samples, dimensional inspection, external defect checks, intergranular corrosion resistance, and marking according to aerospace quality standards.
  • Delivery Conditions:
    Defined heat treatment and aging cycles for consistent mechanical properties during use in aerospace assemblies.
  • Corrosion Resistance:
    Intergranular corrosion testing to meet aerospace reliability needs.
  • Batch Uniformity & Product Qualification:
    Supplier and purchaser agreement on qualification program ensuring batch consistency and adherence to the standard.

Applications

SIST EN 2395:2005 aluminum alloy AL-P2014A sheets and strips are primarily used in aerospace manufacturing due to their:

  • High strength-to-weight ratio essential for aircraft structures.
  • Excellent machinability and formability in T4 and T42 tempers, enabling complex part fabrication.
  • Good fatigue resistance critical for dynamic aerospace components.
  • Corrosion resistance tailored to the harsh environmental conditions encountered during flight.
  • Typical aerospace parts include fuselage skins, structural aircraft components, brackets, and supports where thin, high-strength aluminum sheets are required.

By adhering to SIST EN 2395:2005, aerospace manufacturers ensure reliable material performance, facilitate certification processes, and meet international market expectations.

Related Standards

  • EN 4258: General organization of aerospace metallic material standards – provides structural guidance for series like EN 2395.
  • EN 4400-2: Technical specifications for aluminum and aluminum alloy wrought products, particularly sheets and strips, which underpin the manufacturing and testing methods referenced in EN 2395.
  • EN 4500-2: Rules for drafting and presentation of aerospace metallic material standards for aluminum and magnesium alloys, aligning documentation and compliance practices.

Compliance with SIST EN 2395:2005 in conjunction with these related standards ensures integrated quality management across aerospace aluminum materials, fostering interoperability and supplier transparency.

Keywords: SIST EN 2395:2005, aluminum alloy AL-P2014A, aerospace aluminum sheets, T4 temper, T42 temper, aerospace materials standard, aluminum sheet and strip, aerospace manufacturing, aluminum alloy specifications, aerospace corrosion resistance, rolled aluminum alloy.

Frequently Asked Questions

SIST EN 2395:2005 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - Sheet and strip - 0,4 mm <a <6 mm". This standard covers: This standard specifies the requirements relating to: Aluminium alloy AL-P2014A T4 or T42 Sheet and strip 0,4 mm < or = a < or = 6 mm for aerospace application.

This standard specifies the requirements relating to: Aluminium alloy AL-P2014A T4 or T42 Sheet and strip 0,4 mm < or = a < or = 6 mm for aerospace application.

SIST EN 2395:2005 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.

SIST EN 2395:2005 has the following relationships with other standards: It is inter standard links to SIST EN 2395:2001. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

SIST EN 2395:2005 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-november-2005
1DGRPHãþD
SIST EN 2395:2001
Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - Sheet and strip - 0,4
mm Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - Sheet and strip - 0,4 mm <6 mm
Luft- und Raumfahrt - Aluminiumlegierung AL-P2014A-T4 oder T42 - Bleche und Bänder
- 0,4 mm Série aérospatiale - Alliage d'aluminium AL-P2014A-T4 ou T42 - Tôles et bandes - 0,4
mm Ta slovenski standard je istoveten z: EN 2395:2005
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD EN 2395
NORME EUROPÉENNE
EUROPÄISCHE NORM
June 2005
ICS 49.025.20 Supersedes EN 2395:1994
English version
Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 -
Sheet and strip - 0,4 mm ≤a ≤6 mm
Série aérospatiale - Alliage d'aluminium AL-P2014A-T4 ou Luft- und Raumfahrt - Aluminiumlegierung AL-2014A-
T42 - Tôles et bandes - 0,4 mm ≤a ≤6 mm T4 oder T42 - Bleche und Bänder - 0,4 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,
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 2395:2005: E
worldwide for CEN national Members.

Foreword
This document (EN 2395:2005) 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.
This document supersedes EN 2395:1994.
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, Netherl
...

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