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

This standard specifies the requirements relating to:
Aluminium alloy AL-P2014A
T4 or T42
Clad sheet and strip
0,4 mm for aerospace application.

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

Diese Norm legt die Anforderungen an
Aluminiumlegierung AL-P2014A
T4 oder T42
Bleche und Bänder, plattiert
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 plaquées - 0,4 mm <or= a <or= 6 mm

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

General Information

Status
Published
Publication Date
23-Aug-2005
Withdrawal Date
27-Feb-2006
Technical Committee
ASD-STAN - Aerospace
Drafting Committee
ASD-STAN/D 4 - Metallic
Current Stage
6060 - Definitive text made available (DAV) - Publishing
Start Date
24-Aug-2005
Completion Date
24-Aug-2005

Overview

EN 2088:2005 is a European standard published by the Comité Européen de Normalisation (CEN) that specifies the technical requirements for aluminium alloy AL-P2014A in clad sheet and strip forms. These materials are tailored for aerospace applications, specifically covering thicknesses ranging from 0.4 mm to 6 mm. The standard applies to aluminium alloy in the T4 or T42 temper conditions, ensuring suitability for high-performance aerospace manufacturing.

This standard is part of the broader aerospace series standards designed to regulate metallic materials for aerospace use, providing uniformity in product performance, quality, and testing procedures across the European aerospace sector.

Key Topics

  • Material Specification: Defines aluminium alloy AL-P2014A clad sheet and strip, outlining the specific chemical composition limits to guarantee mechanical performance and corrosion resistance.

  • Temper Conditions: Covers T4 and T42 temper states. T4 includes solution heat-treated and naturally aged conditions, while T42 encompasses a similar heat treatment followed by controlled artificial aging, enhancing mechanical properties for aerospace needs.

  • Dimensional Range: Thickness between 0.4 mm and 6 mm, accommodating various aerospace component design requirements.

  • Cladding: Specifies the use of aluminium cladding to protect against corrosion. The cladding material is typically high-purity aluminium (AL-P1050A or AL-P1145), with defined chemical limits for elements such as silicon, iron, copper, and others.

  • Mechanical Properties: Establishes minimum mechanical criteria like proof stress, tensile strength, and elongation percentages to assure durability and structural integrity under aerospace operating conditions.

  • Testing and Inspection: Refers to established aerospace testing standards (such as EN 4400-2) for dimensional, chemical, mechanical, and surface inspections to maintain batch uniformity and inspection reliability.

Applications

EN 2088:2005 aluminium alloy AL-P2014A clad sheets and strips are critical materials used extensively within aerospace manufacturing, particularly for:

  • Aircraft structural components requiring high strength-to-weight ratios.
  • Panels and shells where corrosion resistance and durability are vital.
  • High-performance aerospace assemblies where consistent material properties guarantee safety and compliance.
  • Manufacturing processes involving rolling and forming operations that benefit from the defined temper and clad characteristics.

Compliance with EN 2088:2005 ensures aerospace manufacturers achieve consistent, reliable aluminium materials optimized for demanding flight environments, contributing to overall aircraft safety, weight efficiency, and lifecycle longevity.

Related Standards

  • EN 4258 – Aerospace series – Metallic materials – General organization of standardization. This standard provides the framework for aerospace metallic material standards, linking the use and classification of EN 2088.

  • EN 4400-2 – Aerospace series – Aluminium and aluminium alloy wrought products – Technical specification – Part 2: Sheet and strip. Provides detailed guidelines on production, testing, and inspection critical for materials meeting EN 2088 requirements.

  • EN 4500-2 – Aerospace series – Metallic materials – Rules for drafting and presentation of material standards – Part 2: Specific rules for aluminium and magnesium alloys. This standard outlines documentation and presentation rules relevant to EN 2088.

These standards collectively ensure harmonized aerospace material regulations across European nations, enabling manufacturers and suppliers to meet international performance and quality expectations.


By adhering to EN 2088:2005, aerospace engineers and manufacturers gain access to rigorously defined aluminium alloy products, supporting innovation while maintaining safety and regulatory compliance within the aerospace sector. This standard is essential for any organization involved in aerospace materials selection and production where AL-P2014A aluminium clad sheets and strips are specified.

Frequently Asked Questions

EN 2088:2005 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Aluminium alloy AL-P2014A - T4 or T42 - Clad sheet and strip - 0,4 mm <or= a <or= 6 mm". This standard covers: This standard specifies the requirements relating to: Aluminium alloy AL-P2014A T4 or T42 Clad 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 Clad sheet and strip 0,4 mm <or= a <or= 6 mm for aerospace application.

EN 2088:2005 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 2088:2005 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-december-2005
Aerospace series - Aluminium alloy AL-P2014A - T4 or T42 - Clad sheet and strip -
0,4 mm Aerospace series - Aluminium alloy AL-P2014A - T4 or T42 - Clad sheet and strip - 0,4
mm Luft- und Raumfahrt - Aluminiumlegierung AL-P2014A - T4 oder T42 - Bleche und
Bänder, plattiert - 0,4 mm Série aérospatiale - Alliage d'aluminium AL-P2014A - T4 ou T42 - Tôles et bandes
plaquées - 0,4 mm Ta slovenski standard je istoveten z: EN 2088:2005
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD EN 2088
NORME EUROPÉENNE
EUROPÄISCHE NORM
August 2005
ICS 49.025.20
English Version
Aerospace series - Aluminium alloy AL-P2014A - T4 or T42 -
Clad sheet and strip - 0,4 mm ≤ a ≤ 6 mm
Série aérospatiale - Alliage d'aluminium AL-P2014A - T4 ou Luft- und Raumfahrt - Aluminiumlegierung AL-P2014A - T4
T42 - Tôles et bandes plaquées - 0,4 mm ≤ a ≤ 6 mm oder T42 - Bleche und Bänder - Plattiert - 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 2088:2005: E
worldwide for CEN national Members.

Contents
Foreword .3
Introduction.4
1 Scope .4
2 Normative references .4

Foreword
This document (EN 2088:2005) 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 February 2006, and conflicting national standards shall be withdrawn
at the latest by February 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.
According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following
...

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