Aerospace series - Aluminium alloy AL-P8090 - T841 - Sheet - 0,6 mm <or= a <or= 6 mm

This standard specifies the requirements relating to:
Aluminium alloy AL-P8090-
T841
Sheet
0,6 mm < or = a < or = 6 mm
for aerospace application.

Luft- und Raumfahrt - Aluminiumlegierung AL-P8090 - T841 - Bleche - 0,6 mm <or= a <or= 6 mm

Diese Norm legt die Anforderungen an
Aluminiumlegierung AL-P8090-
T841
Bleche
0,6 mm £ a £ 6 mm
für Anwendungen in der Luft- und Raumfahrt fest.

Série aérospatiale - Alliage d'aluminium AL-P8090 - T841 - Tôles - 0,6 mm <or= a <or= 6 mm

Aerospace series - Aluminium alloy AL-P8090 - T841 - Sheet - 0,6 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 4204:2005 is a European Standard developed by the European Committee for Standardization (CEN) that specifies requirements for the aerospace-grade aluminium alloy AL-P8090 in the T841 temper condition. This standard applies to rolled sheets with thicknesses ranging from 0.6 mm to 6 mm designed for aerospace applications. The material is part of a series of EN metallic material standards aimed at ensuring high-quality, consistent aerospace components. Compliance with EN 4204:2005 ensures materials meet strict chemical composition, mechanical properties, and manufacturing process standards demanded by the aerospace industry.

Key Topics

  • Material Specification: Defines aluminium alloy AL-P8090 in the T841 temper condition. This alloy includes controlled amounts of copper, magnesium, zirconium, and lithium to provide a balance of strength, corrosion resistance, and lightweight properties crucial for aerospace applications.

  • Thickness Range: Sheets must have thicknesses between 0.6 mm and 6 mm, meeting precise dimensional tolerances.

  • Chemical Composition: Tight limits on elements such as silicon, iron, copper, manganese, magnesium, zinc, lithium, zirconium, titanium, and residuals to ensure consistent performance.

  • Mechanical Properties:

    • Proof stress minimum: 270 MPa
    • Tensile strength minimum: 405 MPa
    • Elongation minimum: 8% (on 50 mm gauge length)
      These properties are critical to guarantee material reliability under aerospace operational stresses.
  • Delivery Condition:

    • Material supplied in the T841 condition, involving solution heat treatment, water quenching, and controlled stretching followed by artificial aging.
    • This treatment optimizes mechanical strength and stress corrosion resistance.
  • Testing & Inspection: Mandates use of standard aerospace test samples and protocols (referencing EN 4400-2) including dimensional inspection, fracture toughness, and corrosion resistance tests.

  • Microstructure and Quality: Sheets are to be fully recrystallized per agreement, ensuring uniform grain structure and performance consistency.

  • Corrosion Resistance: Requirements limit exfoliation corrosion severity to levels not greater than grade EB, essential for longevity in demanding aerospace environments.

  • Marking & Traceability: Products must be properly marked and traceable according to aerospace standards.

Applications

  • Aerospace Manufacturing: EN 4204:2005 aluminium sheets are intended for structural aircraft components where a lightweight, high-strength metal with excellent corrosion resistance is required.

  • Aircraft Skin and Panels: Suitable for outer aircraft skins, fuselage panels, and other sheet metal parts exposed to environmental and operational stresses.

  • Spacecraft Components: The alloy’s properties also make it applicable to certain spacecraft parts requiring stringent mechanical and chemical stability.

  • High-Performance Engineering: Used in aerospace design to reduce weight while maintaining rigidity and durability, thereby improving fuel efficiency and safety.

Related Standards

  • EN 4400-2: Aerospace series technical specification for aluminium and aluminium alloy wrought products - Part 2 covers sheet and strip products, establishing testing and inspection rules complementary to EN 4204.

  • EN 4258: General organization of standardization for aerospace series metallic materials, providing framework and interrelations between different material standards.

  • EN 4500-2: Rules for drafting and presenting standards for metallic materials in aerospace, giving guidance specific to aluminium, its alloys, and magnesium alloys.

  • AECMA-STAN Documents: Based on pre-standardization efforts by the European Association of Aerospace Manufacturers, ensuring alignment with industry needs.


Keywords: EN 4204:2005, aluminium alloy AL-P8090 T841, aerospace aluminium sheet, rolled aluminium sheet aerospace, aerospace material standard, lightweight aerospace metal, corrosion-resistant aluminium, tensile strength aluminium aerospace, aerospace grade aluminium, aluminium sheet 0.6 mm to 6 mm, aerospace manufacturing materials.

Frequently Asked Questions

EN 4204:2005 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Aluminium alloy AL-P8090 - T841 - Sheet - 0,6 mm <or= a <or= 6 mm". This standard covers: This standard specifies the requirements relating to: Aluminium alloy AL-P8090- T841 Sheet 0,6 mm < or = a < or = 6 mm for aerospace application.

This standard specifies the requirements relating to: Aluminium alloy AL-P8090- T841 Sheet 0,6 mm < or = a < or = 6 mm for aerospace application.

EN 4204:2005 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 4204:2005 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-P8090 - T841 - Sheet - 0,6 mm mm
Aerospace series - Aluminium alloy AL-P8090 - T841 - Sheet - 0,6 mm mm
Luft- und Raumfahrt - Aluminiumlegierung AL-P8090 - T841 - Bleche - 0,6 mm Série aérospatiale - Alliage d'aluminium AL-P8090 - T841 - Tôles - 0,6 mm mm
Ta slovenski standard je istoveten z: EN 4204:2005
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD EN 4204
NORME EUROPÉENNE
EUROPÄISCHE NORM
August 2005
ICS 49.025.20
English Version
Aerospace series - Aluminium alloy AL-P8090 - T841 - Sheet -
0,6 mm ≤ a ≤ 6 mm
Série aérospatiale - Alliage d'aluminium AL-P8090 - T841 - Luft- und Raumfahrt - Aluminiumlegierung AL-P8090 - T841
Tôles - 0,6 mm ≤ a ≤ 6 mm - Bleche - 0,6 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 4204:2005: E
worldwide for CEN national Members.

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

Foreword
This document (EN 4204:2005) 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
countries are bound to implement this European Standard: Austria, Belgium, Cyprus, Czech Republic,
Denmark, Estonia, Fin
...

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