EN 4002:2007
(Main)Aerospace series - Aluminium alloy AL-P2219-T81 - Sheet and strip 0,5 mm ≤ a ≤ 6 mm
Aerospace series - Aluminium alloy AL-P2219-T81 - Sheet and strip 0,5 mm ≤ a ≤ 6 mm
This standard specifies the requirements relating to:
Aluminium alloy AL-P2219-T81 - Sheet and strip 0,5 mm
Luft- und Raumfahrt - Aluminiumlegierung AL-P2219-T81 - Bleche und Bänder 0,5 mm a 6 mm
Série aérospatiale - Alliage d'aluminium AL-P2219-T81 - Tôles et bandes 0,5 mm a 6 mm
Aeronavtika - Aluminijeva zlitina AL-P2219-T81 - Pločevina in trakovi 0,5 mm <= a <= 6 mm
General Information
- Status
- Published
- Publication Date
- 21-Aug-2007
- Withdrawal Date
- 28-Feb-2008
- Technical Committee
- ASD-STAN - Aerospace
- Drafting Committee
- ASD-STAN/D 4 - Metallic
- Current Stage
- 6060 - Definitive text made available (DAV) - Publishing
- Start Date
- 22-Aug-2007
- Completion Date
- 22-Aug-2007
Relations
- Effective Date
- 28-Jan-2026
Overview
EN 4002:2007 (CEN) defines the requirements for aerospace series aluminium alloy AL-P2219-T81 in the form of sheet and strip with thicknesses from 0.5 mm to 6 mm. This European Standard is part of the EN metallic material standards for aerospace applications and references general organization and product-specific rules such as EN 4258, EN 4400-2 and EN 4500-2.
The standard covers designation, production form, delivery conditions, heat treatments, mechanical and chemical requirements, and inspection practices relevant to aircraft components where AL-P2219-T81 is selected for its strength and processing characteristics.
Key Topics
- Material designation and form: Aluminium alloy AL-P2219-T81 - sheet and strip, rolled products.
- Thickness range: 0.5 mm ≤ a ≤ 6 mm.
- Delivery and use conditions: Delivery codes include T31 and T81; the use condition is T81.
- Heat treatment: Solution treatment at
530 °C to 540 °C with water quench (WQ) to ≤ 40 °C, followed by cold work (1%) and artificial aging at 171 °C to 182 °C for 16–20 h (as specified for T81 condition). - Chemical composition: The standard provides alloy element ranges for AL‑P2219 (e.g., Cu as a base alloying element with defined min/max limits) consistent with aerospace alloy specification practice (see EN 4002 tables).
- Mechanical properties: Typical requirements include proof stress (R_p0.2) ≥ 320 MPa and tensile strength ≥ 430 MPa, with specified minimum elongation values depending on thickness (e.g., A ≥ 6 % or A ≥ 7 % for 50 mm gauge).
- Inspection & testing: Dimensional and marking inspections and test piece selection are referenced to EN 4400-2. Product qualification programs are to be agreed between manufacturer and purchaser.
Applications
EN 4002:2007 supports selection and procurement of AL-P2219-T81 for aerospace structural and non-structural parts where a high-strength, heat-treatable aluminium alloy is required. Typical application considerations include:
- Aircraft structural components requiring good tensile strength and toughness.
- Forming and fabrication processes for rolled sheet and strip in thickness range 0.5–6 mm.
- Parts subject to defined heat-treatment cycles and post-treatment property verification.
Benefits for specifiers and manufacturers:
- Clear, harmonized material and inspection requirements for cross-border procurement in CEN member states.
- Reduced ambiguity in delivery conditions, mechanical acceptance criteria and testing procedures.
Related Standards
- EN 4258 - organization of aerospace metallic material standards and links between EN types.
- EN 4400-2 - technical specification for aluminium and aluminium alloy sheet and strip (referenced for tests, specimens and inspection rules).
- EN 4500-2 - rules for drafting and presentation for aluminium alloy material standards.
For procurement, certification and qualification actions, consult EN 4400-2 and coordinate product qualification programmes between manufacturer and purchaser as indicated in EN 4002:2007.
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Frequently Asked Questions
EN 4002:2007 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Aluminium alloy AL-P2219-T81 - Sheet and strip 0,5 mm ≤ a ≤ 6 mm". This standard covers: This standard specifies the requirements relating to: Aluminium alloy AL-P2219-T81 - Sheet and strip 0,5 mm <or= a <or= 6 mm for aerospace applications.
This standard specifies the requirements relating to: Aluminium alloy AL-P2219-T81 - Sheet and strip 0,5 mm <or= a <or= 6 mm for aerospace applications.
EN 4002:2007 is classified under the following ICS (International Classification for Standards) categories: 77.150.10 - Aluminium products. The ICS classification helps identify the subject area and facilitates finding related standards.
EN 4002:2007 has the following relationships with other standards: It is inter standard links to EN 4258:2024. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
EN 4002:2007 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-2007
$HURQDYWLND$OXPLQLMHYD]OLWLQD$/3 73ORþHYLQDLQWUDNRYLPP D
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Aerospace series - Aluminium alloy AL-P2219-T81 - Sheet and strip 0,5 mm <= a <= 6
mm
Luft- und Raumfahrt - Aluminiumlegierung AL-P2219-T81 - Bleche und Bänder 0,5 mm
<= a <= 6 mm
Série aérospatiale - Alliage d'aluminium AL-P2219-T81 - Tôles et bandes 0,5 mm <= a
<= 6 mm
Ta slovenski standard je istoveten z: EN 4002:2007
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EUROPEAN STANDARD
EN 4002
NORME EUROPÉENNE
EUROPÄISCHE NORM
August 2007
ICS 77.150.10
English Version
Aerospace series - Aluminium alloy AL-P2219-T81 - Sheet and
strip 0,5 mm ≤ a ≤ 6 mm
Série aérospatiale - Alliage d'aluminium AL-P2219-T81 - Luft- und Raumfahrt - Aluminiumlegierung AL-P2219-T81 -
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 12 June 2006.
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 CEN Management Centre 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 CEN Management Centre has the same status as the
official versions.
CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland,
France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal,
Romania, 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
© 2007 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4002:2007: E
worldwide for CEN national Members.
Contents
Foreword.3
Introduction .4
1 Scope .4
2 Normative references .4
Foreword
This document (EN 4002:2007) has been prepared by the AeroSpace and Defense Industries Association of
Europe - Standardization (ASD-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 ASD,
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 2008, and conflicting national standards shall be withdrawn
at the latest by February 2008.
According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following
countries are bound to implement this
...
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