SIST EN 4214:2005

Aerospace series - Aluminium alloy AL-P7010-T651 - Plate - 6 mm <a <20 mm

This standard specifies the requirements relating to:
Aluminium alloy AL-P7010-
T651
Plate
6 mm < a < or = 20 mm
for aerospace application.

Luft- und Raumfahrt - Aluminiumlegierung AL-P7010-T651 - Platten - 6 mm <a <20 mm

Diese Norm gehört zu der Reihe von EN Normen über metallische Werkstoffe für Anwendungen in der Luft- und Raumfahrt. Die allgemeine Gliederung dieser Normenreihe ist in EN 4258 beschrieben.
Diese Norm wurde in Übereinstimmung mit EN 4500 2 erstellt.

Série aérospatiale - Alliage d'aluminium AL-P7010-T651 - Tôles épaisses - 6 mm <a <20 mm

Aerospace series - Aluminium alloy AL-P7010-T651 - Plate - 6 mm <a <20 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 4214:2005 - Aerospace series - Aluminium alloy AL-P7010-T651 - Plate - 6 mm <a <20 mm

Overview

EN 4214:2005 is a CEN (Aerospace series) standard that specifies requirements for aluminium alloy AL‑P7010‑T651 in plate form for aerospace applications. It covers rolled plates with thicknesses in the range 6 mm < a ≤ 20 mm, defining delivery conditions, heat treatment, mechanical performance, inspection and typical electrical conductivity. This standard is intended for manufacturers, purchasers and design engineers working with high‑strength aerospace aluminium plate.

Key topics and requirements

• Material and form: Aluminium alloy AL‑P7010 in plate form produced by rolling; thickness range 6 mm < a ≤ 20 mm.
• Delivery condition: Temper T651 (solution heat‑treated, water‑quenched, controlled stretch and artificially aged). The standard gives heat‑treatment parameters, for example:
  • Solution treatment: 470–485 °C followed by water quench (to ≤ 40 °C)
  • Controlled stretch: +1.5 % to +3 %
  • Artificial aging: 150–160 °C for 6–12 hours
• Mechanical properties (minimum values by thickness and orientation):
  • Proof stress (p0.2) and tensile strength (Rm) minima are specified for longitudinal (L) and long transverse (LT) directions and differ for 6<a≤12.5 mm and 12.5<a≤20 mm ranges.
  • Elongation: A ≥ 7 % (50 mm gauge) is required.
• Chemical composition and metallurgy: Limits for principal alloying elements (Cu, Mg, Zn, Zr, Si, Fe, Ti, etc.) are specified in the standard to ensure consistent chemistry and properties.
• Inspection and testing: References EN 4400‑1 for plate technical specification, sampling, defect acceptance, dimensional and marking inspections. Typical electrical conductivity value is ~18.0 MS/m.
• Delivery condition code: Specified as U in the document.

Applications and who uses it

• Aerospace structural components: Primary and secondary airframe parts where a high‑strength, corrosion‑resistant aluminium plate is required (e.g., fuselage skins, stringers, fittings).
• Manufacturers and suppliers: Plate mills and aerospace material suppliers use the standard for production, acceptance testing and certification.
• Design and quality engineers: Structural engineers, procurement teams and QA/QC personnel apply EN 4214:2005 to select materials, verify compliance and prepare purchase specifications.
• Repair and maintenance: MRO organizations referencing correct alloy temper and mechanical properties for repairs and replacements.

Related standards

• EN 4400-1 - Aerospace series - Aluminium wrought products - Technical specification (Plate)
• EN 4258 - Organization of aerospace metallic material standards
• EN 4500-2 - Rules for drafting/presentation for aluminium and magnesium alloys

Keywords: EN 4214:2005, AL‑P7010‑T651, aluminium alloy plate, aerospace aluminium plate, T651 temper, rolled plate 6–20 mm, aircraft structural materials, aerospace standards.

Standards Content (Sample)

SLOVENSKI STANDARD
01-november-2005
Aerospace series - Aluminium alloy AL-P7010-T651 - Plate - 6 mm Aerospace series - Aluminium alloy AL-P7010-T651 - Plate - 6 mm Luft- und Raumfahrt - Aluminiumlegierung AL-P7010-T651 - Platten - 6 mm Série aérospatiale - Alliage d'aluminium AL-P7010-T651 - Tôles épaisses - 6 mm mm
Ta slovenski standard je istoveten z: EN 4214:2005
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD EN 4214
NORME EUROPÉENNE
EUROPÄISCHE NORM
June 2005
ICS 49.025.20
English version
Aerospace series - Aluminium alloy AL-P7010-T651 - Plate - 6
mm Série aérospatiale - Alliage d'aluminium AL-P7010-T651 - Luft- und Raumfahrt - Aluminiumlegierung AL-P7010-T651 -
Tôles épaisses - 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.

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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 4214:2005: E
worldwide for CEN national Members.

Foreword
This document (EN 4214:2005) 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, Gree
...