SIST EN 2089:2005

Aerospace series - Aluminium alloy AL-P2014A-T6 or T62 - Sheet and strip - 0,4 mm <a <6 mm

This standard specifies the requirements relating to:
Aluminium alloy AL-P2014A
T6 or T62
Sheet and strip
0,4 mm < or = a < or = 6 mm
for aerospace application.

Luft- und Raumfahrt - Aluminiumlegierung AL-P2014A-T6 oder T62 - Bleche und Bänder - 0,4 mm <a <6 mm

Diese Norm legt die Anforderungen an
Aluminiumlegierung AL P2014A
T6 oder T62
Bleche und Bänder
0,4 mm < oder = a < oder = 6 mm
für Anwendungen in der Luft- und Raumfahrt fest.

Série aérospatiale - Alliage d'aluminium AL-P2014A-T6 ou T62 - Tôles et bandes - 0,4 mm <a <6 mm

Aerospace series - Aluminium alloy AL-P2014A-T6 or T62 - 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 2089:2005 - Aerospace series - Aluminium alloy AL-P2014A-T6 or T62 - Sheet and strip - 0,4 mm <a <6 mm

Relations

• Replaces: SIST EN 2089:2001 - Aerospace series - Aluminium alloy AL-P2014A - T6 or T62 - Sheet and strip - 0,4 mm <= a <= 6 mm
• Effective Date: 22-Dec-2008

Overview

SIST EN 2089:2005 is a European standard developed by CEN, specifying technical and quality requirements for aerospace-grade aluminium alloy AL-P2014A in T6 or T62 temper conditions. This standard applies to sheet and strip products with thicknesses ranging from 0.4 mm to 6 mm. The standard is part of the wider aerospace series for metallic materials, intended to ensure consistency, reliability, and suitability of aluminium alloys used in critical aerospace components.

This standard serves manufacturers and purchasers by defining precise chemical compositions, mechanical properties, heat treatment methods, and dimensional tolerances. It supersedes the earlier EN 2089:1994 standard and aligns with other aerospace standards to facilitate global harmonization in aluminium alloy specifications.

Key Topics

• Material Specification

  • Aluminium alloy AL-P2014A composition limits for elements such as Si, Fe, Cu, Mn, Mg, Cr, Ni, Zn, Ti, Zr
  • Alloy designations: T6 and T62 heat treatment tempers tailored for aerospace application
  • Sheet and strip forms with thicknesses from 0.4 mm up to 6 mm

• Heat Treatment and Delivery Conditions

  • Defined treatment cycles including solution heat treatment, quenching, and artificial aging
  • Delivery conditions coded as F, O, T4, T6, with T62 representing an alternative aging treatment
  • Effects on mechanical properties like proof stress and tensile strength

• Mechanical Properties and Testing

  • Minimum mechanical characteristics including proof stress ≥ 390 MPa, tensile strength ≥ 440 MPa, and elongation ≥ 7%
  • Tests specified according to EN 4400-2 to verify batch uniformity, hardness, and dimensional compliance
  • Emphasis on quality inspections such as marking and dimensional checks during manufacturing

• Dimensional Tolerances and Cladding Thickness

  • Thickness variations controlled between 0.4 mm and 6 mm
  • Cladding specifications for corrosion resistance on aluminium alloy surface layers

• Standard Coordination and Compliance

  • Harmonized with EN 4400-2, EN 4258, and EN 4500-2 standards for metallic aerospace materials
  • Supports production uniformity across European aerospace industry
  • Guidelines for product qualification and agreement between manufacturer and purchaser

Applications

SIST EN 2089:2005 governs the specifications for aluminium alloy sheet and strip products widely utilized in aerospace manufacturing. Its applications include:

• Aircraft structural components requiring high strength-to-weight ratios
• Aerospace manufacturing processes demanding stringent material consistency and certification
• Production of high-performance fuselage skins, wing panels, and internal reinforcements
• Replacement and repair materials in aerospace maintenance and overhaul
• Components requiring excellent fatigue and corrosion resistance properties

The standard ensures materials meet performance requirements under demanding aerospace conditions, such as variable temperatures and mechanical stresses, thus enhancing the safety and longevity of aerospace components.

Related Standards

• EN 4400-2: Technical specification for aluminium and aluminium alloy wrought sheet and strip products in aerospace applications, providing test protocols referenced by EN 2089.
• EN 4258: Defines the general organization and structure of aerospace metallic material standardization, linking various related EN standards.
• EN 4500-2: Specifies rules for drafting and presenting aerospace material standards, particularly for aluminium and magnesium alloys, used in the preparation of EN 2089.
• AECMA-STAN Standards: Former aerospace industry standards organized by the European Association of Aerospace Manufacturers, ensuring compatibility and harmonization across aerospace materials.

By following SIST EN 2089:2005 and its related standards, manufacturers and aerospace engineers can ensure compliance with strict European aerospace material regulations, guaranteeing material reliability and performance in critical flight and structural applications.

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Keywords: EN 2089, aluminium alloy AL-P2014A, aerospace aluminium sheet, aerospace aluminium strip, T6 temper, T62 temper, aerospace material standards, aluminium sheet thickness 0.4-6 mm, aerospace manufacturing standards, CEN aerospace standards, European aerospace aluminium standards, aerospace structural materials, aerospace alloy mechanical properties.

Standards Content (Sample)

SLOVENSKI STANDARD
01-november-2005
1DGRPHãþD
SIST EN 2089:2001
Aerospace series - Aluminium alloy AL-P2014A-T6 or T62 - Sheet and strip - 0,4
mm Aerospace series - Aluminium alloy AL-P2014A-T6 or T62 - Sheet and strip - 0,4 mm <6 mm
Luft- und Raumfahrt - Aluminiumlegierung AL-P2014A-T6 oder T62 - Bleche und Bänder
- 0,4 mm Série aérospatiale - Alliage d'aluminium AL-P2014A-T6 ou T62 - Tôles et bandes - 0,4
mm Ta slovenski standard je istoveten z: EN 2089:2005
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD EN 2089
NORME EUROPÉENNE
EUROPÄISCHE NORM
June 2005
ICS 49.025.20
English version
Aerospace series - Aluminium alloy AL-P2014A-T6 or T62 -
Sheet and strip - 0,4 mm ≤a ≤6 mm
Série aérospatiale - Alliage d'aluminium AL-P2014A-T6 ou Luft- und Raumfahrt - Aluminiumlegierung AL-P2014A-T6
T62 - Tôles et bandes - 0,4 mm ≤a ≤6 mm oder T62 - 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 2089:2005: E
worldwide for CEN national Members.

Foreword
This document (EN 2089:2005) 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 2089:1994.
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, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland
and the United Kingdom.
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