General Information

Abstract

This standard specifies the requirements relating to:
Aluminium alloy AL-P2024-
T42
Plate
6 mm < a < or = 140 mm
for aerospace application.

Status
Published
Publication Date
21-Jun-2005
Withdrawal Date
30-Dec-2005
Technical Committee
ASD-STAN - Aerospace
Drafting Committee
ASD-STAN/D 4 - Metallic
Current Stage
6060 - Definitive text made available (DAV) - Publishing
Start Date
22-Jun-2005
Completion Date
22-Jun-2005

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Overview

EN 4247:2005 defines the requirements for aluminum alloy AL-P2024-T42 plates with thicknesses between 6 mm and 140 mm, specifically for aerospace applications. Issued by the European Committee for Standardization (CEN), this standard ensures high quality and consistency in the production and use of these aluminum plates. It applies to rolled aluminum plates manufactured and delivered in the T42 temper, widely used in the aerospace industry for their strength and durability.

Key Topics

  • Material Specification: This standard covers aluminum alloy AL-P2024-T42, outlining its chemical composition, mechanical properties, and delivery conditions.
  • Plate Dimensions: Applicable to plates with thickness greater than 6 mm and up to 140 mm.
  • Production Methods: Specifies that the product form is a rolled plate and prescribes relevant production and heat treatment methods.
  • Quality Requirements: Addresses sample and test piece selection, inspection protocols, marking, and product qualification.
  • Delivery Conditions: Plates are supplied in the T42 condition, following a specific heat treatment process combining solution heat treatment, quenching, and natural aging.
  • Testing & Inspection: Provides references to testing methods and inspection requirements via cross-references to EN 4400-1, ensuring compliance with aerospace standards.

Applications

EN 4247:2005 is essential for manufacturers, aerospace engineers, quality managers, and procurement specialists involved in the aerospace sector. The main applications include:

  • Aerospace Structures: Used in the fabrication of load-bearing aircraft components such as fuselage panels, wing sections, and frames due to their favorable strength-to-weight ratio.
  • High-Integrity Components: Suitable for critical parts requiring reliable mechanical properties and proven material pedigree.
  • Replacement & Maintenance: Facilitates consistent sourcing of spare parts and maintenance materials by providing a clear standard for material selection.
  • Supplier Compliance: Enables suppliers to demonstrate compliance with European aerospace material requirements, supporting certification and approval processes.
  • Design and Manufacturing: Helps engineers design components to meet both performance and regulatory requirements.

Related Standards

For comprehensive application and compliance, users should review these related European standards:

  • EN 4258: Provides general organization and guidelines for standardization of metallic materials for aerospace purposes.
  • EN 4400-1: Specifies technical requirements for aluminum and aluminum alloy wrought products, including plates, used in the aerospace industry.
  • EN 4500-2: Outlines specific rules for drafting and presentation of standards for aluminum, aluminum alloys, and magnesium alloys.
  • Other EN Aerospace Standards: Refer to additional EN aerospace series standards for rivets, fasteners, and other related materials to ensure complete system compatibility.

Practical Value

Adhering to EN 4247:2005 ensures:

  • Product Consistency: Uniform mechanical and chemical properties for manufacturing and repair.
  • Quality Assurance: Enhanced traceability and inspection processes, minimizing risk in critical aerospace applications.
  • Regulatory Compliance: Alignment with European and international aerospace material requirements.
  • Supply Chain Confidence: Clear communication between manufacturers, suppliers, and customers on material properties and compliance.

In summary, EN 4247:2005 is a foundational standard for aluminum alloy plates in aerospace, supporting safety, reliability, and efficiency in the industry. For maximum benefit and seamless integration, always consult the full standard alongside referenced documents.

Relations

Effective Date
28-Jan-2026
Effective Date
28-Jan-2026

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Frequently Asked Questions

EN 4247:2005 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Aluminium alloy AL-P2024-T42 - Plate - 6 mm <a <140 mm". This standard covers: This standard specifies the requirements relating to: Aluminium alloy AL-P2024- T42 Plate 6 mm < a < or = 140 mm for aerospace application.

This standard specifies the requirements relating to: Aluminium alloy AL-P2024- T42 Plate 6 mm < a < or = 140 mm for aerospace application.

EN 4247:2005 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 4247:2005 has the following relationships with other standards: It is inter standard links to EN 4258:2024, EN 4465:2007. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

EN 4247:2005 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-november-2005
Aerospace series - Aluminium alloy AL-P2024-T42 - Plate - 6 mm Aerospace series - Aluminium alloy AL-P2024-T42 - Plate - 6 mm Luft- und Raumfahrt - Aluminiumlegierung AL-P2024-T42 - Platten - 6 mm Série aérospatiale - Alliage d'aluminium AL-P2024-T42 - Tôles épaisses - 6 mm mm
Ta slovenski standard je istoveten z: EN 4247:2005
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD EN 4247
NORME EUROPÉENNE
EUROPÄISCHE NORM
June 2005
ICS 49.025.20
English version
Aerospace series - Aluminium alloy AL-P2024-T42 - Plate - 6
mm
Série aérospatiale - Alliage d'aluminium AL-P2024-T42 - Luft- und Raumfahrt - Aluminiumlegierung AL-P2024-T42 -
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.

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 4247:2005: E
worldwide for CEN national Members.

Foreword
This document (EN 4247:2005) 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, Czec
...