SIST EN 2395:2005

Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - Sheet and strip - 0,4 mm <a <6 mm

This standard specifies the requirements relating to:
Aluminium alloy AL-P2014A
T4 or T42
Sheet and strip
0,4 mm < or = a < or = 6 mm
for aerospace application.

Luft- und Raumfahrt - Aluminiumlegierung AL-P2014A-T4 oder T42 - Bleche und Bänder - 0,4 mm <a <6 mm

Diese Norm legt die Anforderungen an
Aluminiumlegierung AL-P2014A
T4 oder T42
Bleche und Bänder
0,4 mm >= a >= 6 mm
für Anwendungen in der Luft- und Raumfahrt fest.

Série aérospatiale - Alliage d'aluminium AL-P2014A-T4 ou T42 - Tôles et bandes - 0,4 mm <a <6 mm

Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - 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 2395:2005 - Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - Sheet and strip - 0,4 mm <a <6 mm

Relations

• Replaces: SIST EN 2395:2001 - Aerospace series - Aluminium alloy AL-P2014A - T4 or T42 - Sheet and strip 0,4 mm <= a <= 6 mm
• Effective Date: 22-Dec-2008
• Refers: SIST EN 4258:2024 - Aerospace series - Metallic materials - General organization of standardization - Link between types of European Standards and their use
• Effective Date: 28-Jan-2026
• Referred By: SIST EN 2899:2018 - Aerospace series - Vulcanized rubbers - Test on the susceptibility to corrosion in a damp atmosphere of metals in contact with vulcanized rubbers
• Effective Date: 28-Jan-2026

Overview

SIST EN 2395:2005 is a European Standard developed by the European Committee for Standardization (CEN) that specifies requirements for aluminium alloy AL-P2014A in the T4 or T42 temper. Specifically, it covers sheet and strip with thicknesses ranging from 0.4 mm up to 6 mm used in aerospace applications. This document forms a part of the wider series of EN standards focused on materials and metallic products for the aerospace industry.

The standard ensures that manufacturers and users have a clear framework for ordering, producing, verifying, and utilizing aluminium alloy AL-P2014A-T4 or T42 in aerospace-grade sheets and strips. Adoption of SIST EN 2395:2005 helps ensure product consistency, safety, and interoperability in aerospace construction and maintenance.

Key Topics

SIST EN 2395:2005 addresses several essential areas:

• Material Specifications: Defines chemical composition limits for AL-P2014A alloy, focusing on quality and verifiable characteristics required for aerospace use.
• Product Forms: Lists applicable product types, specifically sheet and strip, falling within the range of 0.4 mm to 6 mm thickness.
• Delivery Conditions: Covers temper designations T4 and T42, including requirements for heat treatment and mechanical properties.
• Dimensional Requirements: Provides dimensional tolerances for supplied material, supporting precise manufacturing practices.
• Inspection and Testing: Refers to procedures and requirements for verification, such as marking inspection, dimensional checks, intergranular corrosion resistance, and batch uniformity, often cross-referencing EN 4400-2.
• Documentation: Outlines the need for documentation in compliance with aerospace quality management protocols, including traceability and compliance records.
• Qualification and Acceptance: Product qualification procedures to be agreed upon between manufacturer and purchaser, ensuring mutual understanding of product conformity.

Applications

The requirements established by SIST EN 2395:2005 are tailored for the aerospace sector, where aluminium alloys are valued for their high strength-to-weight ratio, corrosion resistance, and machinability. Common applications include:

• Aircraft structural components: Fuselage panels, internal frames, bulkheads, and floor panels.
• Aerospace engineering: Parts subject to demanding strength and durability standards, such as brackets, supports, and other load-bearing assemblies.
• Maintenance and repair: Replacement sheet and strip materials for certified aerospace repair shops and original equipment manufacturers (OEMs).
• Precision components: Use in fabricating intricate assemblies requiring consistent mechanical properties and surface quality.

Conformance to SIST EN 2395:2005 ensures materials meet strict mechanical and chemical standards, minimizing risks of failure in critical flight components. This boosts reliability and compliance with international aerospace regulations.

Related Standards

Organizations using SIST EN 2395:2005 should be aware of related and supporting standards, which provide additional details and requirements for material management within the aerospace industry:

• EN 4258: Describes the overall organization of metallic material standards in aerospace applications.
• EN 4400-2: Specifies technical requirements for aluminium and aluminium alloy wrought products, including sheets and strips.
• EN 4500-2: Sets out rules for drafting and presenting material standards, particularly for aluminium, aluminium alloys, and magnesium alloys.
• ICS 49.025.20: International Classification for Standards covering aluminium materials in aerospace.

Adopting SIST EN 2395:2005, in alignment with the above standards, supports quality assurance, interoperability, and seamless integration into aerospace manufacturing and maintenance workflows. Using standardized aluminium alloys not only simplifies supplier evaluation and procurement but also enhances safety and long-term performance in demanding aerospace environments.

Standards Content (Sample)

SLOVENSKI STANDARD
01-november-2005
1DGRPHãþD
SIST EN 2395:2001
Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - Sheet and strip - 0,4
mm Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - Sheet and strip - 0,4 mm <6 mm
Luft- und Raumfahrt - Aluminiumlegierung AL-P2014A-T4 oder T42 - Bleche und Bänder
- 0,4 mm Série aérospatiale - Alliage d'aluminium AL-P2014A-T4 ou T42 - Tôles et bandes - 0,4
mm Ta slovenski standard je istoveten z: EN 2395:2005
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD EN 2395
NORME EUROPÉENNE
EUROPÄISCHE NORM
June 2005
ICS 49.025.20 Supersedes EN 2395:1994
English version
Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 -
Sheet and strip - 0,4 mm ≤a ≤6 mm
Série aérospatiale - Alliage d'aluminium AL-P2014A-T4 ou Luft- und Raumfahrt - Aluminiumlegierung AL-2014A-
T42 - Tôles et bandes - 0,4 mm ≤a ≤6 mm T4 oder T42 - 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 2395:2005: E
worldwide for CEN national Members.

Foreword
This document (EN 2395:2005) 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 2395:1994.
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, Netherl
...