EN 4100:2005

Aerospace series - Aluminium alloy AL-P2219-T6 or T62 - Sheet and strip - 0,5 mm <a <6 mm

This standard specifies the requirements relating to:
Aluminium alloy AL-P2219-
T6 or T62
Sheet and strip
0,5 mm < or = a < or = 6 mm
for aerospace application.

Luft- und Raumfahrt - Aluminiumlegierung AL-P2219-T6 oder T62 - Bleche und Bänder - 0,5 mm <a <6 mm

Diese Norm legt die Anforderungen an
Aluminiumlegierung AL-P2219-
T6 oder T62
Bleche und Bänder
0,5 mm £ a £ 6 mm
für Anwendungen in der Luft- und Raumfahrt fest.

Série aérospatiale - Alliage d'aluminium AL-P2219-T6 ou T62 - Tôles et bandes - 0,5 mm <a <6 mm

Aerospace series - Aluminium alloy AL-P2219-T6 or T62 - Sheet and strip - 0,5 mm <a <6 mm

General Information

• Status: Published
• Publication Date: 21-Jun-2005
• Withdrawal Date: 30-Dec-2005
• ICS: 49.025.20 - Aluminium
• 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
• Ref Project: SIST EN 4100:2005 - Aerospace series - Aluminium alloy AL-P2219-T6 or T62 - Sheet and strip - 0,5 mm <a <6 mm

Relations

• Refers: 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

Overview

EN 4100:2005 is a CEN/AECMA-STAN European standard specifying requirements for aerospace-grade aluminium alloy AL‑P2219 in sheet and strip form with thicknesses 0.5 mm ≤ a ≤ 6 mm. It covers chemical composition, production form, heat treatments (delivery and use conditions), mechanical property requirements and inspection/qualification requirements for aerospace applications.

Key topics and technical requirements

• Material designation and form: Aluminium alloy AL‑P2219 supplied as rolled sheet and strip, thickness range 0.5–6 mm.
• Chemical composition: The standard defines limits for alloying and impurity elements; for example, copper content is specified in the range shown in the standard (≈5.8–6.8% as given in the material table). Silicon, iron and other elements are limited to low levels.
• Heat treatment / delivery conditions: Delivery and use conditions include O, H111, T6 and T62. The document specifies solution heat treatment (≈530–540 °C) with water quench (≤40 °C) and artificial aging (≈185–196 °C for 30–40 h) for T6/T62.
• Mechanical properties and tests: Mechanical property limits (proof stress, tensile strength, elongation) are defined by thickness range and heat condition. Example values in the standard include minimum tensile strengths ≈375 MPa for T6/T62 conditions and proof stress minima ≈250 MPa. Direction of test pieces, ambient test temperature and sampling are specified per EN 4400‑2.
• Inspection and batch control: Requirements reference EN 4400‑2 for dimensional, marking and non‑conformity inspections. Hardness and batch uniformity tolerances (per product and per batch) are included. Typical electrical conductivity values are also given.

Applications and users

• Primary uses: Structural aerospace components where AL‑P2219’s high-strength, heat‑treatable copper‑bearing alloy properties are required (airframe fittings, machined parts, and other structural elements).
• Who uses this standard: Aerospace material engineers, specification writers, OEMs and Tier‑1/2 suppliers, procurement teams, quality/inspection personnel, and testing laboratories preparing or verifying AL‑P2219 sheet and strip for aircraft applications.

Related standards

• EN 4400‑2 (Aluminium and aluminium alloy wrought products - Technical specification - Part 2: Sheet and strip) - referenced for sampling, testing and technical specification format.
• EN 4258 (organization of aerospace metallic material standards) and EN 4500‑2 (rules for drafting aluminium material standards) - provide series context and drafting rules.
• AECMA‑STAN (originating aerospace standardization body) and CEN adoption noted.

Keywords: EN 4100:2005, AL‑P2219, P2219‑T6, P2219‑T62, aerospace aluminium sheet, 0.5–6 mm, CEN, EN 4400‑2, heat treatment.

Standards Content (Sample)

SLOVENSKI STANDARD
01-november-2005
Aerospace series - Aluminium alloy AL-P2219-T6 or T62 - Sheet and strip - 0,5 mm
Aerospace series - Aluminium alloy AL-P2219-T6 or T62 - Sheet and strip - 0,5 mm <6 mm
Luft- und Raumfahrt - Aluminiumlegierung AL-P2219-T6 oder T62 - Bleche und Bänder -
0,5 mm Série aérospatiale - Alliage d'aluminium AL-P2219-T6 ou T62 - Tôles et bandes - 0,5 mm
Ta slovenski standard je istoveten z: EN 4100:2005
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD EN 4100
NORME EUROPÉENNE
EUROPÄISCHE NORM
June 2005
ICS 49.025.20
English version
Aerospace series - Aluminium alloy AL-P2219-T6 or T62 - Sheet
and strip - 0,5 mm ≤a ≤6 mm
Série aérospatiale - Alliage d'aluminium AL-P2219-T6 ou Luft- und Raumfahrt - Aluminiumlegierung AL-P2219-T6
T62 - Tôles et bandes - 0,5 mm ≤a ≤6 mm oder T62 - Bleche und Bänder - 0,5 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.
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© 2005 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4100:2005: E
worldwide for CEN national Members.

Foreword
This document (EN 4100:2005) 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, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania,
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