SIST EN 3342:2006

Aerospace series - Aluminium alloy AL-P6061 - T4 or T42 - Drawn or extruded bar and section - a or D <or= 150 mm

This standard specifies the requirements relating to:
Aluminium alloy AL-P6061-
T4 or T42
Drawn or extruded bar and section
a or D < 150 mm
for aerospace application.
The order shall state whether the extruded or drawn condition is required.

Luft- und Raumfahrt - Aluminiumlegierung AL-P6061-T4 oder T42 - Gezogene oder stranggepresste Stangen und Profile - a oder D <or= 150 mm

Diese Norm legt die Anforderungen an
Aluminiumlegierung AL-P6061
T4 oder T42
gezogene oder stranggepresste Stangen und Profile
a oder D £ 150 mm
für Anwendungen in der Luft- und Raumfahrt fest.
Die Bestellung muss angeben ob die stranggepresste oder gezogene Ausführung gefordert wird.

Série aérospatiale - Alliage d'aluminium AL-P6061 - T4 ou T42 - Barres et profilés étirés ou filés - a ou D <or= 150 mm

Aeronavtika – Aluminijeva zlitina AL-P6061 - T4 ali T42 – Vlečene ali iztiskane palice in profili - a ali D ? 150 mm

General Information

• Status: Published
• Publication Date: 30-Jun-2006
• ICS: 49.025.20 - Aluminium
• Technical Committee: I13 - Imaginarni 13
• Current Stage: 6060 - National Implementation/Publication (Adopted Project)
• Start Date: 01-Jul-2006
• Due Date: 01-Jul-2006
• Completion Date: 01-Jul-2006
• Ref Project: EN 3342:2005 - Aerospace series - Aluminium alloy AL-P6061 - T4 or T42 - Drawn or extruded bar and section - a or D <or= 150 mm

Overview

EN 3342:2005 is a CEN (Aerospace series) standard that defines requirements for aluminium alloy AL‑P6061 in the T4 or T42 tempers, supplied as drawn or extruded bar and section with cross‑sectional dimension a or diameter D ≤ 150 mm. It is intended specifically for aerospace applications and sets delivery conditions, mechanical property minima and inspection/qualification references.

Key topics and requirements

• Material designation: Aluminium alloy AL‑P6061, temper T4 or T42.
• Form and size: Drawn or extruded bar and section, maximum a or D ≤ 150 mm. Orders must state whether product is extruded or drawn.
• Heat treatment / delivery conditions: Solution heat treatment and quenching followed by ageing are specified in the standard (e.g., solution 520–540 °C, quench to ≤ 40 °C and subsequent ageing/natural ageing as required for T4/T42) - refer to the full text for exact treatment wording and delivery codes (F, O, T4, T42).
• Mechanical property minima (representative values in the standard):
  • Proof stress R_p0.2 ≥ 110 MPa
  • Tensile strength R_m ≥ 210 MPa
  • Elongation A ≥ 14% (A or A50 mm)
• Inspection and testing: Dimensions, marking and inspection rules refer to EN 4400‑3 (Bar and section technical specification). Test pieces and sampling are also defined by EN 4400‑3.
• Quality / qualification: Product qualification program to be agreed between manufacturer and purchaser; batch uniformity, internal/external defect criteria follow EN 4400‑3.

Applications and who uses it

• Aerospace OEMs and suppliers specifying raw wrought aluminium bar and profile material for structural components, fittings and machined parts.
• Procurement and quality managers who need standardized purchase specifications and acceptance criteria for AL‑P6061 bars and sections.
• Design and materials engineers selecting alloy temper and form for machinability, strength and corrosion performance in aircraft applications.
• Material testing and inspection laboratories carrying out acceptance testing per EN 4400‑3 references.

Related standards

• EN 4400‑3 - Aerospace series: Aluminium wrought products - Part 3: Bar and section (technical specification, testing and inspection).
• EN 4258 - Organization of aerospace metallic material standards.
• EN 4500‑2 - Rules for drafting/presentation of aluminium alloy material standards.

Keywords: EN 3342:2005, aluminium AL‑P6061, T4, T42, aerospace materials, drawn bar, extruded section, EN 4400‑3, aerospace standard.

Standards Content (Sample)

SLOVENSKI STANDARD
01-julij-2006
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Aerospace series - Aluminium alloy AL-P6061 - T4 or T42 - Drawn or extruded bar and
section - a or D Luft- und Raumfahrt - Aluminiumlegierung AL-P6061-T4 oder T42 - Gezogene oder
stranggepresste Stangen und Profile - a oder D Série aérospatiale - Alliage d'aluminium AL-P6061 - T4 ou T42 - Barres et profilés étirés
ou filés - a ou D Ta slovenski standard je istoveten z: EN 3342:2005
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD EN 3342
NORME EUROPÉENNE
EUROPÄISCHE NORM
October 2005
ICS 49.025.20
English Version
Aerospace series - Aluminium alloy AL-P6061 - T4 or T42 -
Drawn or extruded bar and section - a or D ≤ 150 mm
Série aérospatiale - Alliage d'aluminium AL-P6061 - T4 ou Luft- und Raumfahrt - Aluminiumlegierung AL-P6061 - T4
oder T42 - Gezogene oder Stranggepreßte Stangen und
T42 - Barres et profilés étirés ou filés - a ou D ≤ 150 mm
Profile - a oder D ≤ 150 mm
This European Standard was approved by CEN on 19 September 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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EUROPÄISCHES KOMITEE FÜR NORMUNG

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© 2005 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 3342:2005: E
worldwide for CEN national Members.

Contents Page
Foreword .3
Introduction.4
1 Scope.4
2 Normative references.4

Foreword
This European Standard (EN 3342:2005) 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 April 2006, and conflicting national standards shall be withdrawn at the
latest by April 2006.
Attention is drawn to the possibility tha
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