Aerospace series - Aluminium alloy AL-P8090-T89 - Die forgings - a <125 mm

This standard specifies the requirements relating to:
Aluminium alloy AL-P8090-
T89
Die forgings
a < or = 125 mm
for aerospace application.

Luft- und Raumfahrt - Aluminiumlegierung AL-P8090-T89 - Gesenkschmiedestücke - a <125 mm

Diese Norm legt die Anforderungen an
Aluminiumlegierung AL-P8090-
T89
Gesenkschmiedestück
a < or = 125 mm
für Anwendungen in der Luft- und Raumfahrt fest.

Série aérospatiale - Alliage d'aluminium AL-P8090-T89 - Pieces matricées - a <125 mm

Aerospace series - Aluminium alloy AL-P8090-T89 - Die forgings - a <125 mm

General Information

Status
Published
Publication Date
31-Oct-2005
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
01-Nov-2005
Due Date
01-Nov-2005
Completion Date
01-Nov-2005

Overview

SIST EN 4286:2005 is a European Standard developed by CEN, specifying the technical and quality requirements for die forgings made from Aluminium alloy AL-P8090-T89 with a thickness (a) of 125 mm or less. This standard is part of the aerospace series of metallic material standards designed to ensure consistent quality and performance of aerospace materials. It was prepared by the European Association of Aerospace Manufacturers (AECMA-STAN) and has been adopted by multiple national standard bodies across Europe.

The scope of SIST EN 4286:2005 covers the chemical composition, mechanical properties, heat treatment conditions, and testing protocols for AL-P8090-T89 aluminium alloy used in critical aerospace applications. It aligns with related standards such as EN 2082-3 and EN 4258, ensuring compatibility and comprehensive coverage for aerospace manufacturing needs.

Key Topics

  • Material Specification: Defines Aluminium alloy AL-P8090-T89 die forgings with hardness and composition limits specifically suited for aerospace components.
  • Maximum Dimension: Applies to die forgings with thickness up to 125 mm, focusing on optimizing mechanical properties within this size limit.
  • Chemical Composition: Specifies limits for elements such as Silicon (Si), Iron (Fe), Copper (Cu), Magnesium (Mg), Zinc (Zn), Lithium (Li), and others to maintain alloy consistency.
  • Heat Treatment: Details the T89 temper-solution heat treatment within 525 °C to 535 °C, water quenching, and artificial aging between 170 °C to 180 °C for 20 to 30 hours, with controlled cold deformation.
  • Mechanical Properties: Includes minimum proof stress (R p0.2) of 330 MPa, tensile strength (R m) of 430 MPa, elongation percentages, and fracture toughness values critical for aerospace safety and reliability.
  • Testing Methods: Requires fracture toughness, internal/external defects inspections, density measurement by displacement, and other mechanical tests as per referenced standards (EN 2082-3, EN 6018).
  • Quality Control: Mandates strict dimensional inspection, batch uniformity checks, and marking requirements to ensure traceability and conformance.
  • Product Qualification: Qualification processes are agreed upon between manufacturers and purchasers, supporting custom aerospace manufacturing demands.

Applications

SIST EN 4286:2005 aluminium alloy AL-P8090-T89 die forgings are primarily intended for aerospace applications, where lightweight, high-strength materials are critical. Specific use cases include:

  • Aircraft Structural Components: Critical load-bearing parts benefiting from high tensile strength and toughness.
  • Engine Components: Parts requiring excellent mechanical performance under thermal and dynamic stresses.
  • Aerospace Forgings: Precision die forging products with controlled composition and mechanical properties for airframes and systems.
  • Lightweight Assemblies: Aerospace designs emphasizing weight reduction without compromising durability or safety.

Manufacturers and suppliers use EN 4286 to ensure compliance with industry-recognized aerospace materials specifications, promoting reliability and uniformity in aerospace material supply chains.

Related Standards

SIST EN 4286:2005 complements and references several key aerospace standards to provide a complete framework for aluminium alloy forgings:

  • EN 2082-3: Aerospace series - Aluminium alloy forging stock and forgings - Technical specification – provides detailed technical requirements and testing methods.
  • EN 4258: General organization of metallurgical standardization for aerospace materials - defines how related standards interact and are used.
  • EN 4291: Defines specifications for AL-P8090 forging stock, ensuring raw material consistency.
  • EN 4500-2: Drafting and presentation rules specific to aluminium and magnesium alloy standards ensuring clarity and uniformity.
  • EN 6018: Test method for determining density by displacement for metallic aerospace materials.

These interconnected standards deliver a robust system for controlling the quality, safety, and performance of aerospace aluminium forgings in compliance with international aerospace manufacturing requirements.


Keywords: EN 4286, aluminium alloy AL-P8090-T89, aerospace die forgings, aluminium aerospace standard, aerospace aluminium alloy, die forging specifications, aerospace materials standard, aluminium forging aerospace, aerospace metal standards, heat treatment aluminium aerospace

Frequently Asked Questions

SIST EN 4286:2005 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Aluminium alloy AL-P8090-T89 - Die forgings - a <125 mm". This standard covers: This standard specifies the requirements relating to: Aluminium alloy AL-P8090- T89 Die forgings a < or = 125 mm for aerospace application.

This standard specifies the requirements relating to: Aluminium alloy AL-P8090- T89 Die forgings a < or = 125 mm for aerospace application.

SIST EN 4286:2005 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.

SIST EN 4286:2005 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-P8090-T89 - Die forgings - a <125 mm
Aerospace series - Aluminium alloy AL-P8090-T89 - Die forgings - a <125 mm
Luft- und Raumfahrt - Aluminiumlegierung AL-P8090-T89 - Gesenkschmiedestücke - a
<125 mm
Série aérospatiale - Alliage d'aluminium AL-P8090-T89 - Pieces matricées - a <125 mm
Ta slovenski standard je istoveten z: EN 4286:2005
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD EN 4286
NORME EUROPÉENNE
EUROPÄISCHE NORM
June 2005
ICS 49.025.20
English version
Aerospace series - Aluminium alloy AL-P8090-T89 - Die forgings
- a ≤125 mm
Série aérospatiale - Alliage d'aluminium AL-P8090-T89 - Luft- und Raumfahrt - Aluminiumlegierung AL-P8090-T89 -
Pièces matricées - a ≤125 mm Gesenkschmiedestücke - a ≤125 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.

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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 4286:2005: E
worldwide for CEN national Members.

Foreword
This document (EN 4286:2005) 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,
Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland
and the United Kingdom.
SIST
...

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