Aerospace series - Aluminium alloy AL-P2014A T4511 - Extruded bars and sections a or D < or = 200 mm

This standard specifies the requirements relating to extruded bars and sections in aluminium alloy AL-P2014A, for use in the T4511 condition, a or D inferior or equal to 200 mm, for aerospace applications.
This standard may also be used to supply material in the T4510 condition, if the purchaser specifies this condition on the order. In this case, the designation of line 97 shall not be used.

Luft- und Raumfahrt - Aluminiumlegierung AL-P2014A T4511 - Stranggepreßte Stangen und Profile a oder D < oder = 200 mm

Série aérospatiale - Alliage d'aluminium AL-P2014A T4511 - Barres et profilés filés a ou D < ou = 200 mm

Aerospace series - Aluminium alloy AL-P2014A T4511 - Extruded bars and sections a or D < or = 200 mm

General Information

Status
Published
Publication Date
29-Sep-1992
Withdrawal Date
30-Mar-1993
Technical Committee
ASD-STAN - Aerospace
Drafting Committee
ASD-STAN/D 4 - Metallic
Current Stage
6060 - Definitive text made available (DAV) - Publishing
Start Date
30-Sep-1992
Completion Date
30-Sep-1992

Relations

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

Overview

EN 2100:1992 is a widely recognized standard from CEN covering requirements for extruded bars and sections made from aluminium alloy AL-P2014A in the T4511 temper, with dimensions where the width (a) or diameter (D) is less than or equal to 200 mm. This standard is specifically developed for aerospace applications, ensuring material quality and traceability in critical environments. Adoption of EN 2100:1992 helps manufacturers and suppliers maintain consistent production, meet demanding aerospace specifications, and ensure compatibility throughout the supply chain.

Key Topics

  • Material Specification: Details the requirements for aluminium alloy AL-P2014A, a high-strength alloy frequently used in aerospace structures.
  • Extrusion Process: Outlines acceptable manufacturing practices for extruding bars and sections, guaranteeing consistency and quality.
  • Mechanical Properties: Establishes criteria for the T4511 temper condition, which combines optimized strength and workability for aerospace uses.
  • Dimensional Tolerances: Defines maximum size parameters for bars and sections (a or D ≤ 200 mm) to facilitate compatibility with typical aerospace designs.
  • Alternative Tempers: Permits supply in the T4510 condition if specified by the purchaser, ensuring flexibility in procurement.

Applications

Extruded bars and sections conforming to EN 2100:1992 are essential in multiple critical aerospace applications, including:

  • Aircraft Structural Components: Used for frames, supports, and braces where strength-to-weight ratio is crucial.
  • Engine and Landing Gear Parts: Ideal for parts needing high mechanical integrity and precise dimensions.
  • Spacecraft Assemblies: Ensures reliability under the strict environmental and load conditions found in space.
  • Aerospace Tooling and Fixtures: Common material choice for developing precision jigs and fixtures used during assembly or maintenance.

Suppliers and manufacturers outside the aerospace industry may also reference this standard for high-performance aluminium products requiring strict quality control and traceability.

Related Standards

EN 2100:1992 is part of a family of standards addressing the needs of the aerospace sector for aluminium materials. Related standards include:

  • EN 485 Series: Specifications for wrought aluminium sheets, strips, and plates.
  • EN 586 Series: Standards for aluminium alloy extruded rods, bars, tubes, and profiles.
  • EN 2500 Series: Other standards for aerospace-grade aluminium alloys, covering different tempers and forms.
  • EN 2000 Series: General aerospace materials requirements and testing methods.
  • ISO 209: International standard for wrought aluminium and aluminium alloys - chemical composition and mechanical properties.

By adhering to EN 2100:1992 and its related standards, organizations ensure compliance with aerospace procurement requirements and boost material reliability across highly demanding applications.


Keywords: EN 2100:1992, aluminium alloy AL-P2014A, T4511, extruded bars, aerospace standards, aluminium sections, CEN, material specification, aerospace aluminium, quality control

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Frequently Asked Questions

EN 2100:1992 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Aluminium alloy AL-P2014A T4511 - Extruded bars and sections a or D < or = 200 mm". This standard covers: This standard specifies the requirements relating to extruded bars and sections in aluminium alloy AL-P2014A, for use in the T4511 condition, a or D inferior or equal to 200 mm, for aerospace applications. This standard may also be used to supply material in the T4510 condition, if the purchaser specifies this condition on the order. In this case, the designation of line 97 shall not be used.

This standard specifies the requirements relating to extruded bars and sections in aluminium alloy AL-P2014A, for use in the T4511 condition, a or D inferior or equal to 200 mm, for aerospace applications. This standard may also be used to supply material in the T4510 condition, if the purchaser specifies this condition on the order. In this case, the designation of line 97 shall not be used.

EN 2100:1992 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 2100:1992 has the following relationships with other standards: It is inter standard links to EN ISO 11399:2000, EN ISO 7933:2004, CR 1752:1998, EN ISO 10551:2001. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

EN 2100:1992 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)


2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Aluminium alloy AL-P2014A T4511 - Extruded bars and sections a or D < or = 200 mmLuft- und Raumfahrt - Aluminiumlegierung AL-P2014A T4511 - Stranggepreßte Stangen und Profile a oder D < oder = 200 mmSérie aérospatiale - Alliage d'aluminium AL-P2014A T4511 - Barres et profil
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