EN 2115:2009
(Main)Aerospace series - Aluminium alloy 2117-T42 - Wire for solid rivets - D ≤ 10 mm
Aerospace series - Aluminium alloy 2117-T42 - Wire for solid rivets - D ≤ 10 mm
This standard specifies the requirements relating to:
Aluminium alloy 2117-T42
Wire for solid rivets
D < or = 10 mm
for aerospace applications.
Luft- und Raumfahrt - Aluminiumlegierung 2117-T42 - Nietdrähte für Vollniete - D ≤ 10 mm
Diese Norm legt die Anforderungen an
Aluminiumlegierung 2117-T42
Nietdrähte für Vollniete
D ≤ 10 mm
für Anwendungen in der Luft- und Raumfahrt fest.
Série aérospatiale - Alliage d’aluminium 2117-T42 - Fils pour rivets pleins - D ≤ 10 mm
Aeronavtika - Aluminijeva zlitina 2117-T42 - Žica za polne kovice - D =< 10 mm
General Information
- Status
- Published
- Publication Date
- 10-Feb-2009
- Withdrawal Date
- 30-Aug-2009
- Technical Committee
- ASD-STAN - Aerospace
- Drafting Committee
- ASD-STAN/D 4 - Metallic
- Current Stage
- 9093 - Decision to confirm - Review Enquiry
- Start Date
- 21-Jan-2025
- Completion Date
- 21-Jan-2026
Relations
- Effective Date
- 28-Jan-2026
- Referred By
EN 6069:2009 - Aerospace series - Rivet, 100° reduced flush head, close tolerance - Inch series - Effective Date
- 28-Jan-2026
- Referred By
EN 6069:2022 - Aerospace series - Rivet, 100° reduced flush head, close tolerance - Inch series - Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
Overview
EN 2115:2009 is a CEN (ASD‑STAN) aerospace standard that specifies requirements for aluminium alloy 2117‑T42 supplied as wire for solid rivets with a diameter of D ≤ 10 mm. The document defines material designation, manufacturing form and method, delivery and use conditions, heat treatment reference, mechanical characteristics and required inspections tailored to aerospace applications.
Key topics and requirements
- Material and form
- Aluminium alloy: 2117‑T42.
- Form: wire for manufacture of solid rivets.
- Production method: cold drawn.
- Maximum diameter: D ≤ 10 mm.
- Chemical composition
- The standard sets compositional limits for elements including Si, Fe, Cu, Mn, Mg, Cr, Zn and Al (composition limits are specified in the standard).
- Heat treatment and conditions
- Delivery condition: H14 (alternatively H13 or H15 are acceptable).
- Use condition: T42 (reference heat treatment provided).
- Reference heat treatment: (specified as) solution treatment followed by water quench and natural aging to T42 - the standard gives temperature, time and quench parameters (see EN 2115:2009 for exact values).
- Mechanical properties and tests
- Tensile strength (Rm) and shear strength requirements are defined (Rm range and shear minimums are provided in the standard).
- Test pieces and sample preparation follow the provisions of EN 2070‑6 (rivet wire technical specification).
- Direction of test piece, ambient test temperature, and inspection procedures are specified.
- Inspection and inspection criteria
- External defects, marking and dimensional inspections reference EN 2070‑6.
- Dimensions and tolerances should comply with order requirements or dimensional standards referenced in TR 2410.
- Qualification
- Product qualification program to be agreed between manufacturer and purchaser.
Applications and who uses this standard
- Primary users: aerospace manufacturers, rivet producers, fastener suppliers, material and quality engineers, procurement teams and design engineers specifying rivets for airframes and structural assemblies.
- Practical uses: specifying rivet wire material and condition in purchase orders, verifying supplier compliance during incoming inspection, defining heat‑treatment schedules to achieve T42 condition, and ensuring mechanical performance for aircraft riveting operations.
Related standards
- EN 2070‑6 - Aluminium & aluminium alloy wrought products: Technical specification - Part 6: Rivet wire
- EN 2032‑2 - Coding of metallurgical condition in delivery condition
- EN 4258 - Organization of aerospace metallic material standards
- EN 4500‑2 - Rules for drafting aluminium/magnesium material standards
- TR 2410 - Relationship between dimensional and material standards
Keywords: EN 2115:2009, Aluminium alloy 2117‑T42, wire for solid rivets, rivet wire D ≤ 10 mm, aerospace standard, CEN, ASD‑STAN.
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Frequently Asked Questions
EN 2115:2009 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Aluminium alloy 2117-T42 - Wire for solid rivets - D ≤ 10 mm". This standard covers: This standard specifies the requirements relating to: Aluminium alloy 2117-T42 Wire for solid rivets D < or = 10 mm for aerospace applications.
This standard specifies the requirements relating to: Aluminium alloy 2117-T42 Wire for solid rivets D < or = 10 mm for aerospace applications.
EN 2115:2009 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 2115:2009 has the following relationships with other standards: It is inter standard links to EN 4258:2024, EN 6069:2009, EN 6069:2022, EN ISO 8504-3:2001. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
EN 2115:2009 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-maj-2009
Aeronavtika - Aluminijeva zlitina 2117-T42 - Žica za polne kovice - D =< 10 mm
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PP
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Ta slovenski standard je istoveten z: EN 2115:2009
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EUROPEAN STANDARD
EN 2115
NORME EUROPÉENNE
EUROPÄISCHE NORM
February 2009
ICS 49.025.20
English Version
Aerospace series - Aluminium alloy 2117-T42 - Wire for solid
rivets - D ≤ 10 mm
Série aérospatiale - Alliage d'aluminium 2117-T42 - Fils Luft- und Raumfahrt - Aluminiumlegierung 2117-T42 -
pour rivets pleins - D ≤ 10 mm Nietdrähte für Vollniete - D ≤ 10 mm
This European Standard was approved by CEN on 16 August 2008.
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 CEN Management Centre 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 CEN Management Centre has the same status as the
official versions.
CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland,
France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal,
Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre: Avenue Marnix 17, B-1000 Brussels
© 2009 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 2115:2009: E
worldwide for CEN national Members.
Foreword
This document (EN 2115:2009) has been prepared by the Aerospace and Defence Industries Association of
Europe - Standardization (ASD-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 ASD,
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 August 2009, and conflicting national standards shall be withdrawn at
the latest by August 2009.
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, Bulgaria, Cyprus, Czech
Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia,
Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain,
Sweden, Switzerland and the United Kingd
...
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