SIST EN 3314:2019
(Main)Aerospace series - Titanium alloy TI-P64001 - Solution treated and aged - Bar for machining - D ≤ 75 mm
Aerospace series - Titanium alloy TI-P64001 - Solution treated and aged - Bar for machining - D ≤ 75 mm
This document specifies the requirements relating to:
Titanium alloy TI-P64001
Solution treated and aged
Bar for machining
D ≤ 75 mm
for aerospace applications.
Luft- und Raumfahrt - Titanlegierung TI-P64001 - Lösungsgeglüht und ausgelagert - Stangen zum Zerspanen - D ≤ 75 mm
Diese Europäische Norm legt die Anforderungen an:
Titanlegierung TI P64001
Lösungsgeglüht und ausgelagert
Stangen zum Zerspanen
D ≤ 75 mm
zur Anwendung in der Luft und Raumfahrt fest.
Série aérospatiale - Alliage de titane TI-P64001 - Mis en solution et revenu - Barres pour usinage - D ≤ 75 mm
Aeronavtika - Titanova zlitina TI-P64001 - Topilno žarjena in starana - Palice za obdelavo - D ≤ 75 mm
Ta dokument določa zahteve, ki se nanašajo na:
titanove zlitine TI-P64001,
topilno žarjene in starane,
palice za obdelavo,
D ≤ 75 mm,
za uporabo v aeronavtiki.
General Information
- Status
- Published
- Publication Date
- 15-Apr-2019
- Technical Committee
- I13 - Imaginarni 13
- Current Stage
- 6060 - National Implementation/Publication (Adopted Project)
- Start Date
- 11-Apr-2019
- Due Date
- 16-Jun-2019
- Completion Date
- 16-Apr-2019
Relations
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Referred By
SIST EN 3268:2015 - Aerospace series - Pipe coupling 8°30' in titanium alloy - Pressure plugs - Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
Overview
SIST EN 3314:2019 defines requirements for titanium alloy TI-P64001, specifically for bars with diameters not exceeding 75 mm, which have undergone solution treatment and aging. Developed by the Slovenian Institute for Standardization (SIST), this European standard is tailored for aerospace applications, ensuring optimal material performance for machining processes. By following this standard, manufacturers and suppliers deliver titanium bars with consistent quality and properties aligned with international aerospace demands.
Key Topics
- Material Specification: The standard focuses on titanium alloy TI-P64001, recognized for its strength, lightweight nature, and corrosion resistance - essential attributes in aerospace engineering.
- Delivery Condition: Bars covered must be delivered in a solution treated and aged condition, providing enhanced mechanical properties suitable for demanding aerospace applications.
- Dimensional Limits: Applicable to bars intended for machining, with a maximum diameter (D) of 75 mm, supporting precise manufacturing and component fabrication.
- Mechanical Properties: Requirements address essential mechanical characteristics, including proof stress, tensile strength, elongation, and reduction of area, tested at ambient temperature to ensure structural reliability.
- Microstructure & Quality Control: The standard details acceptable microstructures (referencing EN 3114-002 and EN 4800-002) and mandates rigorous inspection for internal and external defects, supporting consistent quality for critical aerospace components.
Applications
SIST EN 3314:2019 is particularly valuable for:
- Aerospace Component Manufacturing: Titanium alloy bars manufactured to this standard are ideal for components where high strength-to-weight ratio, machinability, and durability are paramount, such as aircraft fasteners, landing gear parts, engine mountings, and structural airframe elements.
- High-Performance Engineering: Beyond aerospace, industries such as defense, motorsport, and advanced transportation benefit from the use of titanium bars meeting these strict specifications, especially where mechanical integrity and weight savings are critical.
- Machining & Fabrication: The defined properties and dimensions facilitate efficient precision machining, ensuring that final products meet stringent aerospace tolerances and service requirements.
Related Standards
To ensure compliance and seamless integration, SIST EN 3314:2019 references several related standards:
- EN 2500-004: Guidance on drafting and use of metallic material standards for the aerospace sector.
- EN 2600: Specifies rules for designating metallic semi-finished products.
- EN 3114-002: Outlines test methods and microstructure evaluation for (α + β) titanium alloy wrought products.
- EN 4258: Structures general organization of aerospace metallic materials standardization.
- EN 4267: Provides dimensions for round bars in titanium and titanium alloys.
- EN 4500-004: Sets rules for drafting material standards, particularly for titanium and titanium alloys.
- EN 4800-002: Technical specification for titanium and titanium alloy bars and sections.
Practical Value
Following SIST EN 3314:2019 offers significant practical advantages:
- Guarantees that titanium alloy bars for aerospace purposes are reliable, manufacturers are assured of consistent mechanical and physical properties.
- Streamlines procurement and quality assurance processes by aligning with recognized European standards.
- Enhances safety, performance, and longevity of aerospace components through stringent controls on alloy composition, treatment, and testing.
- Facilitates international collaboration and supply chain integration by harmonizing technical requirements across member states.
Keywords: titanium alloy bar, TI-P64001, aerospace series, solution treated and aged, machining, mechanical properties, SIST EN 3314:2019, European standard, material requirements, quality assurance, precision engineering.
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Frequently Asked Questions
SIST EN 3314:2019 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Titanium alloy TI-P64001 - Solution treated and aged - Bar for machining - D ≤ 75 mm". This standard covers: This document specifies the requirements relating to: Titanium alloy TI-P64001 Solution treated and aged Bar for machining D ≤ 75 mm for aerospace applications.
This document specifies the requirements relating to: Titanium alloy TI-P64001 Solution treated and aged Bar for machining D ≤ 75 mm for aerospace applications.
SIST EN 3314:2019 is classified under the following ICS (International Classification for Standards) categories: 49.025.30 - Titanium. The ICS classification helps identify the subject area and facilitates finding related standards.
SIST EN 3314:2019 has the following relationships with other standards: It is inter standard links to SIST EN 2600:2019, SIST EN 4800-002:2025, SIST EN 3114-002:2009, SIST EN 4500-004:2024, SIST EN 4258:2024, SIST EN 4267:2002, SIST EN 3268:2015, SIST EN 4686:2015. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
SIST EN 3314:2019 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)
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Ta slovenski standard je istoveten z: EN 3314:2019
ICS:
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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EN 3314
EUROPEAN STANDARD
NORME EUROPÉENNE
April 2019
EUROPÄISCHE NORM
ICS 49.025.30
English Version
Aerospace series - Titanium alloy TI-P64001 - Solution
treated and aged - Bar for machining - D ≤ 75 mm
Série aérospatiale - Alliage de titane TI-P64001 - Mis Luft- und Raumfahrt - Titanlegierung TI-P64001 -
Lösungsgeglüht und ausgelagert - Stangen zum
en solution et revenu - Barres pour usinage - D ≤ 75
mm Zerspanen - D ≤ 75 mm
This European Standard was approved by CEN on 2 December 2018.
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-CENELEC 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-CENELEC Management
Centre has the same status as the official versions.
CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia,
Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania,
Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland,
Turkey and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
CEN-CENELEC Management Centre: Rue de la Science 23, B-1040 Brussels
© 2019 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 3314:2019 E
worldwide for CEN national Members.
Contents Page
European foreword . 3
Introduction . 4
1 Scope . 5
2 Normative references . 5
3 Terms and definitions . 5
4 Requirements . 5
European foreword
This document (EN 3314:2019) 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 October 2019, and conflicting national standards shall
be withdrawn at the latest by October 2019.
Attention is drawn to the possibility that some of the elements of this document may be the subject of
patent rights. CEN 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, Croatia,
Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France,
Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands,
Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden,
...