SIST EN 3852:2004
(Main)Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 - Straight unions, welded, threaded
Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 - Straight unions, welded, threaded
This standard specifies the characteristics of threaded welded straight unions for pipe couplings, 60°, spherical, in TI-P64001, for aerospace applications.
NOTE Assembly in accordance with TR 4052.
Luft- und Raumfahrt - Rohrverschraubungen mit Kugelbuchsen, 60 °, aus Titanlegierung TI-P64001 - Gerade Verschraubungen zum Anschweißen
Diese Norm legt die Eigenschaften von geraden Verschraubungen zum Anschweißen für Rohrverschraubungen 60° mit Kugelbuchse, aus TI P64001, für Anwendungen in der Luft- und Raumfahrt fest.
ANMERKUNG Montage nach TR 4052.
Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 - Straight unions, welded, threaded
General Information
- Status
- Published
- Publication Date
- 30-Apr-2004
- Technical Committee
- I08 - Imaginarni 08
- Current Stage
- 6060 - National Implementation/Publication (Adopted Project)
- Start Date
- 01-May-2004
- Due Date
- 01-May-2004
- Completion Date
- 01-May-2004
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 62931:2017 - GX16t-5 capped tubular LED lamp - Safety specifications (IEC 62931:2017) - Effective Date
- 09-Feb-2026
- Referred By
SIST EN 62776:2015 - Double-capped LED lamps for general lighting services - Safety specifications - Effective Date
- 09-Feb-2026
- Effective Date
- 09-Feb-2026
- Referred By
SIST EN IEC 60598-1:2025 - Luminaires - Part 1: General requirements and tests (IEC 60598-1:2024) - Effective Date
- 09-Feb-2026
- Referred By
SIST EN IEC 62031:2020 - LED modules for general lighting - Safety specifications (IEC 62031:2018) - Effective Date
- 09-Feb-2026
- Effective Date
- 09-Feb-2026
- Effective Date
- 09-Feb-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
Overview
SIST EN 3852:2004 is a European standard developed by CEN for the aerospace sector, specifically addressing pipe couplings of the 60° spherical type, utilizing titanium alloy TI-P64001. It details the specifications for threaded, welded straight unions, which are critical components in aerospace hydraulic and fluid conveyance systems. The standard ensures the uniformity, compatibility, and reliability of these unions across aerospace applications, supporting both quality and safety requirements.
Key Topics
- Product Scope: The standard defines characteristics for straight unions that are both threaded and welded, suitable for 60° spherical pipe couplings manufactured in titanium alloy TI-P64001.
- Material Specification: Titanium alloy TI-P64001 is emphasized for its high strength, lightweight properties, and corrosion resistance, crucial qualities for aerospace environments.
- Dimensional Requirements: Detailed guidelines for dimensions, tolerances, and configuration ensure precise fit and function in fluid and hydraulic applications. These prescriptions reference ISO and EN standards for threads and tolerances.
- Marking and Identification: Consistent marking requirements based on EN 2424 enable traceability and identification, supporting maintenance and quality assurance.
- Quality Assurance: Includes references to EN 2000 for quality system approval, ensuring that manufacturers meet stringent aerospace quality criteria.
- Assembly and Processing: Noted alignment with technical report TR 4052, which provides assembly recommendations for these unions in practice.
Applications
SIST EN 3852:2004-compliant straight unions are integral to:
- Aerospace Hydraulic Systems: Used extensively in hydraulic and fuel lines, where lightweight strength and reliable sealing are mandatory.
- Maintenance and Retrofitting: Standardized unions simplify replacement, upgrades, and repairs in both new and existing aerospace systems.
- OEM and Supply Chain Standardization: Enables aircraft manufacturers and suppliers to achieve interoperability, streamline logistics, and assure component quality throughout production and field operations.
- Critical Fluid Conveyance: The specified titanium alloy is particularly suited to demanding aerospace applications, offering performance in extreme environments and reducing the risk of corrosion-related failure.
By adhering to SIST EN 3852:2004, organizations benefit from increased safety, simplified integration, and compliance with European aerospace industry requirements.
Related Standards
Understanding and applying SIST EN 3852:2004 often involves coordination with associated standards:
- ISO 286-2: Governs tolerance grades and limit deviations for holes and shafts, referenced for dimensional accuracy.
- ISO 5855-3: Defines MJ thread profiles and limits, ensuring thread compatibility in aerospace fluid systems.
- EN 2000: Provides quality assurance guidance for the approval of aerospace product manufacturers.
- EN 2424: Specifies marking procedures for consistent identification of aerospace products.
- EN 2530: Pertains to the material properties and specifications for titanium alloy TI-P63, relevant for comparisons and cross-material selection.
- EN 2656: Details welded end configuration requirements for pipe couplings.
- TR 4052: Offers assembly recommendations specifically for 60° spherical pipe couplings in titanium alloy.
Summary
SIST EN 3852:2004 contributes significantly to safe and efficient aerospace fluid systems through detailed specifications for pipe coupling straight unions in titanium alloy TI-P64001. By providing a unified approach to material selection, dimensions, marking, and quality assurance, it ensures compatibility, performance, and regulatory compliance across the aerospace industry. Manufacturers, suppliers, and maintenance organizations in the aerospace sector rely on this standard for high-performance, durable pipelines and hydraulic systems.
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Frequently Asked Questions
SIST EN 3852:2004 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 - Straight unions, welded, threaded". This standard covers: This standard specifies the characteristics of threaded welded straight unions for pipe couplings, 60°, spherical, in TI-P64001, for aerospace applications. NOTE Assembly in accordance with TR 4052.
This standard specifies the characteristics of threaded welded straight unions for pipe couplings, 60°, spherical, in TI-P64001, for aerospace applications. NOTE Assembly in accordance with TR 4052.
SIST EN 3852:2004 is classified under the following ICS (International Classification for Standards) categories: 49.080 - Aerospace fluid systems and components. The ICS classification helps identify the subject area and facilitates finding related standards.
SIST EN 3852:2004 has the following relationships with other standards: It is inter standard links to SIST EN 9133:2018, SIST EN 2656:2002, oSIST prEN 415-2:2022, SIST EN 9100:2018, SIST EN 2424:2008, SIST EN 1715-1:1998, SIST EN 62931:2017, SIST EN 62776:2015, SIST EN 62031:2008/A2:2015, SIST EN IEC 60598-1:2025, SIST EN IEC 62031:2020, SIST EN 62838:2016, SIST EN 62560:2013/A1:2015, SIST EN 3855:2004, SIST EN 13272-1:2020. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
SIST EN 3852:2004 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-2004
Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 -
Straight unions, welded, threaded
Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 - Straight
unions, welded, threaded
Luft- und Raumfahrt - Rohrverschraubungen mit Kugelbuchsen, 60 °, aus Titanlegierung
TI-P64001 - Gerade Verschraubungen zum Anschweißen
Ta slovenski standard je istoveten z: EN 3852:2002
ICS:
49.080 /HWDOVNLLQYHVROMVNL Aerospace fluid systems and
KLGUDYOLþQLVLVWHPLLQGHOL components
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EUROPEAN STANDARD
EN 3852
NORME EUROPÉENNE
EUROPÄISCHE NORM
November 2002
ICS 49.080
English version
Aerospace series - Pipe couplings, 60°, spherical, in titanium
alloy TI-P64001 - Straight unions, welded, threaded
Série aérospatiale - Raccords sphériques, 60° , en alliage
de titane TI-P64001 - Raccords droits, soudés, filetés
This European Standard was approved by CEN on 30 August 2002.
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 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 Management Centre has the same status as the official
versions.
CEN members are the national standards bodies of Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece,
Iceland, Ireland, Italy, Luxembourg, Malta, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre: rue de Stassart, 36 B-1050 Brussels
© 2002 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 3852:2002 E
worldwide for CEN national Members.
Contents
Foreword.3
1 Scope .3
2 Normative references .3
3 Required characteristics.4
3.1 Configuration - Dimensions – Tolerances.4
3.2 Material.4
4 Designation.7
5 Marking .7
6 Quality assurance .7
Foreword
This document (EN 3852:2002) 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 May 2003, and conflicting national standa
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