Abstract

This standard specifies the characteristics for blanking plugs with lockring for pipe couplings 8°30', in titanium alloy, for aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range: - 55 °C to  + 135 °C

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

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SIST EN 3270:2004 is the Slovenian standard for blanking plugs with lockring for 8°30' pipe couplings in titanium alloy, issued by SIST on the basis of EN 3270:2001. It specifies the characteristics needed for aerospace applications, including dimensions, materials, surface treatment, marking and designation. Engineers, manufacturers, inspectors and buyers use it to specify and check compatible parts for aerospace fluid system connections.

What does SIST EN 3270:2004 specify?

SIST EN 3270:2004 specifies blanking plugs with lockring for pipe couplings 8°30' in titanium alloy, intended for aerospace use. It covers parts up to a nominal pressure of 28 000 kPa and a temperature range from -55 °C to +135 °C.

The standard is organized into six clauses: scope, normative references, required characteristics, designation, marking and technical specification. Clause 3 is the main technical part, because it ties the plug geometry, materials and surface treatment to the referenced figures, table and external standards.

What are the key requirements of SIST EN 3270:2004?

SIST EN 3270:2004 sets out the plug's configuration, materials, surface condition, identification and related technical basis. In practice, it tells the manufacturer what to make, what references to follow and how the finished part is to be identified.

Geometry and dimensions

Clause 3.1 says the configuration, dimensions and mass are given by Figure 1 and Table 1, and that dimensions apply before lubricating or anodizing. This matters because the part has to fit the matching coupling correctly before any coating changes its final size.

Table 1 links each code to the thread designation, associated dimensions, mass and lockring reference. For the reader, this is the ordering and drawing reference for selecting the correct size.

Surface condition

Clause 3.2 states that surface roughness follows Figure 1 unless the design documentation says otherwise. That gives the designer or supplier a defined finish to meet when the drawing does not override it.

Materials

Clause 3.3 requires the blanking plug material to comply with EN 3311 or EN 3314. This means the plug must be made from one of the specified titanium alloy bar materials suitable for machining.

Surface treatments

Clause 3.4 gives two approved surface-treatment routes. One is lubrication according to EN 2491 on all surfaces, after abrasive blasting with non-metallic grit, with a film thickness in the stated range. The other is anodizing according to AMS 2488D, type 2. In practice, this gives the supplier a controlled choice of finish, depending on the build specification.

Designation

Clause 4 gives the ordering designation format: a description block, the standard reference and the code from Table 1, with code I9005 inserted if needed. This matters for procurement because it fixes how the part is named on documents and purchase orders.

Marking

Clause 5 requires marking according to EN 2424, style A, and Figure 1. That tells production and inspection teams how the part is to be identified on the component itself.

Technical specification

Clause 6 points to EN 3079, type II. This links the blanking plug to the technical specification for the related pipe coupling family, so users know which broader coupling requirements apply.

What terms does SIST EN 3270:2004 define?

  • Blanking plug - A threaded plug used to close the coupling opening and protect the port.
  • Lockring - The ring used with the plug to secure the connection in service.
  • Pipe coupling 8°30' - The aerospace coupling geometry addressed by this standard.
  • MJ threads - The thread form used for the plug sizes listed in the standard.
  • Port end - The coupling-side end, whose dimensions are referenced to EN 2603.
  • Style A - The marking style required by EN 2424 for these parts.
  • Type II - The technical specification category referenced from EN 3079.

Who uses SIST EN 3270:2004?

SIST EN 3270:2004 is used by aerospace manufacturers, machining suppliers, quality control teams and buyers who specify titanium alloy pipe-coupling parts. It is also useful for inspectors and engineers who need to verify dimensions, materials, surface treatment, marking and part designation for blanking plugs with lockring.

What changed in SIST EN 3270:2004 from the previous edition?

SIST EN 3270:2004 is identical to EN 3270:2001.

Which standards are used with SIST EN 3270:2004?

SIST EN 3270:2004 relies on several companion standards:

  • ISO 5855-3 - limit dimensions for MJ threads for fluid-system fittings.
  • EN 2424 - marking of aerospace products.
  • EN 2491 - coating methods for molybdenum disulphide dry lubricants.
  • EN 2602 - dimensions for ports for straight metric-size unions with locking ring.
  • EN 2603 - dimensions for the port end of straight metric-size unions with locking ring.
  • EN 2645 - dimensions for the locking ring.
  • EN 3079 - technical specification for the related 8°30' pipe coupling adaptors.
  • EN 3311 and EN 3314 - titanium alloy bar materials for machining.
  • AMS 2488D - anodic treatment for titanium and titanium alloys.

What does the SIST EN 3270:2004 document contain?

The document contains a figure for the plug configuration and a table that ties each code to the corresponding thread, dimensions, mass and lockring reference. It also provides an example designation to show how the part is identified for ordering.

Clause 3 is the main technical section, because it combines geometry, roughness, materials and surface treatment. Clause 4 supports procurement and part identification, while Clause 5 supports product marking and Clause 6 links the plug to the broader coupling technical specification.

Relations

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28-Jan-2026
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28-Jan-2026
Effective Date
28-Jan-2026
Effective Date
01-May-2004

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Frequently Asked Questions

SIST EN 3270:2004 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Pipe coupling 8°30' in titanium alloy - Blanking plugs with lockring". This standard covers: This standard specifies the characteristics for blanking plugs with lockring for pipe couplings 8°30', in titanium alloy, for aerospace applications. Nominal pressure: up to 28 000 kPa Temperature range: - 55 °C to + 135 °C

This standard specifies the characteristics for blanking plugs with lockring for pipe couplings 8°30', in titanium alloy, for aerospace applications. Nominal pressure: up to 28 000 kPa Temperature range: - 55 °C to + 135 °C

SIST EN 3270:2004 is classified under the following ICS (International Classification for Standards) categories: 49.030.20 - Bolts, screws, studs. The ICS classification helps identify the subject area and facilitates finding related standards.

SIST EN 3270:2004 has the following relationships with other standards: It is inter standard links to SIST EN 2602:2006, SIST EN 3311:2024, oSIST prEN 415-2:2022, SIST EN 3079:2009, SIST EN 2491:2011, SIST EN 2645:2006, SIST EN 2603:2006, SIST EN 2424:2008, SIST EN 2608:2006, SIST EN 3270:2004/AC:2004. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

SIST EN 3270:2004 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 coupling 8°30' in titanium alloy - Blanking plugs with
lockring
Aerospace series - Pipe coupling 8°30' in titanium alloy - Blanking plugs with lockring
Luft- und Raumfahrt - Rohrverschraubung 8°30' aus Titanlegierung -
Verschlußschrauben mit Sicherungsring
Série aérospatiale - Systeme de raccordement 8°30' en alliage de titane - Obturateurs
filetés avec bague de freinage
Ta slovenski standard je istoveten z: EN 3270:2001
ICS:
49.030.20 Sorniki, vijaki, stebelni vijaki Bolts, screws, studs
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD
EN 3270
NORME EUROPÉENNE
EUROPÄISCHE NORM
October 2001
ICS 49.030.20
English version
Aerospace series - Pipe coupling 8°30' in titanium alloy -
Blanking plugs with lockring
Série aérospatiale - Système de raccordement 8°30' en Luft- und Raumfahrt - Rohrverschraubung 8°30' aus
alliage de titane - Obturateurs filetés avec bague de Titanlegierung - Verschlußschrauben mit Sicherungsring
freinage
This European Standard was approved by CEN on 6 January 2001.
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, 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
© 2001 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 3270:2001 E
worldwide for CEN national Members.

Foreword
This European Standard has been prepared by the European Association of Aerospace Manufacturers
(AECMA).
After inquiries 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 April 2002, and conflicting national standards shall be withdrawn at
the latest by April 2002.
According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following
countries are bound to implement this European Standard: Austria, Belgium, Czech Republic, Denmark,
Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal,
Spain, Sweden, Switzerland and the United Kingdom.
1 Scope
This standard specifies the characteristics for blanking plugs with lockring for pipe couplings 830', in titanium
alloy, for aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range: – 55 C to + 135 C
2 Normative references
This European Standard inco
...