Aerospace series - Screw, pan head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C

This document specifies the characteristics of externally threaded fasteners, pan head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated, for aerospace applications.
Classification: 1 100 MPa /315 °C .

Luft- und Raumfahrt - Flachkopfschraube mit Spiral Antrieb, grobe Schafttoleranz, mittlere Gewindelänge, aus Titanlegierung, anodisiert, MoS2 geschmiert - Klasse: 1 100 MPa (bei Raumtemperatur)/315 °C

Dieses Dokument legt die Eigenschaften von Verbindungselementen mit Außengewinde, Flachkopfschraube, Spiral-Antrieb, grobe Schafttoleranz, mittellanges Gewinde, aus Titanlegierung, anodisiert, MoS2-geschmiert, für Luft- und Raumfahrtanwendungen fest.
Klasse: 1 100 MPa /315 °C .

Série aérospatiale - Vis à tête cylindrique, empreinte en spirale, tige normale à tolérance large, filetage moyen, en alliage de titane, anodisée, lubrifiée au MoS2 - Classification : 1 100 MPa (à température ambiante)/315 °C

Le présent document spécifie les caractéristiques des éléments de fixation à filetage extérieur, à tête cylindrique, empreinte en spirale, tige normale à tolérance large, filetage moyen, en alliage de titane, anodisés, lubrifiés au MoS2, pour les applications aérospatiales.
Classification : 1 100 MPa/315 °C.

Aeronavtika - Vijak, valjasta glava, spiralna vdolbina, široka toleranca, srednja navojna dolžina, iz titanove zlitine, anodiziran, mazan z MoS2 - Klasifikacija: 1100 MPa (pri temperaturi okolice)/315 °C

Ta dokument določa značilnosti zunanjih navojnih veznih elementov – valjasta glava, spiralna vdolbina, široka toleranca, srednja navojna dolžina, iz titanove zlitine, anodiziranih, mazanih z MoS2 – za uporabo v aeronavtiki.
Klasifikacija: 1100 MPa/315 °C.

General Information

Status
Published
Publication Date
05-Apr-2022
Technical Committee
I13 - Imaginarni 13
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
30-Mar-2022
Due Date
04-Jun-2022
Completion Date
06-Apr-2022

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SIST EN 4848:2022

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Overview

SIST EN 4848:2022 is a European standard developed by the Slovenian Institute for Standardization (SIST) that specifies the requirements for pan head screws designed for aerospace applications. These screws feature a Spiral Drive Recess, coarse tolerance normal shank, medium length thread, and are manufactured from titanium alloy. The fasteners are anodized for enhanced corrosion resistance and lubricated with molybdenum disulphide (MoS2) to reduce friction and wear. The standard classifies these screws with a minimum tensile strength of 1 100 MPa at ambient temperature and a maximum recommended operating temperature of 315 °C.

Use of this standard ensures reliability, mechanical performance, and quality in demanding aerospace engineering environments.

Key Topics

  • Scope and Purpose
    SIST EN 4848:2022 provides detailed specifications for externally threaded, pan head screws with a Spiral Drive Recess, aimed at the aerospace sector. It covers classification by mechanical and thermal performance, surface finishes, lubrication, marking, and quality assurance requirements.

  • Material and Surface Treatment

    • Fabrication from titanium alloys ensures a high strength-to-weight ratio and excellent corrosion resistance.
    • Anodizing is required for improved surface durability and oxidation resistance, according to EN 2808.
    • Lubrication with MoS2 (per EN 3021 and EN 2491) minimizes thread galling and torque variability.
  • Mechanical and Thermal Classification

    • Minimum tensile strength: 1 100 MPa at ambient conditions.
    • Maximum operating temperature: 315 °C, beyond which permanent property changes may occur.
  • Geometry and Tolerances

    • Dimensions and tolerances for threads, shank, and head are tightly controlled to ensure compatibility with aerospace assemblies.
    • References to other standards for threads (ISO 5855-2), form (ISO 7913), and Spiral Drive geometry (EN 4609).
  • Quality and Marking

    • Stringent quality management systems (such as EN 9100) are mandatory for manufacturers.
    • Indelible marking is specified for traceability, following EN 2424.

Applications

The screws covered by SIST EN 4848:2022 are used primarily in aerospace applications where high mechanical strength, light weight, and reliable performance under fluctuating temperatures are critical. Typical uses include:

  • Aircraft and spacecraft structural assemblies
  • Engine components subject to vibration and thermal cycling
  • Avionics and interior hardware needing corrosion protection and precise tolerance fits

Additionally, these pan head, Spiral Drive Recess screws are ideal for fastener applications where high resistance to stripping and ease of maintenance are valued, due to the drive’s effective torque transmission and reduced cam-out.

Related Standards

Adherence to SIST EN 4848:2022 often requires familiarity with interrelated standards for full compliance and performance assurance:

  • EN 2424 - Marking of aerospace products
  • EN 2491 / EN 3021 - MoS2 dry lubricants and coating methods
  • EN 2808 - Anodizing of titanium and titanium alloys
  • EN 3813 - Titanium alloy procurement
  • EN 4609 - Spiral Drive recess geometric requirements
  • ISO 5855-2 - MJ thread limits
  • ISO 7913 - Tolerances of form and position for bolts and screws
  • EN 9100 - Aerospace quality management systems
  • EN 9133 - Qualification procedures for aerospace standard products

SIST EN 4848:2022 ensures that screws used in critical aerospace environments meet stringent durability, strength, and quality demands, supporting safety and longevity in high-performance applications.

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SIST EN 4848:2022

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Frequently Asked Questions

SIST EN 4848:2022 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Screw, pan head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C". This standard covers: This document specifies the characteristics of externally threaded fasteners, pan head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated, for aerospace applications. Classification: 1 100 MPa /315 °C .

This document specifies the characteristics of externally threaded fasteners, pan head, Spiral Drive Recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated, for aerospace applications. Classification: 1 100 MPa /315 °C .

SIST EN 4848:2022 is classified under the following ICS (International Classification for Standards) categories: 49.025.30 - Titanium; 49.030.20 - Bolts, screws, studs. The ICS classification helps identify the subject area and facilitates finding related standards.

SIST EN 4848:2022 has the following relationships with other standards: It is inter standard links to SIST EN 2808:2001, SIST EN 4609:2020, SIST EN 2491:2011, SIST EN 3021:2017, SIST EN 840-6:2004+A1:2008, SIST EN 2424:2008, SIST EN 3813:2014, SIST EN 14460:2006. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

SIST EN 4848:2022 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-2022
Aeronavtika - Vijak, valjasta glava, spiralna vdolbina, široka toleranca, srednja
navojna dolžina, iz titanove zlitine, anodiziran, mazan z MoS2 - Klasifikacija: 1100
MPa (pri temperaturi okolice)/315 °C
Aerospace series - Screw, pan head, Spiral Drive Recess, coarse tolerance normal
shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated -
Classification: 1 100 MPa (at ambient temperature)/315 °C
Luft- und Raumfahrt - Flachkopfschraube mit Spiral Antrieb, grobe Schafttoleranz,
mittlere Gewindelänge, aus Titanlegierung, anodisiert, MoS2 geschmiert - Klasse: 1 100
MPa (bei Raumtemperatur)/315 °C
Série aérospatiale - Vis à tête cylindrique, empreinte en spirale, tige normale à tolérance
large, filetage moyen, en alliage de titane, anodisée, lubrifiée au MoS2 - Classification : 1
100 MPa (à température ambiante)/315 °C
Ta slovenski standard je istoveten z: EN 4848:2022
ICS:
49.025.30 Titan Titanium
49.030.20 Sorniki, vijaki, stebelni vijaki Bolts, screws, studs
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EN 4848
EUROPEAN STANDARD
NORME EUROPÉENNE
March 2022
EUROPÄISCHE NORM
ICS 49.030.20
English Version
Aerospace series - Screw, pan head, Spiral Drive Recess,
coarse tolerance normal shank, medium length thread, in
titanium alloy, anodized, MoS2 lubricated - Classification:
1 100 MPa (at ambient temperature)/315 °C
Série aérospatiale - Vis à tête cylindrique, empreinte en Luft- und Raumfahrt - Flachkopfschraube mit Spiral
spirale, tige normale à tolérance large, filetage moyen, Antrieb, grobe Schafttoleranz, mittlere Gewindelänge,
en alliage de titane, anodisée, lubrifiée au MoS2 - aus Titanlegierung, anodisiert, MoS2 geschmiert -
Classification : 1 100 MPa (à température Klasse: 1 100 MPa (bei Raumtemperatur)/315 °C
ambiante)/315 °C
This European Standard was approved by CEN on 10 January 2022.

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, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway,
Poland, Portugal, Republic of North Macedonia, 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
© 2022 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4848:2022 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 . 6
4.1 Configuration — Dimensions — Masses . 6
4.2 Tolerances of form and position . 9
4.3 Materials . 9
4.4 Surface treatment . 9
4.5 Lubrication . 9
5 Designation . 9
6 Marking . 9
7 Technical specification . 10
Bibliography. 11

European foreword
This document (EN 4848:2022) 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 September 2022, and conflicting national standards shall
be withdrawn at the latest by September 2022.
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, Switzerland, Turkey and
the United Kingdom.
Introduction
Aerospace and Defence Standardisation (ASD-STAN) draws attention to the fact that it is claimed that
compliance with this document may involve the use of a patent „Spiral Drive System for Threaded
Fasteners“ EP1025370B1.
ASD-STAN takes no position concerning the evidence, validity and scope of this patent right.
The hold
...