EN 6105:2016
(Main)Aerospace series - Stud with shoulder
Aerospace series - Stud with shoulder
This standard specifies the dimensions, tolerances, required characteristics and mass of a stud for use in fuselage interior equipment and structural applications. This standard shall be used in conjunction with retaining washer per EN6090A01 (conform to EN 6090) and receptacles per EN 6092 or EN 6093.
Luft- und Raumfahrt - Verschlussbolzen mit Bund
Série aérospatiale - Axe à épaulement
Aeronavtika - Stojni vijak z ramo
Ta standard določa dimenzije, tolerance, zahtevane lastnosti in maso stojnih vijakov za uporabo v notranji opremi v trupu letala ter konstrukcijsko uporabo. Ta standard je treba uporabljati v povezavi z določili za zadrževalne podložke v skladu s standardom EN6090A01 (EN 6090) in za vtičnice v skladu s standardom EN 6092 ali EN 6093.
General Information
- Status
- Published
- Publication Date
- 06-Sep-2016
- Withdrawal Date
- 30-Mar-2017
- Technical Committee
- ASD-STAN - Aerospace
- Drafting Committee
- ASD-STAN/D 3 - Mechanical
- Current Stage
- 6060 - Definitive text made available (DAV) - Publishing
- Start Date
- 07-Sep-2016
- Completion Date
- 07-Sep-2016
Relations
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
Overview
EN 6105:2016 - "Aerospace series - Stud with shoulder" is a CEN standard that specifies the configuration, dimensions, tolerances, required characteristics and mass of a shoulder-type stud intended for fuselage interior equipment and structural aerospace applications. The standard is to be used in conjunction with retaining washers (EN 6090 / EN6090A01) and receptacles (EN 6092 or EN 6093), and sets requirements for material, surface treatment, mechanical performance and marking.
Key topics and technical requirements
- Dimensions & tolerances
- Dimensions are given in millimetres (see Figure 1 / Table 2 of the standard). Tolerances not specified follow ISO 2768‑1. All dimensions/tolerances apply after surface treatment.
- Burrs must be removed and sharp edges broken.
- Size range & mass
- Multiple size codes (010–160) with defined grip ranges. Mass per 1 000 pieces approximately 1.63 kg to 6.42 kg depending on size.
- Thread options
- Accepts 0.1640‑32 UNJC‑3B (SAE‑AS8879) or 0.1640‑32 UNC‑3B (MIL‑S‑7742), 2 lead (optional versions noted).
- Materials & surface treatment
- Materials include corrosion‑resistant steels (e.g., SAE‑AMS5629, SAE‑AMS5737) or heat‑resisting alloy per EN 4318. Passivation per SAE‑AMS2700 or IVD coating per MIL‑DTL‑83488 are referenced.
- Mechanical characteristics
- Ultimate tension load: 6 300 N (note: fastening system with receptacle EN 6092/6093 = 6 000 N).
- Ultimate shear load: 9 000 N.
- Installation torque: 2.8 Nm to 3.2 Nm (with EN 6092 / EN 6093 receptacles).
- Operating temperature
- Rated for –55 °C to +150 °C.
- Designation & marking
- Marking per EN 2424, style C. Technical specification referenced: EN 6095.
Practical applications and who uses EN 6105:2016
- Intended for designers and engineers of aircraft fuselage interiors and structural assemblies requiring removable fastenings with controlled grip and load capacity.
- Used by:
- Aerospace OEMs and suppliers specifying standard hardware
- Procurement and quality assurance teams to verify conformity
- MRO organizations and installation technicians applying correct torque and components
- Test engineers validating mechanical performance with matching receptacles (EN 6092 / EN 6093)
- Typical applications: panel attachments, interior equipment mounting, and structural retention points where a shoulder stud with defined grip range and controlled installation characteristics is required.
Related standards (normative references)
- EN 6090 / EN6090A01 (washer, retaining), EN 6092, EN 6093 (receptacles), EN 6094, EN 6095
- EN 2424 (marking), EN 2516, EN 4318
- ISO 2768‑1, SAE‑AMS2700, SAE‑AMS5629, SAE‑AMS5737, SAE‑AS8879, MIL‑DTL‑83488, MIL‑S‑7742, NASM 33781
Keywords: EN 6105:2016, stud with shoulder, aerospace stud, fuselage interior, receptacle EN 6092, EN 6093, retaining washer EN 6090, installation torque, aerospace fasteners, dimensions tolerances.
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Frequently Asked Questions
EN 6105:2016 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Stud with shoulder". This standard covers: This standard specifies the dimensions, tolerances, required characteristics and mass of a stud for use in fuselage interior equipment and structural applications. This standard shall be used in conjunction with retaining washer per EN6090A01 (conform to EN 6090) and receptacles per EN 6092 or EN 6093.
This standard specifies the dimensions, tolerances, required characteristics and mass of a stud for use in fuselage interior equipment and structural applications. This standard shall be used in conjunction with retaining washer per EN6090A01 (conform to EN 6090) and receptacles per EN 6092 or EN 6093.
EN 6105:2016 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.
EN 6105:2016 has the following relationships with other standards: It is inter standard links to EN 4318:2025, EN ISO/ASTM 52945:2024, EN ISO 13703-2:2023, EN ISO 4884:2019. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
EN 6105:2016 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-november-2016
Aeronavtika - Stojni vijak z ramo
Aerospace series - Stud with shoulder
Luft- und Raumfahrt - Verschlußbolzen mit Bund
Série aérospatiale - Axe à épaulement
Ta slovenski standard je istoveten z: EN 6105:2016
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.
EN 6105
EUROPEAN STANDARD
NORME EUROPÉENNE
September 2016
EUROPÄISCHE NORM
ICS 49.030.20
English Version
Aerospace series - Stud with shoulder
Série aérospatiale - Axe à épaulement Luft- und Raumfahrt - Verschlussbolzen mit Bund
This European Standard was approved by CEN on 11 March 2016.
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, 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: Avenue Marnix 17, B-1000 Brussels
© 2016 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 6105:2016 E
worldwide for CEN national Members.
Contents Page
European foreword . 3
1 Scope . 4
2 Normative references . 4
3 Requirements . 5
3.1 Configuration, dimensions, tolerances and mass . 5
3.2 Material and surface treatment. 6
3.3 Mechanical characteristics . 7
3.3.1 General . 7
3.3.2 Static values . 7
3.3.3 Installation torque . 7
3.4 Operating temperature . 7
4 Designation . 7
5 Marking . 7
6 Technical specification . 7
7 Example of installation . 8
European foreword
This document (EN 6105:2016) 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 March 2017, and conflicting national standards shall be withdrawn
at the latest by March 2017.
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, Croatia, Cyprus, Czech
Republic, Denmar
...
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