EN 6092:2016

Aerospace series - Receptacle, floating, double lug

This European Standard specifies the dimensions, tolerances, required characteristics and mass of a receptacle for use in fuselage interior equipment and structural applications. This standard shall be used in conjunction with studs per EN 6088 or EN 6105.

Luft- und Raumfahrt - Haltenocken, schwimmend, zweiseitig

Série aérospatiale - Réceptacle, flottant, double patte

Aeronavtika - Vtičnica, gibljiva, dvostranska

Ta evropski standard določa dimenzije, tolerance, zahtevane lastnosti in maso vtičnic za uporabo v notranji opremi v trupu letala ter konstrukcijsko uporabo. Ta standard je treba uporabljati v povezavi z določili za stojne vijake v skladu s standardom EN 6088 ali EN 6105.

General Information

• Status: Published
• Publication Date: 30-Aug-2016
• Withdrawal Date: 27-Feb-2017
• ICS: 49.030.99 - Other fasteners
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 3 - Mechanical
• Current Stage: 6060 - Definitive text made available (DAV) - Publishing
• Start Date: 31-Aug-2016
• Completion Date: 31-Aug-2016
• Ref Project: SIST EN 6092:2016 - Aerospace series - Receptacle, floating, double lug

Overview

EN 6092:2016 is a European aerospace standard that specifies the design, dimensions, tolerances, materials, surface treatments and mass for a floating, double-lug receptacle intended for fuselage interior equipment and structural applications. The receptacle is intended for use with studs conforming to EN 6088 or EN 6105 and is designed to deliver controlled floatability and reliable mechanical retention across typical aircraft environmental and mechanical conditions.

Key Topics

• Configuration and tolerances: Dimensions and tolerances are specified in millimetres and apply after surface treatment. Unspecified tolerances default to ISO 2768-1 (class m). All burrs are to be removed and sharp edges broken.
• Materials and finishes: The standard lists acceptable corrosion-resistant steels and titanium alloy options with specific surface treatments such as passivation, dry film lubricant (MIL-PRF-46010), IVD coating (MIL-DTL-83488) and anodizing of titanium per EN 2808. Material options include stainless steels (e.g. 1.4303, 1.4404) and titanium alloy caps where specified.
• Mechanical requirements: EN 6092 defines minimum floatability (0.64 mm radial), maximum axial tensile load (6 000 N) and recommended locking torque range (2.8–3.2 Nm). Operating temperature range is −55 °C to 150 °C.
• Procurement and marking: Receptacles may be supplied as assemblies or separate parts with procurement codes and bag quantities defined. Marking follows EN 2424 (style F) and EN 6095 is referenced for the technical specification.

Applications

EN 6092 receptacles are used where secure, repeatable attachment points are required inside aircraft fuselages or in structural subassemblies. Practical benefits include:

• Interchangeability and standardization: Conformance to EN 6092 ensures parts are compatible across suppliers and installations that use EN 6088/EN 6105 studs.
• Controlled float: The specified floatability accommodates alignment variation between panels and studs, reducing stress concentrations and easing installation.
• Environmental robustness: Specified materials and surface treatments provide corrosion resistance and performance across the stated temperature range.
• Predictable mechanical performance: Defined axial load and torque limits support reliable structural and equipment retention.

Related Standards

• EN 6088 / EN 6105 - Studs used with this receptacle
• EN 6094, EN 6090, EN 6091 - Retaining washers and circlips referenced for installation
• EN 2424 - Marking of aerospace products
• EN 6095 - Technical specification referenced by EN 6092
• EN 10088-3, EN 2516, EN 2808 - Material and surface treatment references

Adopting EN 6092:2016 in procurement and design helps ensure compatibility, repeatable installation, and predictable mechanical behaviour for aircraft interior and structural fastening points.

Standards Content (Sample)

SLOVENSKI STANDARD
01-november-2016
$HURQDYWLND9WLþQLFDJLEOMLYDGYRVWUDQVND
Aerospace series - Receptacle, floating, double lug
Luft- und Raumfahrt - Haltenocken, schwimmend, zweiseitig
Série aérospatiale - Réceptacle, flottant, double patte
Ta slovenski standard je istoveten z: EN 6092:2016
ICS:
49.030.99 Drugi vezni elementi Other fasteners
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EN 6092
EUROPEAN STANDARD
NORME EUROPÉENNE
August 2016
EUROPÄISCHE NORM
ICS 49.030.99
English Version
Aerospace series - Receptacle, floating, double lug
Série aérospatiale - Réceptacle, flottant, double patte Luft- und Raumfahrt - Haltenocken, schwimmend,
zweiseitig
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 6092:2016 E
worldwide for CEN national Members.

Contents Page
European foreword . 3
1 Scope . 4
2 Normative references . 4
3 Requirements . 5
4 Designation . 9
5 Marking . 9
6 Technical specification . 9
7 Example of installation . 9

European foreword
This document (EN 6092:2016) 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 February 2017, and conflicting national standards shall be
withdrawn at the latest by February 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, 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 the United Kingdom.
1 Scope
This European Standard specifies the dimensions, tolerances, required characteristics and mass of a
receptacle for use in fuselage interior equipment and structural applications. This standard shall be used in
conjunction with studs per EN 6088 or EN 6105.
2 Normative references
The following documents, in whole or in part, are normatively referenced in this document and are
indispensable for its application. For dated references, only the edition cited applies. For undated references,
the latest edition of the referenced document (including any amendments) applies.
DIN 17850, Titanium,
...