EN 6052:2022
(Main)Aerospace series - Rivet-collar-system, aluminium alloy, shear type, inch series - Technical Specification
Aerospace series - Rivet-collar-system, aluminium alloy, shear type, inch series - Technical Specification
This document defines the requirements for qualification, acceptance, delivery and inspection of 100° countersunk head, 100° countersunk reduced head and protruding head close tolerance pins, shear type in aluminium alloy 7050-T73 and collars of aluminium alloy 3003 and of aluminium alloy 6061-T7 for use as permanent fasteners in aerospace applications.
Luft- und Raumfahrt - Passniet-Schließring-System aus Aluminiumlegierung für Scherbeanspruchung, Zöllige Reihe - Technische Lieferbedingungen
Dieses Dokument legt die Anforderungen für die Qualifikation, Abnahme, Auslieferung und Prüfung von 100° Senk-Passstiften, 100° Senk-Passstiften mit kleinem Kopf und Senk-Passstiften mit überstehendem Kopf für Scherbeanspruchung aus Aluminiumlegierung 7050 T73 und Schließringe aus Aluminiumlegierung 3003 und Aluminiumlegierung 6061 T7 für die Verwendung als dauerhafte Verbindungselemente in Anwendungen der Luft- und Raumfahrt fest.
Série aérospatiale - Système rivet-collier, alliage d'aluminium, type cisaillement, série en inches - Spécification technique
Le présent document définit les exigences relatives à la qualification, la réception, la livraison et le contrôle des broches à tête fraisée 100°, à tête fraisée réduite 100° et à tête saillante, à tolérance serrée et de type cisaillement en alliage d’aluminium 7050-T73, ainsi que des colliers en alliages d’aluminium 3003 et 6061-T7, pour une utilisation en tant qu’élément de fixation permanent dans les applications aérospatiales.
Aeronavtika - Sistem zakovic, aluminijeva zlitina, strižni tip, palčne mere - Tehnična specifikacija
General Information
Standards Content (Sample)
SLOVENSKI STANDARD
01-december-2022
Aeronavtika - Sistem zakovic, aluminijeva zlitina, strižni tip, palčne mere -
Tehnična specifikacija
Aerospace series - Rivet-collar-system, aluminium alloy, shear type, inch series -
Technical Specification
Luft- und Raumfahrt - Passniet-Schließring-System aus Aluminiumlegierung für
Scherbeanspruchung, Zöllige Reihe - Technische Lieferbedingungen
Série aérospatiale - Système rivet-collier, alliage d'aluminium, type cisaillement, série en
inches - Spécification technique
Ta slovenski standard je istoveten z: EN 6052:2022
ICS:
49.025.20 Aluminij Aluminium
49.030.60 Kovice Rivets
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EN 6052
EUROPEAN STANDARD
NORME EUROPÉENNE
October 2022
EUROPÄISCHE NORM
ICS 49.030.60
English Version
Aerospace series - Rivet-collar-system, aluminium alloy,
shear type, inch series - Technical Specification
Série aérospatiale - Système rivet-collier, alliage Luft- und Raumfahrt - Passniet-Schließring-System aus
d'aluminium, type cisaillement, série en inches - Aluminiumlegierung für Scherbeanspruchung, Zöllige
Spécification technique Reihe - Technische Lieferbedingungen
This European Standard was approved by CEN on 6 October 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, Türkiye 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 6052:2022 E
worldwide for CEN national Members.
Contents Page
European foreword . 3
1 Scope . 4
2 Normative references . 4
3 Terms and definitions . 4
4 General requirements . 5
5 Requirements for pins in aluminium alloy 7050-T73 . 5
6 Requirements for collars in aluminium alloy 3003 and 6061. 8
7 Certification and quality assurance . 10
7.1 Qualification tests . 10
7.2 Quality conformance inspection . 10
7.3 Quality control records . 10
7.4 Lot . 10
8 Delivery . 20
8.1 Unit type containers . 20
8.2 Unit packages . 20
9 Quality management system. 20
Annex A (informative) Record of revisions . 21
Bibliography. 22
European foreword
This document (EN 6052:2022) 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 document has
received the approval of the National Associations and the Official Services of the member countries of
ASD-STAN, 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 2023, and conflicting national standards shall be
withdrawn at the latest by April 2023.
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.
Any feedback and questions on this document should be directed to the users’ national standards body.
A complete listing of these bodies can be found on the CEN website.
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, 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, Türkiye and the
United Kingdom.
1 Scope
This document defines the requirements for qualification, acceptance, delivery and inspection of 100°
countersunk head, 100° countersunk reduced head and protruding head close tolerance pins, shear
type in aluminium alloy 7050-T73 and collars of aluminium alloy 3003 and of aluminium alloy 6061-T7
for use as permanent fasteners in aerospace applications.
2 Normative references
The following documents are referred to in the text in such a way that some or all of their content
constitutes requirements of this document. For dated references, only the edition cited applies. For
undated references, the latest edition of the referenced document (including any amendments) applies.
EN 3115, Aerospace series — Aluminium alloy 7050-T73 — Wire for solid rivets — D ≤ 10 mm
ANSI/ASQ Z 1.4, Sampling Procedures and Tables for Inspection by Attributes
ANSI/ASME B 46.1, Surface Texture, Surface Roughness, Waviness and Lay
ASTM-B193, Standard Test Method for Resistivity of Electrical Conductor Materials
ASTM E 1417/E 1417M, Standard Practice for Liquid Penetrant Testing
ASTM E 8/E 8Ma, Standard Test Methods for Tension Testing of Metallic Materials
ASTM-E92, Standard Test Methods for Vickers Hardness and Knoop Hardness of Metallic Materials
ASTM-G-110, Standard Practice for Evaluating Intergranular Corrosion Resistance of Heat Treatable
Aluminum Alloys by Immersion in Sodium Chloride + Hydrogen Peroxide Solution
NASM1312, Fastener Test Methods
FED-SPEC QQ-A-430, Aluminium Alloy Rod and Wire, for Rivets and Cold Heading
SAE AMS2644, Inspection Material, Penetrant
3 Terms and definitions
No terms and definitions are listed in this document.
ISO and IEC maintain terminological databases for use in standardization at the following addresses:
• ISO Online browsing platform: available at https://www.iso.org/obp/
• IEC Electropedia: available at https://www.electropedia.org/
1 Published by: Department of Defense (DoD), the Pentagon, Washington, D.C., 20307, USA.
2 Published by: American Society for Testing and Materials, 100 Barr Harbor Dr., West Conshohocken, P.A., 19428,
USA.
3 Published by: Aerospace Industries Association of America Inc. (AIA), 1250 Eye Street, N.W., Washington, D.C.,
20005-3924, USA.
4 Published by: Superindendent of documents, US Government Printing House, Washington, D.C., 20402, USA.
5 Published by: Engineering Society for Advancing Mobility Land, Sea, Air and Space International (SAE),
400 Commonwealth Drive, Warrendale, P.A., 15096-0001, USA.
4 General requirements
The close tolerance pins and collars covered by this specification shall be of the types, sizes,
configurations and materials designated by the part numbers specified on the applicable standards
which refer to this specification.
5 Requirements for pins in aluminium alloy 7050-T73
The requirements for 7050-T73 aluminium alloy pins, shear type are given in Table 1. These
requirements complement the requirements of all other standards or specifications referenced in the
document of the pins and may be overridden only when specially instructed in the definition document.
Inspection tests given in Table 1 and Table 2 are mandatory (except as noted) on each lot as defined in
7.2 for the fastener manufacturer. Tests which are not mandatory for the fastener manufacturer may be
applied by the receiving contractor.
Table 1 — Requirements for pins in aluminium alloy 7050-T73
Inspection and test Qualification Acceptance
Clause Characteristic Technical requirement
method Sampling Sampling
5.1 General The dimensions and any deviations in Conventional
dimensions form and position, measured at measuring methods
ambient temperature, shall be within
the limits specified in the standard part
drawings and this procurement
specification
5.2 Shank Underfill permissible, shall be within Standard
diameter the specified shank diameter range micrometer 6,35 mm
(¼”) diameter
5.3 Shank Refer to Table 8 Conventional
straightness measuring methods
According to According to
5.4 Sealant escape Refer to Figure 3 and Table 10
Table 3 Table 5
groove
5.5 Head According to standard part drawings In accordance with
protrusion EN pin standards
(100° heads)
5.6 Surface texture Visual examination
according to
ANSI/ASME B 46.1
5.7 Lubricants According to
applicable
5.8 Finish
specification and
visual examination
5.9 Product Visual examination
identification
5.10 Delivery Refer to Clause 8 N/A
5.11 Shear strength Table 7 double shear values are Test no 13 of
applicable for pins having a grip of 2 × NASM1312
nominal diameter or greater for
protruding head type and grip of 2,5 ×
According to According to
nominal diameter or greater for flush
Table 3 Table 6
head type. If the pin is too short to
perform the shear test, a piece of wire
of the same raw material lot heat
treated with the fasteners shall be
tested. The test wire shall have the
Inspection and test Qualification Acceptance
Clause Characteristic Technical requirement
method Sampling Sampling
same coating as for pins.
Minimum shear strength test of
fasteners is to be performed on pins or
wire without cetyl alcohol lubrication
applied.
5.12 Tensile Table 7 values are applicable for pins Test no 8 of
strength having a grip of 1,5 × nominal diameter NASM1312
or greater.
Qualification and acceptance testing
shall be performed with a 7° sloped
surface (collar side) in minimum and
maximum grip with collar according to
collar standard.
5.13 Head dishing After installation in a clearance fit of Test no. 8 of
0,025 mm, head dishing of flush head NASM1312
pins shall not exceed 0,076 mm (see
Figure 6).
Testing shall be performed with a
7° sloped surface (collar side) in
minimum and maximum grip.
5.14 Pin break load Table 7 values are applicable.
Tensile load shall be applied axially at Test no. 8 of
a rate, which breaks the pin at a NASM1312
minimum of 4 s of load application.
Test plate countersink for countersunk
pins shall have 2° angular
misalignment from the hole centerline.
Test plate for protruding head pins
shall have a 2° slope under the pin
head.
After evaluation of the pin break loads, ASTM E 1417/E 141
head dishing of flush head pins shall 7M
not exceed 0,076 mm (see Figure 6).
Cracks shall not be allowed in any
location of the pin. The presence of
cracks shall be determined by
fluorescent penetrant inspection
according to ASTM E 1417/E 1417M,
method B or D, sensitivity level 2 or
higher.
The penetrant materials used shall be
according to SAE AMS2644. Examine
all surfaces at 10 × to 30 ×
magnification.
Inspection and test Qualification Acceptance
Clause Characteristic Technical requirement
method Sampling Sampling
Penetrant inspection shall be
performed prior to all surface coating
and lubricating.
5.15 Preload Table 7 values are applicable to pins Test no. 16 of
having a nominal grip of 1,5 × nominal NASM1312
diameter or greater.
...
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