EN 6129:2016
(Main)Aerospace series - Blind bolt, protruding head, high strength, pulltype
Aerospace series - Blind bolt, protruding head, high strength, pulltype
This standard specifies the configuration, dimension, tolerances and mass of a stainless steel blind bolt with protruding head, for aerospace application.
Luft- und Raumfahrt - Blindniet, Universalkopf, hochfest (Zugtyp)
Série aérospatiale - Boulon aveugle, tête saillante, haute résistance, installation en tirant
Aeronavtika - Slepa kovica, štrleča glava, zelo trdna, povlečni tip
Ta standard določa konfiguracijo, dimenzije, tolerance in maso slepih kovic iz nerjavnega jekla s štrlečo glavo za uporabo v aeronavtiki.
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Standards Content (Sample)
SLOVENSKI STANDARD
01-november-2016
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Aerospace series - Blind bolt, protruding head, high strength, pulltype
Luft- und Raumfahrt - Blindniet, Universalkopf, hochfest (Zugtyp)
Série aérospatiale - Boulon aveugle, tête protubérante, haute résistance, installation en
tirant
Ta slovenski standard je istoveten z: EN 6129:2016
ICS:
49.030.20 Sorniki, vijaki, stebelni vijaki Bolts, screws, studs
49.030.60 Kovice Rivets
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EN 6129
EUROPEAN STANDARD
NORME EUROPÉENNE
September 2016
EUROPÄISCHE NORM
ICS 49.030.20; 49.030.60
English Version
Aerospace series - Blind bolt, protruding head, high
strength, pulltype
Série aérospatiale - Boulon aveugle, tête protubérante, Luft- und Raumfahrt - Blindniet, Universalkopf,
haute résistance, installation en tirant hochfest (Zugtyp)
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 6129:2016 E
worldwide for CEN national Members.
Contents Page
European foreword . 3
1 Scope . 4
2 Normative references . 4
3 Requirements . 4
3.1 Configuration, dimensions and tolerances . 4
3.2 Grip range and weight . 4
3.3 Material, finish, lubrication . 5
4 Designation . 10
5 Marking . 10
6 Technical specification . 10
European foreword
This document (EN 6129:2016) 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, 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 standard specifies the configuration, dimension, tolerances and mass of a stainless steel blind bolt with
protruding head, for aerospace application.
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.
EN 2424, Aerospace series — Marking of aerospace products
1)
EN 4473, Aerospace series — Aluminium pigmented coatings for fasteners — Technical specification
2)
AS 5272, Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting Procurement Specification
2)
SAE AMS 5687, Nickel Alloy, Corrosion and Heat-Resistant, Wire 74Ni — 15,5Cr — 8,0Fe — Annealed
SAE AMS 5737, Steel, corrosion and heat-resistant, bars, wire, forgings and tubing 15Cr — 25.5Ni — 1.2Mo —
2.1Ti — 0.006B — 0.30V, consumable electrode melted, 1650 °F (899 °C), solution and precipitation heat
2)
treated
2)
AMS-QQ-P-35, Passivation treatments for Corrosion-Resistant Steel
3)
MIL-PRF-46010F, Lubricant, Solid Film, Heat cured, Corrosion Inhibiting NATO Code-S-1738
3)
SAE AS 87132, Lubricant, Cetyl Alcohol, 1- Hexadecanol, Application to fasteners
3)
DOD-L-85645, Lubricant, Dry Thin Film, Molecular Bonded
NASM 8975, Fasteners, Blind, High Strength, Installation Formed, Corrosion Resistant Steel, Heat Resistant
4)
Steel and Titanium, General Specification for
3 Requirements
3.1 Configuration, dimensions and tolerances
The configuration, dimensions, tolerances, static and dynamic values shall conform to Figures 1 and 2 and
Tables 1 and 2.
3.2 Grip range and weight
See Tables 3 and 4.
1)
Published as AECMA Prestandard at the date of publication of this standard.
2)
Published by: Society of Automotive Engineers (SAE), 400 Commonwealth drive, Warrendale, PA 15096-0001, USA.
) Published by: Department of Defense (DoD), the Pentagon, Washington, D.C. 20301, USA.
4)
Published by: Aerospace Industries Association of America, Inc. (AIA), 1250 Eye Street, N.W., Washington,
D.C. 20005-3924, USA.
3.3 Material, finish, lubrication
See Tables 5 and 6.
Key
1 Marking, see clause 5. 5 Grip
2 Sleeve shall not rotating. 6 Locking collar
3 Diameter of serrated pin head shall not 7 Shifting anvil: Fasteners are supplied with shifting
exceed Ø D max. anvil of man
...
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