EN 4458:2005
(Main)Aerospace series - Studs, MJ threads, in titanium alloy TI-P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel - Strength class: 1 100 MPa (at ambient temperature) - Technical specification
Aerospace series - Studs, MJ threads, in titanium alloy TI-P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel - Strength class: 1 100 MPa (at ambient temperature) - Technical specification
This standard specifies the characteristics, qualification and acceptance requirements for studs with MJ threads in TI-P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel.
Strength class: 1 100 MPa
It is applicable whenever referenced.
Luft- und Raumfahrt - Stiftschrauben, MJ-Gewinde aus Titanlegierung TI-P64001, MoS2 beschichtet, mit Ringsicherung aus korrosionsbeständigem Stahl - Festigkeitsklasse: 1 100 MPa (bei Raumtemperatur) - Technische Lieferbedingungen
Diese Norm legt die Eigenschaften sowie die Qualifikations- und Annahmeanforderungen für Stiftschrauben mit MJ-Gewinde aus TI-P64001, MoS2-beschichtet, mit verzahntem Sicherungsring aus korrosionsbestän¬digem Stahl fest.
Festigkeitsklasse: 1 100 MPa )
Sie ist immer dann anzuwenden, wenn auf sie verwiesen wird.
Série aérospatiale - Goujons, filetage MJ, en alliage de titane TI-P64001, revêtus MoS2, avec bague de verrouillage dentelée en acier résistant à la corrosion - Classe de résistance : 1 100 MPa (à température ambiante) - Spécification technique
Aeronavtika – Stebelni vijaki, navoj MJ, iz titanove zlitine TI-P64001, prevlečeni z MoS2, z nagubanim pritrdilnim obročem iz korozijsko odpornega jekla – Trdnostni razred: 1 100 MPa (pri temperaturi okolice) – Tehnična specifikacija
General Information
- Status
- Published
- Publication Date
- 15-Nov-2005
- Withdrawal Date
- 30-May-2006
- Technical Committee
- ASD-STAN - Aerospace
- Drafting Committee
- ASD-STAN/D 3 - Mechanical
- Current Stage
- 6060 - Definitive text made available (DAV) - Publishing
- Start Date
- 16-Nov-2005
- Completion Date
- 16-Nov-2005
Relations
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
Overview
EN 4458:2005 is a CEN aerospace technical specification that defines the characteristics, qualification and acceptance requirements for studs with MJ threads made from titanium alloy TI‑P64001, MoS2 coated, and fitted with a serrated locking ring in corrosion‑resisting steel. The studs are classified strength class 1 100 MPa (minimum tensile strength at ambient temperature). The standard applies whenever referenced in procurement, design or quality documents for aerospace standard parts.
Key topics and technical requirements
- Material and strength
- Titanium alloy TI‑P64001 studs; minimum tensile strength 1 100 MPa at ambient temperature.
- Hydrogen content limit: ≤ 0.0125 % on material removed from the head.
- Coating and locking feature
- MoS2 (molybdenum disulfide) coating specified; serrated locking ring made of corrosion‑resisting steel.
- Manufacturing controls
- Forging and heat treatment controls (blanks not heat treated more than twice).
- Threads formed by a single rolling process after full heat treatment.
- Inspection and testing
- Qualification and batch acceptance schemes (sampling by simple random sampling).
- Mechanical tests: tensile, tension‑fatigue (mean life ≥ 65 000 cycles; individual ≥ 45 000 cycles; max 130 000 cycles) and rotational resistance.
- Metallurgical checks: macroscopic thread grain flow, microscopic microstructure (to detect overheating, contamination), and surface discontinuity inspection (fluorescent penetrant per ISO 3452).
- Surface contamination limit: ≤ 0,08 mm for all diameters.
- Quality and sampling
- Uses sampling plans and AQLs per ISO 2859‑1; defects classified (critical/major/minor) with example AQLs (e.g., 0.065 % for surface discontinuities, 1 % for thread size/coating/marking).
- Ancillary requirements
- Product marking, packaging and labelling requirements; test blocks and mechanical test assembly defined in Annex A and B.
Applications
- Specification for procurement, manufacture and acceptance of aerospace fasteners where high‑strength titanium studs with locking rings are required.
- Used in structural and joining assemblies in aircraft and aerospace systems where weight, strength and corrosion resistance are critical.
- Provides the basis for supplier qualification, lot release, and quality assurance processes.
Who uses this standard
- Aerospace manufacturers and OEMs
- Fastener and specialty hardware suppliers
- Procurement and quality engineers
- Design engineers specifying fasteners for aerostructures
- Test laboratories performing tensile, fatigue and NDT inspections
Related standards
- ISO 2859‑1 (sampling procedures), ISO 3452 (penetrant inspection), ISO 7961 (bolts test methods), EN ISO 4288 (surface texture) and EN 9133 (qualification for aerospace standard parts). EN 4460 (installation/removal procedure) is also referenced.
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Frequently Asked Questions
EN 4458:2005 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Studs, MJ threads, in titanium alloy TI-P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel - Strength class: 1 100 MPa (at ambient temperature) - Technical specification". This standard covers: This standard specifies the characteristics, qualification and acceptance requirements for studs with MJ threads in TI-P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel. Strength class: 1 100 MPa It is applicable whenever referenced.
This standard specifies the characteristics, qualification and acceptance requirements for studs with MJ threads in TI-P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel. Strength class: 1 100 MPa It is applicable whenever referenced.
EN 4458:2005 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 4458:2005 has the following relationships with other standards: It is inter standard links to EN 4460:2005, EN 196-1:1994, EN ISO 21920-3:2022, EN 9133:2018, EN 4421:2007. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
EN 4458:2005 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)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Studs, MJ threads, in titanium alloy TI-P64001, MoS2 coated, with serrated locking ring in corrosion resisting steel - Strength class: 1 100 MPa (at ambient temperature) - Technical specificationLMDSérie aérospatiale - Goujons, filetage MJ, en alliage de titane TI-P64001, revetus MoS2, avec bague de verrouillage dentelée en acier résistant a la corrosion - Classe de résistance : 1 100 MPa (a température ambiante) - Spécification techniqueLuft- und Raumfahrt - Stiftschrauben, MJ-Gewinde aus Titanlegierung TI-P64001, MoS2 beschichtet, mit Ringsicherung aus korrosionsbeständigem Stahl - Festigkeitsklasse: 1 100 MPa (bei Raumtemperatur) - Technische LieferbedingungenTa slovenski standard je istoveten z:EN 4458:2005SIST EN 4458:2006en49.030.20ICS:SLOVENSKI
STANDARDSIST EN 4458:200601-september-2006
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 4458November 2005ICS 49.030.20 English VersionAerospace series - Studs, MJ threads, in titanium alloy TI-P64001, MoS2 coated, with serrated locking ring in corrosionresisting steel - Strength class: 1 100 MPa (at ambienttemperature) - Technical specificationSérie aérospatiale - Goujons, filetage MJ, en alliage detitane TI-P64001, revêtus MoS2, avec bague deverrouillage dentelée en acier résistant à la corrosion -Classe de résistance : 1 100 MPa (à températureambiante) - Spécification techniqueLuft- und Raumfahrt - Stiftschrauben, MJ-Gewinde ausTitanlegierung TI-P64001, MoS2 beschichtet, mitRingsicherung aus korrosionsbeständigem Stahl -Festigkeitsklasse: 1 100 MPa (bei Raumtemperatur) -Technische LieferbedingungenThis European Standard was approved by CEN on 26 September 2005.CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this EuropeanStandard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such nationalstandards may be obtained on application to the Central Secretariat or to any CEN member.This European Standard exists in three official versions (English, French, German). A version in any other language made by translationunder the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the officialversions.CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France,Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia,Slovenia, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMITÉ EUROPÉEN DE NORMALISATIONEUROPÄISCHES KOMITEE FÜR NORMUNGManagement Centre: rue de Stassart, 36
B-1050 Brussels© 2005 CENAll rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 4458:2005: E
Definition of test block.16 Annex B (normative)
Assembly for mechanical tests.17
1) Minimum tensile strength of the material at ambient temperature. 2) Published as AECMA Prestandard at the date of publication of this standard.
3.2.1 crack rupture in the material which may extend in any direction and which may be intercrystalline or transcrystalline in character 3.2.2 seam open surface defect 3.2.3 lap surface defect caused by folding over metal fins or sharp corners and then compressing them into the surface 3.3 test temperature ambient temperature, unless otherwise specified 3.4 simple random sampling the taking of n items from a population of N items in such a way that all possible combinations of n items have the same probability of being chosen
3.5 critical defect a defect that, according to judgement and experience, is likely to result in hazardous or unsafe conditions for individuals using, maintaining, or depending upon the considered product, or that is likely to prevent performance of the function of a major end item 3.6 major defect a defect other than critical, that is likely to result in a failure or to reduce materially the usability of the considered product for its intended purpose
3.7 minor defect a defect that is not likely to reduce materially the usability of the considered product for its intended purpose, or that is a departure from established specification having little bearing on the effective use or operation of this product 3.8 sampling plan a plan according to which one or more samples are taken in order to obtain information and possibly to reach a decision
3.9 limiting quality in a sampling plan, the quality limit which corresponds to the specified 10 % probability of acceptance 3.10 acceptable quality limit (AQL) a quality limit which in a sampling plan corresponds to a specified but relatively high probability of acceptance It is the maximum per cent defective (or the maximum number of defects per hundred units) that, for purposes of sampling inspection can be considered satisfactory as a process average.
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