prEN 3327
(Main)Aerospace series - Bolts, double hexagon head, close tolerance, medium thread length, in heat resisting nickel base alloy NI-P100HT (Inconel 718), uncoated - Classification: 1 275 MPa/650 °C
Aerospace series - Bolts, double hexagon head, close tolerance, medium thread length, in heat resisting nickel base alloy NI-P100HT (Inconel 718), uncoated - Classification: 1 275 MPa/650 °C
This document specifies the dimensions of uncoated double hexagon head bolts, close tolerance, with MJ-thread, medium thread length, in heat-resisting nickel base alloy NI-P100HT for aerospace applications.
Maximum test temperature of the parts is 650 °C.
These bolts are used in aerospace fastening systems mainly stressed in shearing force.
Luft- und Raumfahrt - Zwölfkant-Passschrauben, mittlere Gewindelänge, aus hochwarmfester Nickelbasislegierung NI-P100HT (Inconel 718), blank - Klasse: 1 275 MPa/650 °C
Dieses Dokument legt die Maße von blanken Zwölfkant Passschrauben mit MJ Gewinde mittlerer Gewindelänge aus hochwarmfester Nickelbasislegierung NI P100HT für die Verwendung in der Luft- und Raumfahrt fest.
Die maximale Prüftemperatur der Teile beträgt 650 °C.
Diese Schrauben sind in Verbindungssystemen der Luft- und Raumfahrt zu verwenden, die hauptsächlich auf Scherkraft beansprucht werden.
Série aérospatiale - Vis de précision à tête bihexagonale, filetage moyen, en alliage résistant à chaud base nickel NI-P100HT (Inconel 718), non revêtues - Classification : 1 275 MPa/650 °C
Le présent document spécifie les dimensions des vis de précision à tête bihexagonale, à filetage MJ moyen, en alliage résistant à chaud base nickel NI-P100HT, pour les applications aérospatiales.
La température maximale d'essai des pièces est de 650 °C.
Ces vis sont à utiliser dans les systèmes de fixation aérospatiaux essentiellement soumis à des efforts de cisaillement.
Aeronavtika - Sorniki, dvojna šestroba glava, ozka toleranca, srednja navojna dolžina, iz toplotnoodporne zlitine na nikljevi osnovi NI-P100HT (Inconel 718), brez prevleke - Klasifikacija: 1 275 MPa/650 °C
General Information
- Status
- Not Published
- Publication Date
- 06-Dec-2026
- Technical Committee
- ASD-STAN - Aerospace
- Drafting Committee
- ASD-STAN/D 3/S 2 - Fasteners
- Current Stage
- 4060 - Closure of enquiry - Enquiry
- Start Date
- 04-Sep-2025
- Completion Date
- 04-Sep-2025
Relations
- Effective Date
- 12-Feb-2025
Overview
prEN 3327 is a CEN draft European standard for aerospace fasteners: double hexagon (bihexagonal) head bolts, close tolerance, medium thread length, manufactured from the heat‑resisting nickel‑base alloy NI‑P100HT (Inconel 718), uncoated. The standard defines configuration, dimensions, tolerances and masses for MJ‑threaded bolts used in aerospace assemblies. These parts are classified 1 275 MPa/650 °C and are intended for components with a maximum test temperature of 650 °C, typically loaded primarily in shearing force.
Key topics and requirements
- Bolt geometry and tolerances: Detailed configuration drawing (Figure 1) plus tables of nominal diameters, head and shank dimensions, and mass per 1 000 pieces (Tables 1 & 2). Sizes cover MJ codes (nominal diameters) and length codes for medium thread lengths.
- Thread form: MJ‑thread compliant with aerospace thread standards (ISO 5855 series) and thread lead/runout guidance (ISO 3353‑1).
- Material: Nickel‑base alloy NI‑P100HT (Inconel 718); material conformity referenced to TR 3775 and SAE AMS5662.
- Surface condition: Bolts are uncoated (no surface treatment).
- Marking and designation: Designation format defined (e.g., DOUBLE HEXAGON HEAD BOLT EN 3327 080 050). Marking requirements follow EN 2424 (Style A).
- Technical specification and conformity: Bolts must meet the technical requirements referenced in EN 2583; manufacturer options permitted for unspecified form details.
Practical applications and users
- Applications: High‑temperature aerospace fastening systems - engine mounts, hot‑section assemblies, and other structures where fasteners face elevated temperatures (up to 650 °C) and shear loading.
- Who uses this standard:
- Aerospace design and stress engineers selecting fasteners for elevated‑temperature environments.
- Fastener manufacturers and forgings specialists producing Inconel 718 bolts to aerospace tolerances.
- Procurement and inspection/QC teams ensuring parts meet dimensional, material and marking requirements.
- MRO and certification teams verifying part interchangeability and traceability.
Benefits and keywords
- Benefits: Ensures interchangeability, consistent high‑temperature performance, traceability via standardized marking, and compatibility with aerospace MJ threads.
- Relevant keywords: prEN 3327, double hexagon head bolts, Inconel 718, NI‑P100HT, MJ thread, close tolerance bolts, aerospace fasteners, 650 °C, shear load, SAE AMS5662.
Related standards
- EN 2583 - Technical specification reference
- EN 2424 - Marking of aerospace products
- ISO 5855‑1 / ISO 5855‑2 - MJ threads requirements and dimensions
- ISO 3353‑1 - Lead and runout threads (rolled external)
- ISO 4095 - Bihexagonal drives (wrenching configuration)
- TR 3775 and SAE AMS5662 - Material specifications for Inconel 718
This standard helps manufacturers, designers and quality teams specify and verify high‑temperature, uncoated bihexagon bolts for aerospace applications where consistent dimensions, material integrity and shear performance are critical.
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Frequently Asked Questions
prEN 3327 is a draft published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Bolts, double hexagon head, close tolerance, medium thread length, in heat resisting nickel base alloy NI-P100HT (Inconel 718), uncoated - Classification: 1 275 MPa/650 °C". This standard covers: This document specifies the dimensions of uncoated double hexagon head bolts, close tolerance, with MJ-thread, medium thread length, in heat-resisting nickel base alloy NI-P100HT for aerospace applications. Maximum test temperature of the parts is 650 °C. These bolts are used in aerospace fastening systems mainly stressed in shearing force.
This document specifies the dimensions of uncoated double hexagon head bolts, close tolerance, with MJ-thread, medium thread length, in heat-resisting nickel base alloy NI-P100HT for aerospace applications. Maximum test temperature of the parts is 650 °C. These bolts are used in aerospace fastening systems mainly stressed in shearing force.
prEN 3327 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.
prEN 3327 has the following relationships with other standards: It is inter standard links to EN 3327:2008. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
prEN 3327 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-september-2025
Aeronavtika - Sorniki, dvojna šestroba glava, ozka toleranca, srednja navojna
dolžina, iz toplotnoodporne zlitine na nikljevi osnovi NI-P100HT (Inconel 718), brez
prevleke - Klasifikacija: 1 275 MPa/650 °C
Aerospace series - Bolts, double hexagon head, close tolerance, medium thread length,
in heat resisting nickel base alloy NI-P100HT (Inconel 718), uncoated - Classification: 1
275 MPa/650 °C
Luft- und Raumfahrt - Zwölfkant-Passschrauben, mittlere Gewindelänge, aus
hochwarmfester Nickelbasislegierung NI-P100HT (Inconel 718), blank - Klasse: 1 275
MPa/650 °C
Série aérospatiale - Vis de précision à tête bihexagonale, à filetage moyen, en alliage
résistant à chaud à base de nickel NI-P100HT (Inconel 718), non revêtu - Classification :
1 275 MPa/650 °C
Ta slovenski standard je istoveten z: prEN 3327
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.
DRAFT
EUROPEAN STANDARD
NORME EUROPÉENNE
EUROPÄISCHE NORM
June 2025
ICS 49.030.20 Will supersede EN 3327:2008
English Version
Aerospace series - Bolts, double hexagon head, close
tolerance, medium thread length, in heat resisting nickel
base alloy NI-P100HT (Inconel 718), uncoated -
Classification: 1 275 MPa/650 °C
Série aérospatiale - Vis de précision à tête Luft- und Raumfahrt - Zwölfkant-Passschrauben,
bihexagonale, à filetage moyen, en alliage résistant à mittlere Gewindelänge, aus hochwarmfester
chaud à base de nickel NI-P100HT (Inconel 718), non Nickelbasislegierung NI-P100HT (Inconel 718), blank -
revêtu - Classification : 1 275 MPa/650 °C Klasse: 1 275 MPa/650 °C
This draft European Standard is submitted to CEN members for enquiry. It has been drawn up by the Technical Committee ASD-
STAN.
If this draft becomes a European Standard, 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.
This draft European Standard was established by CEN 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.
Recipients of this draft are invited to submit, with their comments, notification of any relevant patent rights of which they are
aware and to provide supporting documentation.
Warning : This document is not a European Standard. It is distributed for review and comments. It is subject to change without
notice and shall not be referred to as a European Standard.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
CEN-CENELEC Management Centre: Rue de la Science 23, B-1040 Brussels
© 2025 CEN All rights of exploitation in any form and by any means reserved Ref. No. prEN 3327:2025 E
worldwide for CEN national Members.
Contents Page
European foreword . 3
1 Scope . 4
2 Normative references . 4
3 Terms and definitions . 4
4 Required characteristics . 4
4.1 Configuration, dimensions, tolerances, masses . 4
4.2 Material . 10
4.3 Surface treatment . 10
5 Designation . 10
6 Marking . 10
7 Technical specification . 10
European foreword
This document (prEN 3327:2025) has been prepared by 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 document is currently submitted to the CEN Enquiry.
This document will supersede EN 3327:2008.
— 4.2 “Material”: material standard SAE AMS5662 added;
— 4.4 “Thread surface” removed.
1 Scope
This document specifies the dimensions of uncoated double hexagon head bolts, close tolerance, with MJ-
thread, medium thread length, in heat-resisting nickel base alloy NI-P100HT for aerospace applications.
Maximum test temperature of the parts is 650 °C.
These bolts are used in aerospace fastening systems mainly stressed in shearing force.
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 2424, Aerospace series — Marking of aerospace products
EN 2583, Aerospace series — Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601
(Inconel 718) — Classification: 1 275 MPa (at ambient temperature)/650°C — Technical specification
ISO 3353-1, Aerospace — Lead and runout threads — Part 1: Rolled external threads
ISO 4095, Aerospace — Bihexagonal drives — Wrenching configuration — Metric series
ISO 5855-1, Aerospace — MJ threads — Part 1: General requirements
ISO 5855-2, Aerospace — MJ threads — Part 2: Limit dimensions for bolts and nuts
TR 3775, Bolts and pins — Materials
SAE AMS5662, Nickel Alloy, Corrosion- and Heat-Resistant, Bars, Forgings, Rings, and Stock for Forgings
and Rings 52.5Ni — 19Cr — 3.0Mo — 5.1Cb (Nb) — 0.90Ti — 0.50Al — 18Fe Consumable Electrode or
Vacuum Induction Melted 1 775 °F (968 °C) Solution Heat Treated, Precipitation-Hardenable
3 Terms and definitions
No terms and definitions are listed in this document.
ISO and IEC maintain terminology 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/
4 Required characteristics
4.1 Configuration, dimensions, tolerances, masses
Configuration shall be
...




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