EN 4465:2007
(Main)Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 150 mm - Rm ≥ 1 300 MPa
Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 150 mm - Rm ≥ 1 300 MPa
This standard specifies the requirements relating to:
Steel FE-PM1506 (X5CrNiMoAl13-8-2)
Vacuum induction melted and consumable electrode remelted
Solution treated and precipitation treated
Forgings
a or D ≤ 150 mm
Rm ≥ 1 300 MPa
for aerospace applications.
Luft- und Raumfahrt - Stahl FE-PM1506 (X5CrNiMoAl13-8-2) - Vakuuminduktionserschmolzen und mit selbstverzehrender Elektrode umgeschmolzen - Lösungsgeglüht und ausgelagert - Schmiedestücke - a oder D ≤ 150 mm - Rm ≥ 1 300 MPa
Diese Norm legt die Anforderungen an
Stahl FE PM1506 (X5CrNiMoAl13-8-2)
Vakuuminduktionserschmolzen und
mit selbstverzehrender Elektrode umgeschmolzen
Lösungsgeglüht und ausgehärtet
Schmiedestücke
a oder D ≤ 150 mm
Rm ≥ 1 300 MPa
für Anwendungen in der Luft- und Raumfahrt fest.
Série aérospatiale - Acier FE-PM1506 (X5CrNiMoAl13-8-2) - Élaboré sous vide par induction et refondu à l'électrode consommable - Mis en solution et vieilli - Pièces forgées et pièces matricées - a ou D ≤ 150 mm - Rm ≥ 1 300 MPa
Aeronavtika - Jeklo FE-PM1506 (X5CrNiMoAl13-8-2) - Izkovki a ali D ≤ 150 mm - Rm ≥ 1300 MPa, taljeni z vakuumsko indukcijo in pretaljeni s talilno elektrodo, žarjeni v topilu in utrjeni
General Information
- Status
- Published
- Publication Date
- 10-Jul-2007
- Withdrawal Date
- 30-Jan-2008
- Technical Committee
- ASD-STAN - Aerospace
- Drafting Committee
- ASD-STAN/D 4 - Metallic
- Current Stage
- 9093 - Decision to confirm - Review Enquiry
- Start Date
- 30-Jun-2017
- Completion Date
- 28-Jan-2026
Relations
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
Overview
EN 4465:2007 is a European standard developed by CEN that specifies the technical requirements for Steel FE-PM1506 (X5CrNiMoAl13-8-2), tailored specifically for aerospace applications. This high-performance steel grade is vacuum induction melted and consumable electrode remelted, ensuring superior metallurgical quality and consistency. The material is supplied as forgings with dimensions (a or diameter) up to 150 mm and satisfies a minimum tensile strength (Rm) of 1300 MPa.
This standard ensures that the steel meets stringent aerospace quality and safety criteria through specific heat treatments including solution treatment and precipitation treatment. EN 4465:2007 is part of a wider aerospace metallic materials series, organized under EN 4258, and follows guidelines outlined in EN 4500-5 for steel standard preparation.
Key Topics
- Material Composition: Defines the precise chemical makeup of Steel FE-PM1506, including chromium, nickel, molybdenum, aluminum, and other elemental limits, optimized for aerospace-grade corrosion resistance and mechanical performance.
- Melting and Production Methods:
- Vacuum induction melting to reduce impurities and improve homogeneity.
- Consumable electrode remelting for enhanced steel cleanliness.
- Forgings made from controlled forging stock as per EN 4347.
- Dimensions and Form: Forgings with a thickness or diameter up to 150 mm (a or D ≤ 150 mm).
- Heat Treatment:
- Solution treatment within 830 °C to 930 °C range followed by rapid cooling (oil, air, or water quench).
- Precipitation aging between 530 °C to 550 °C for a minimum of 4 hours to achieve required mechanical properties.
- Mechanical Properties:
- Minimum ultimate tensile strength (Rm) ≥ 1300 MPa.
- Proof stress (Rp0.2) not less than 1200 MPa.
- Specified elongation and reduction of area ensuring good ductility.
- Hardness requirements between 363 HB and 380 HB depending on heat treatment.
- Testing and Inspection:
- Comprehensive evaluation including grain size, external/internal defect inspection, batch uniformity, and dimensional checks in accordance with EN 4700-6.
- Specific test sample orientations for strength and impact resistance.
- Certification: Qualification programmes between manufacturers and purchasers ensure consistent compliance.
Applications
EN 4465 steel Grade FE-PM1506 is designed primarily for aerospace components requiring exceptional strength, corrosion resistance, and structural reliability. Typical applications include:
- Aerospace structural forgings in critical load-bearing parts.
- Engine components subjected to high thermal and mechanical stress.
- Landing gear parts where strength and toughness are critical.
- Safety-critical fasteners and fittings needing superior fatigue resistance.
- High-performance aerospace assemblies demanding uniform material properties and traceability.
The material’s qualification under this standard guarantees its suitability for demanding environments encountered in aerospace and defense sectors.
Related Standards
- EN 4258: General organization of aerospace metallic material standards, providing a framework linking EN 4465 to other material specifications.
- EN 4347: Details specifications for similar steel forging stocks with larger dimensions.
- EN 4500-5: Rules for drafting and presenting steel material standards consistently.
- EN 4700-6: Technical specifications including pre-production and production forging guidelines aligned with EN 4465 requirements.
Conclusion
EN 4465:2007 provides a comprehensive and rigorous framework ensuring the quality, performance, and reliability of Steel FE-PM1506 forgings for aerospace use. Manufacturers and suppliers adhering to this standard deliver high-strength, precisely heat-treated, and defect-controlled steel components critical for modern aerospace engineering challenges. This standard is essential for aerospace engineers, metallurgists, and quality assurance professionals focusing on advanced steel materials for safety-critical aerospace applications.
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Frequently Asked Questions
EN 4465:2007 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 150 mm - Rm ≥ 1 300 MPa". This standard covers: This standard specifies the requirements relating to: Steel FE-PM1506 (X5CrNiMoAl13-8-2) Vacuum induction melted and consumable electrode remelted Solution treated and precipitation treated Forgings a or D ≤ 150 mm Rm ≥ 1 300 MPa for aerospace applications.
This standard specifies the requirements relating to: Steel FE-PM1506 (X5CrNiMoAl13-8-2) Vacuum induction melted and consumable electrode remelted Solution treated and precipitation treated Forgings a or D ≤ 150 mm Rm ≥ 1 300 MPa for aerospace applications.
EN 4465:2007 is classified under the following ICS (International Classification for Standards) categories: 49.025.10 - Steels. The ICS classification helps identify the subject area and facilitates finding related standards.
EN 4465:2007 has the following relationships with other standards: It is inter standard links to EN 4247:2005, EN 4258:2024, EN 4700-006:2025. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
EN 4465:2007 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.03D49.025.10JeklaSteelsICS:Ta slovenski standard je istoveten z:EN 4465:2007SIST EN 4465:2009en,de01-maj-2009SIST EN 4465:2009SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 4465
July 2007 ICS 49.025.10 English Version
Aerospace series - Steel FE-PM1506 (X5CrNiMoAl13-8-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 150 mm - Rm ≥ 1 300 MPa
Série aérospatiale - Acier FE-PM1506 (X5CrNiMoAl13-8-2) - Élaboré sous vide par induction et refondu à l'électrode consommable - Mis en solution et vieilli - Pièces forgées et pièces matricées - a ou D ≤ 150 mm - Rm ≥ 1 300 MPa
Luft- und Raumfahrt - Stahl FE-PM1506 (X5CrNiMoAl13-8-2) - Vakuuminduktionserschmolzen und mit selbstverzehrender Elektrode umgeschmolzen - Lösungsgeglüht und ausgelagert - Schmiedestücke - a oder D ≤ 150 mm - Rm ≥ 1 300 MPa This European Standard was approved by CEN on 15 February 2007.
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 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 Management Centre has the same status as the official versions.
CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre: rue de Stassart, 36
B-1050 Brussels © 2007 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4465:2007: ESIST EN 4465:2009
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