Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 150 mm - Rm ≥ 1 400 MPa

This standard specifies the requirements relating to:
Steel FE-PM1505 (X1CrNiMoAlTi12-9-2)
Vacuum induction melted and consumable electrode remelted
Solution treated and precipitation treated
Forgings
a or D ≤ 150 mm
Rm ≥ 1 400 MPa
for aerospace applications.

Luft- und Raumfahrt - Stahl FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vakuuminduktionserschmolzen und mit selbstverzehrender Elektrode umgeschmolzen - Lösungsgeglüht und ausgehägert - Schmiedestücke - a oder D ≤ 150 mm - Rm ≥ 1 400 MPa

Diese Norm legt die Anforderungen an
Stahl FE PM1505 (X1CrNiMoAlTi12-9-2)
Vakuuminduktionserschmolzen und mit selbstverzehrender Elektrode umgeschmolzen
Lösungsgeglüht und ausgehärtet
Schmiedestücke
a oder D  150 mm
Rm ≥ 1 400 MPa
für Anwendungen in der Luft- und Raumfahrt fest.

Série aérospatiale - Acier FE-PM1505 (X1CrNiMoAlTi12-9-2) - 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 ≥ 1 400 MPa

Aeronavtika - Jeklo FE-PM1505 (X1CrNiMoAlTi12-9-2) - Izkovki a ali D ≤ 150 mm - Rm ≥ 1400 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
Effective Date
28-Jan-2026

Overview

EN 4472:2007 is a European standard developed by CEN that specifies the technical requirements for aerospace-grade steel FE-PM1505 (X1CrNiMoAlTi12-9-2). This premium steel grade is characterized by its vacuum induction melting and consumable electrode remelting processes, combined with solution and precipitation heat treatments. The standard focuses on forgings with a thickness or diameter (a or D) up to 150 mm and guarantees a minimum tensile strength (Rm) of 1,400 MPa.

This standard is specifically intended for the aerospace sector, ensuring that materials meet stringent durability, strength, and performance criteria for critical aerospace components.

Key Topics

Steel Grade and Composition

  • Material: Steel FE-PM1505 (X1CrNiMoAlTi12-9-2)
  • Chemical composition limits: Chromium (Cr) ~11.5-12.5%, Molybdenum (Mo) ~1.85-2.15%, Nickel (Ni) ~8.5-9.5%, Aluminum (Al) ~0.6-0.8%, Titanium (Ti) ~0.28-0.37%, with minimal carbon, silicon, and manganese content.
  • The steel is nitrogen-controlled and derived from vacuum induction melting followed by consumable electrode remelting, enhancing purity and mechanical properties.

Manufacturing Process

  • Forgings: The standard applies to forged products manufactured from approved forging stock.
  • Melting method: Vacuum induction melting and consumable electrode remelting to ensure high-quality microstructure.
  • Heat treatment: Includes solution treatment at temperatures between 820 °C and 860 °C, followed by precipitation treatment (aging) at 510 °C to 530 °C for a minimum of 4 hours to achieve required mechanical properties.

Mechanical Properties

  • Tensile strength (Rm): Minimum 1,400 MPa for aerospace applications.
  • Proof stress (Rp0.2): ≥ 1,300 MPa.
  • Elongation (A): ≥ 8-9% depending on test direction.
  • Reduction of area (Z): ≥ 40-50%.
  • Hardness: Between 363 HB (Brinell hardness) maximum in softened conditions to ≥ 400 HB in precipitation-treated condition.
  • Impact strength: Minimum 30-40 Joules with notch sensitivity.

Dimensions and Testing

  • Applicable to forgings with thickness or diameter (a or D) ≤ 150 mm.
  • Test directions include longitudinal (L) and transverse (T), with the option to test either direction depending on forging size.
  • Strict control of grain size, internal and external defects, batch uniformity, dimensional and marking inspections according to related aerospace standards and test protocols.
  • Compliance with related standards for product qualification and acceptance testing.

Applications

EN 4472:2007 steel FE-PM1505 is engineered for critical aerospace components that require exceptional mechanical strength, corrosion resistance, and reliability. Typical aerospace applications include:

  • Structural forgings and components for aircraft engines and airframes.
  • High-performance mechanical parts where fatigue resistance and toughness are vital.
  • Components subjected to high temperature and stress conditions, such as turbine disks and landing gear parts.
  • Aerospace assemblies requiring material consistency, traceability and compliance with international aerospace quality standards.

Related Standards

EN 4472:2007 is part of a wider series of aerospace metallic material standards coordinated under EN 4258. Key related standards include:

  • EN 4258: General organization of aerospace metallic material standards.
  • EN 4346: Steel FE-PM1505 in softened forging stock condition up to 300 mm diameter or thickness.
  • EN 4500-5: Rules for drafting and presenting aerospace metallic material standards, including specific rules for steels.
  • EN 4700-6: Technical specification for aerospace steel and heat-resistant alloy forgings, covering pre-production and production processes.

These standards collectively ensure that aerospace manufacturers and suppliers maintain consistent quality, mechanical properties, and traceability for critical aerospace components.


Keywords: EN 4472:2007, steel FE-PM1505, aerospace steel forgings, vacuum induction melting, consumable electrode remelting, solution treatment, precipitation treatment, aerospace materials standard, high strength steel, tensile strength 1400 MPa, aerospace forgings, European aerospace standards.

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Frequently Asked Questions

EN 4472:2007 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 150 mm - Rm ≥ 1 400 MPa". This standard covers: This standard specifies the requirements relating to: Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) Vacuum induction melted and consumable electrode remelted Solution treated and precipitation treated Forgings a or D ≤ 150 mm Rm ≥ 1 400 MPa for aerospace applications.

This standard specifies the requirements relating to: Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) Vacuum induction melted and consumable electrode remelted Solution treated and precipitation treated Forgings a or D ≤ 150 mm Rm ≥ 1 400 MPa for aerospace applications.

EN 4472:2007 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 4472:2007 has the following relationships with other standards: It is inter standard links to EN 4258:2024, EN 4700-006:2025, EN 4346:2007, EN 4632-004:2012. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

EN 4472:2007 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 4472:2007SIST EN 4472:2009en,de01-maj-2009SIST EN 4472:2009SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 4472
July 2007 ICS 49.025.10 English Version
Aerospace series - Steel FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 150 mm - Rm ≥ 1 400 MPa
Série aérospatiale - Acier FE-PM1505 (X1CrNiMoAlTi12-9-2) - 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 ≥ 1 400 MPa
Luft- und Raumfahrt - Stahl FE-PM1505 (X1CrNiMoAlTi12-9-2) - Vakuuminduktionserschmolzen und mit selbstverzehrender Elektrode umgeschmolzen - Lösungsgeglüht und ausgelagert - Schmiedestücke - a oder D ≤ 150 mm - Rm ≥ 1 400 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 4472:2007: ESIST EN 4472:2009
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