Aerospace series - Steel X4CrNiMo16-5-1 - Air melted - Hardened and tempered - Sheets and plates - 0,3 mm ≤ a ≤ 50 mm - 900 MPa ≤ Rm ≤ 1 050 MPa

This European Standard specifies the requirements relating to:
Steel X4CrNiMo16-5-1
Air melted
Hardened and tempered
Sheets and plates
0,3 mm ≤ a ≤ 50 mm
900 MPa ≤ Rm ≤ 1 050 MPa
for aerospace applications.
ASD-STAN designation: FE-PM 3504.

Luft- und Raumfahrt - Stahl X4CrNiMo16-5-1 - Lufterschmolzen - Gehärtet- und angelassen - Bleche und Platten - 0,3 mm ≤ a ≤ 50 mm - 900 MPa ≤ Rm ≤ 1 050 MPa

Diese Europäische Norm legt die Anforderungen an:
Stahl X4CrNiMo16 5 1
Lufterschmolzen
Gehärtet und angelassen
Bleche und Platten
0,3 mm ≤ a ≤ 50 mm
900 MPa ≤ Rm ≤ 1 050 MPa
für Anwendungen in der Luft- und Raumfahrt fest.
ASD STAN-Werkstoffbezeichnung: FE PM 3504.

Série aérospatiale - Acier X4CrNiMo16-5-1 - Élaboré à l'air - Trempé et revenu - Tôles et plaques - 0,3 mm ≤ a ≤ 50 mm - 900 MPa ≤ Rm ≤ 1 050 MPa

Le présent document spécifie les exigences relatives à :
Acier X4CrNiMo16-5-1
Élaboré à l’air
Trempé et revenu
Tôles et plaques
0,3 mm ≤ a ≤ 50 mm
900 MPa ≤ Rm ≤ 1 050 MPa
pour les applications aérospatiales.
Désignation ASD-STAN : FE-PM 3504.

Aeronavtika - Jeklo X4CrNiMo16-5-1 - Taljeno na zraku - Utrjeno in mehko žarjeno - Pločevina in plošče - 0,3 mm ≤ a ≤ 50 mm - 900 MPa ≤ Rm ≤ 1050 MPa

Ta evropski standard določa zahteve za:
jeklo X4CrNiMo16-5-1,
taljeno na zraku,
utrjeno in mehko žarjeno,
pločevino in plošče,
0,3 mm ≤ a ≤ 50 mm,
900 MPa ≤ Rm ≤ 1050 MPa
za uporabo v aeronavtiki.
Oznaka ASD-STAN: FE-PM 3504.

General Information

Status
Published
Public Enquiry End Date
31-Jul-2020
Publication Date
07-Jun-2022
Technical Committee
I13 - Imaginarni 13
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
25-May-2022
Due Date
30-Jul-2022
Completion Date
08-Jun-2022

Relations

Effective Date
26-Feb-2023

Overview

EN 4890:2022 is a CEN (ASD‑STAN) aerospace series standard that specifies requirements for Steel X4CrNiMo16‑5‑1 in sheet and plate form. The standard covers air‑melted, hot‑rolled, hardened and tempered material with thicknesses from 0.3 mm to 50 mm and tensile strength Rm between 900 MPa and 1 050 MPa. ASD‑STAN designation: FE‑PM 3504. EN 4890:2022 was approved by CEN on 13 March 2022 and is intended specifically for aerospace applications.

Key topics and technical requirements

  • Material and melting: Steel designation X4CrNiMo16‑5‑1, produced by air melting and hot rolling (sheets and plates).
  • Chemical composition (typical limits per the standard):
    • C ≤ 0.06 %, Si ≤ 0.70 %, Mn ≤ 1.50 %, P ≤ 0.040 %, S ≤ 0.015 %
    • N 0.02–0.08 %, Cr 15.00–17.00 %, Mo 0.80–1.50 %, Ni 4.00–6.00 %
  • Heat treatment / delivery conditions:
    • Delivered softened or hardened and tempered.
    • Typical austenitizing: 1010 °C – 1060 °C (AC/AQ/OQ/PQ); tempering 580 °C – 650 °C, or by agreement between manufacturer and purchaser.
  • Mechanical property targets:
    • Tensile strength Rm: 900–1 050 MPa.
    • Proof stress Rp0.2: ≥700 MPa for defined thickness ranges.
    • Hardness: softened condition ≤255 HB; hardened and tempered typically 280–320 HV.
    • Impact energy: specified minima (e.g., ≥120 J at 20 °C and ≥70 J at −40 °C for thicker sections where applicable).
  • Metallurgical and quality limits:
    • δ‑ferrite content ≤ 5 %
    • Grain size: G ≥ 5 (per EN 4700‑001)
    • Inclusion, visual and dimensional inspections and ultrasonic testing as referenced.
  • Test and inspection references: normative references include EN 4700‑001, EN 2951, and EN 4050‑4.

Applications and users

Practical applications focus on aerospace components that require high strength and reliable toughness in sheet/plate form. Typical users:

  • Aircraft and aerospace manufacturers (material selection and procurement)
  • Suppliers of aerospace-grade steel sheets and plates
  • Design and structural engineers specifying materials for load‑bearing parts
  • Quality, inspection and testing personnel ensuring compliance with aerospace material standards
  • Contractors and maintenance organisations that source certified materials

Keywords for search: EN 4890:2022, X4CrNiMo16‑5‑1, aerospace steel, hardened and tempered, air melted, sheets and plates, 900–1050 MPa.

Related standards

  • EN 4700‑001 - Steel and heat resisting alloys - Wrought products - Technical specification (plate, sheet, strip)
  • EN 2951 - Micrographic determination of non‑metallic inclusions
  • EN 4050‑4 - Ultrasonic inspection acceptance criteria
  • EN 4258, EN 4500‑005 - organizational and drafting rules for aerospace metallic material standards

For procurement or design, reference EN 4890:2022 alongside the cited normative documents to ensure full compliance with aerospace material and inspection requirements.

Frequently Asked Questions

SIST EN 4890:2022 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Steel X4CrNiMo16-5-1 - Air melted - Hardened and tempered - Sheets and plates - 0,3 mm ≤ a ≤ 50 mm - 900 MPa ≤ Rm ≤ 1 050 MPa". This standard covers: This European Standard specifies the requirements relating to: Steel X4CrNiMo16-5-1 Air melted Hardened and tempered Sheets and plates 0,3 mm ≤ a ≤ 50 mm 900 MPa ≤ Rm ≤ 1 050 MPa for aerospace applications. ASD-STAN designation: FE-PM 3504.

This European Standard specifies the requirements relating to: Steel X4CrNiMo16-5-1 Air melted Hardened and tempered Sheets and plates 0,3 mm ≤ a ≤ 50 mm 900 MPa ≤ Rm ≤ 1 050 MPa for aerospace applications. ASD-STAN designation: FE-PM 3504.

SIST EN 4890:2022 is classified under the following ICS (International Classification for Standards) categories: 49.025.10 - Steels; 77.140.50 - Flat steel products and semi-products. The ICS classification helps identify the subject area and facilitates finding related standards.

SIST EN 4890:2022 has the following relationships with other standards: It is inter standard links to SIST EN 4890:2022/A1:2024. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

You can purchase SIST EN 4890:2022 directly from iTeh Standards. The document is available in PDF format and is delivered instantly after payment. Add the standard to your cart and complete the secure checkout process. iTeh Standards is an authorized distributor of SIST standards.

Standards Content (Sample)


SLOVENSKI STANDARD
01-julij-2022
Aeronavtika - Jeklo X4CrNiMo16-5-1 - Taljeno na zraku - Utrjeno in mehko žarjeno -
Pločevina in plošče - 0,3 mm ≤ a ≤ 50 mm - 900 MPa ≤ Rm ≤ 1050 MPa
Aerospace series - Steel X4CrNiMo16-5-1 - Air melted - Hardened and tempered -
Sheets and plates - 0,3 mm ≤ a ≤ 50 mm - 900 MPa ≤ Rm ≤ 1 050 MPa
Luft- und Raumfahrt - Stahl X4CrNiMo16-5-1 - Lufterschmolzen - Gehärtet- und
angelassen - Bleche und Platten - 0,3 mm ≤ a ≤ 50 mm - 900 MPa ≤ Rm ≤ 1 050 MPa
Série aérospatiale - Acier X4CrNiMo16-5-1 - Élaboré à l'air - Trempé et revenu - Tôles et
plaques - 0,3 mm ≤ a ≤ 50 mm - 900 MPa ≤ Rm ≤ 1 050 MPa
Ta slovenski standard je istoveten z: EN 4890:2022
ICS:
49.025.10 Jekla Steels
77.140.50 Ploščati jekleni izdelki in Flat steel products and semi-
polizdelki products
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EN 4890
EUROPEAN STANDARD
NORME EUROPÉENNE
May 2022
EUROPÄISCHE NORM
ICS 49.025.10
English Version
Aerospace series - Steel X4CrNiMo16-5-1 - Air melted -
Hardened and tempered - Sheets and plates - 0,3 mm  a 
50 mm - 900 MPa  Rm  1 050 MPa
Série aérospatiale - Acier X4CrNiMo16-5-1 - Élaboré à Luft- und Raumfahrt - Stahl X4CrNiMo16-5-1 -
l'air - Trempé et revenu - Tôles et plaques - 0,3 mm Lufterschmolzen - Gehärtet- und angelassen - Bleche
 a  50 mm - 900 MPa  Rm  1 050 MPa und Platten - 0,3 mm  a  50 mm - 900 MPa  Rm 
1 050 MPa
This European Standard was approved by CEN on 13 March 2022.

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, 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, Turkey and
United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
C O M I T É E U R O P É E N D E N O R M A L I S A T I O N

E U R O P Ä I S C H E S K O M I T E E F Ü R N O R M U N G

CEN-CENELEC Management Centre: Rue de la Science 23, B-1040 Brussels
© 2022 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4890:2022 E
worldwide for CEN national Members.

Contents Page
European foreword . 3
Introduction . 4
1 Scope . 5
2 Normative references . 5
3 Terms and definitions . 5
4 Requirements . 5
Bibliography . 9

European foreword
This document (EN 4890:2022) 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 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 shall be given the status of a national standard, either by publication of an identical text
or by endorsement, at the latest by November 2022, and conflicting national standards shall be
withdrawn at the latest by November 2022.
Attention is drawn to the possibility that some of the elements of this document may be the subject of
patent rights. CEN 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 document: Austria, Belgium, Bulgaria, Croatia, Cyprus,
Czech Repu
...

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