SIST EN 2816:2019
(Main)Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 200 mm - Rm ≥ 965 MPa
Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 200 mm - Rm ≥ 965 MPa
This document specifies the requirements relating to:
Steel FE-PM1802 (X5CrNiCu15-5)
Consumable electrode remelted
Solution treated and precipitation treated
Forgings
a or D ≤ 200 mm
Rm ≥ 965 MPa
Luft- und Raumfahrt - Stahl FE-PM1802 (X5CrNiCu15-5) - Mit selbstverzehrender Elektrode umgeschmolzen - Lösungsgeglüht und ausgelagert - Schmiedestücke - a oder D ≤ 200 mm - Rm ≥ 965 MPa
Dieses Dokument legt die Anforderungen an
Stahl FE-PM1802 (X5CrNiCu15-5)
mit selbstverzehrender Elektrode umgeschmolzen,
lösungsgeglüht und ausgehärtet,
Schmiedestücke
a oder D ≤ 200 mm,
Rm ≥ 965 MPa,
für Anwendungen in der Luft- und Raumfahrt fest.
Série aérospatiale - Acier FE-PM1802 (X5CrNiCu15-5) - Refondu à l'électrode consommable - Mis en solution et vieilli - Pièces forgées et pièces matricées - a ou D ≤ 200 mm - Rm ≥ 965 MPa
Cette présente Norme européenne spécifie les exigences relatives à :
Acier FE-PM1802 (X5CrNiCu15-5)
Refondu à l'électrode consommable
Mis en solution et précipité
Pièces forgées ou matricées
a ou D ≤ 200 mm
Rm ≥ 965 MPa
pour applications aérospatiales.
Aeronavtika - Jeklo FE-PM1802 (X5CrNiCu15-5) - Pretaljeno s taljivo elektrodo - Topilno žarjena in izločevalno utrjena - Izkovki - a ali D ≤ 200 mm - Rm ≥ 965 MPa
Ta dokument določa zahteve, ki se navezujejo na: jeklo FE-PM1802 (X5CrNiCu15-5) – pretaljeno s taljivo elektrodo – topilno žarjeno in izločevalno utrjeno – izkovke – a ali D ≤ 200 mm Rm ≥ 965 MPa
General Information
- Status
- Published
- Publication Date
- 08-Oct-2019
- Technical Committee
- I13 - Imaginarni 13
- Current Stage
- 6060 - National Implementation/Publication (Adopted Project)
- Start Date
- 04-Oct-2019
- Due Date
- 09-Dec-2019
- Completion Date
- 09-Oct-2019
Overview
SIST EN 2816:2019 is a European standard issued by CEN that specifies the technical requirements for aerospace-grade Steel FE-PM1802, also known as X5CrNiCu15-5. This steel is characterized by its consumable electrode remelted production, solution treatment, and precipitation treatment processes. The standard covers forgings with dimensions up to 200 mm in thickness or diameter (a or D ≤ 200 mm) and ensures a minimum ultimate tensile strength (Rm) of 965 MPa. It is part of the EN metallic materials series designed specifically for aerospace applications, providing consistent quality and performance for critical aerospace components.
Key Topics
- Material Composition: Steel FE-PM1802 (X5CrNiCu15-5) is defined with strict chemical composition limits, including:
- Chromium (Cr): 14.0% - 15.5%
- Nickel (Ni): 3.5% - 5.5%
- Copper (Cu): 2.5% - 4.5%
- Carbon (C): Max 0.07%
- Silicon (Si) and Manganese (Mn): Up to 1.0%
- Other alloying elements such as Niobium + Tantalum (Nb + Ta) up to 0.45%
- Manufacturing Process:
- Steel is remelted using a consumable electrode technique for purity.
- Forgings are produced from specified forging stock as per EN 3364.
- Heat Treatment:
- Solution treatment at 1025°C to 1055°C for at least 30 minutes.
- Followed by precipitation treatment between 580°C and 610°C for a minimum of 4 hours.
- Air cooling or oil quenching applied to achieve required microstructure and mechanical properties.
- Mechanical Properties:
- Minimum tensile strength (Rm) of 965 MPa.
- Yield strength (Rp0.2) of at least 790 MPa.
- Elongation between 9% and 12%.
- Hardness limited to between 302 and 363 HV.
- Impact strength withnotch (KV) ≥ 100 J in transverse (T) direction.
- Dimensions: Forgings up to 200 mm in thickness or diameter are specified, ensuring suitability for medium-sized aerospace components.
- Quality and Inspection:
- Compliance with EN 2157-3 for forging specifications.
- Inspection includes dimensional, marking, and batch uniformity verification.
- Grain size and external discontinuities are controlled as per referenced standards.
Applications
SIST EN 2816:2019 steel is tailored for applications within the aerospace industry where high strength, corrosion resistance, and reliability are critical. Typical use cases include:
- Structural aerospace components requiring excellent fatigue resistance and high tensile strength.
- Critical forgings for aircraft engine parts, landing gear components, and airframe assemblies.
- Precision aerospace forgings up to 200 mm thickness or diameter where mechanical performance must meet strict regulatory standards.
- Components that require advanced heat treatment to achieve enhanced mechanical properties and durability under operational stress.
This standard supports manufacturers and suppliers in producing consistent, certified materials that comply with international aerospace quality expectations.
Related Standards
- EN 3364 – Covers the technical specifications for steel FE-PM1802 forging stock, applicable for initial stock materials.
- EN 2157-3 – Addresses requirements for pre-production and production forgings, including testing and inspection methods used in conjunction with EN 2816.
- EN 4258 – Provides general guidance on the organization of aerospace metallic material standards, framing how EN 2816 fits within the broader aerospace materials standardization.
- EN 4500-005 – Sets the drafting rules for aerospace steel materials standards, ensuring consistency in presentation and technical requirements.
Summary
SIST EN 2816:2019 is an essential standard for aerospace manufacturers and suppliers dealing with Steel FE-PM1802 (X5CrNiCu15-5) forgings. By specifying precise chemical composition, heat treatment, mechanical properties, and dimensional criteria, it ensures the steel’s suitability for demanding aerospace applications. Compliance with this standard guarantees high-performance forgings with superior strength and reliability, crucial for the safety and efficiency of aerospace systems.
Keywords: SIST EN 2816:2019, aerospace steel standard, FE-PM1802, X5CrNiCu15-5, consumable electrode remelted steel, solution treated steel, precipitation treated steel, aerospace forgings, mechanical properties, CEN standards, aerospace materials specification.
Frequently Asked Questions
SIST EN 2816:2019 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D ≤ 200 mm - Rm ≥ 965 MPa". This standard covers: This document specifies the requirements relating to: Steel FE-PM1802 (X5CrNiCu15-5) Consumable electrode remelted Solution treated and precipitation treated Forgings a or D ≤ 200 mm Rm ≥ 965 MPa
This document specifies the requirements relating to: Steel FE-PM1802 (X5CrNiCu15-5) Consumable electrode remelted Solution treated and precipitation treated Forgings a or D ≤ 200 mm Rm ≥ 965 MPa
SIST EN 2816:2019 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.
SIST EN 2816:2019 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-december-2019
Aeronavtika - Jeklo FE-PM1802 (X5CrNiCu15-5) - Pretaljeno s taljivo elektrodo -
Topilno žarjena in izločevalno utrjena - Izkovki - a ali D ≤ 200 mm - Rm ≥ 965 MPa
Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted
- Solution treated and precipitation treated - Forgings - a or D ≤ 200 mm - Rm ≥ 965 MPa
Luft- und Raumfahrt - Stahl FE-PM1802 (X5CrNiCu15-5) - Mit selbstverzehrender
Elektrode umgeschmolzen - Lösungsgeglüht und ausgelagert - Schmiedestücke - a oder
D ≤ 200 mm - Rm ≥ 965 MPa
Série aérospatiale - Acier FE-PM1802 (X5CrNiCu15-5) - Refondu à l'électrode
consommable - Mis en solution et vieilli - Pièces forgées et pièces matricées - a ou D ≤
200 mm - Rm ≥ 965 MPa
Ta slovenski standard je istoveten z: EN 2816:2019
ICS:
49.025.10 Jekla Steels
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EN 2816
EUROPEAN STANDARD
NORME EUROPÉENNE
September 2019
EUROPÄISCHE NORM
ICS 49.025.10
English Version
Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) -
Consumable electrode remelted - Solution treated and
precipitation treated - Forgings - a or D ≤ 200 mm - Rm ≥
965 MPa
Série aérospatiale - Acier FE-PM1802 (X5CrNiCu15-5) - Luft- und Raumfahrt - Stahl FE-PM1802 (X5CrNiCu15-
Refondu à l'électrode consommable - Mis en solution et 5) - Mit selbstverzehrender Elektrode umgeschmolzen
- Lösungsgeglüht und ausgelagert - Schmiedestücke - a
vieilli - Pièces forgées et pièces matricées - a ou D ≤
oder D ≤ 200 mm - Rm ≥ 965 MPa
200 mm - Rm ≥ 965 MPa
This European Standard was approved by CEN on 30 December 2018.
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
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
CEN-CENELEC Management Centre: Rue de la Science 23, B-1040 Brussels
© 2019 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 2816:2019 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 2816:2019) 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 Standard has
received the approval of the National Associations and the Official Services of the member countries of
ASD, prior to its presentation to CEN.
This European Standard shall be given the status of a national standard, either by publication of an
identical text or by endorsement, at the latest by March 2020, and conflicting national standards shall be
withdrawn at the latest by March 2020.
Attention is drawn to the possibility that some of the elements of this document may be the subject of
patent rig
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