Aerospace series - Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980) - Consumable electrode remelted - Not heat treated - Forging stock - a or D ≤ 200 mm

This document specifies the requirements relating to:
Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980)
Consumable electrode remelted
Not heat treated
Forging stock
a or D ≤ 200 mm
for aerospace applications.
W.nr: 1.4980.
ASD-STAN designation: FE-PA2601.

Luft- und Raumfahrt - Hochwarmfeste Legierung X6NiCrTiMoV26-15 (1.4980) - Mit selbstverzehrender Elektrode umgeschmolzen - Nicht wärmebehandelt - Schmiedevormaterial - a oder D ≤ 200 mm

No Scope available

Série aérospatiale - Alliage résistant à chaud X6NiCrTiMoV26-15 (1.4980) - Refondu à l'électrode consommable - Non traité thermiquement - Produits destinés à la forge - a ou D ≤ 200 mm

Le présent document spécifie les exigences relatives à :
Alliage résistant à chaud X6NiCrTiMoV26-15 (1.4980)
Refondu à l'électrode consommable
Non traité thermiquement
Produits destinés à la forge
a ou D ≤ 200 mm
pour les applications aérospatiales.
W.nr : 1.4980.
Désignation ASD-STAN : FE-PA2601.

Aeronavtika - Toplotno odporna zlitina X4NiCrTiMoV26-15 (1.4980) - Toplotno neobdelana - Material za kovanje - a ali D ≤ 200 mm

General Information

Status
Published
Publication Date
16-Dec-2025
Technical Committee
ASD-STAN - Aerospace
Current Stage
6060 - Definitive text made available (DAV) - Publishing
Start Date
17-Dec-2025
Completion Date
17-Dec-2025

Relations

Effective Date
18-Jan-2023

Overview

EN 4317:2025 is a European standard developed by CEN under the ASD-STAN agreement, focusing on the aerospace series of heat-resisting alloys. Specifically, it covers the heat-resisting alloy X6NiCrTiMoV26-15 (1.4980) in the form of consumable electrode remelted forging stock with dimensions a or D ≤ 200 mm that is not heat treated. This standard ensures consistent quality and technical specifications essential for aerospace manufacturing and engineering.

The standard supersedes EN 4317:2007 and harmonizes industry requirements for materials designed for critical aerospace applications where resistance to high temperatures is mandatory. It provides manufacturers and engineers with a comprehensive framework for chemical composition, mechanical properties, and testing methods of this particular alloy.

Key Topics

  • Material Designation: Defines the alloy X6NiCrTiMoV26-15, also known under W.nr 1.4980 and ASD-STAN designation FE-PA2601, tailored for aerospace use.
  • Chemical Composition: Specifies exact ranges for carbon, silicon, manganese, phosphorus, sulfur, aluminum, boron, chromium, molybdenum, nickel, titanium, and vanadium, ensuring consistency and high performance.
  • Manufacturing Process: Covers the consumable electrode remelted method, contributing to impurity reduction and uniform material quality.
  • Forging Stock: Details dimensions limited to a or D ≤ 200 mm, suitable for forging applications in aerospace components.
  • Delivery Condition: The alloy is delivered in a non-heat-treated state, coded as 'U', with specific mechanical property requirements such as proof stress, tensile strength, elongation, and hardness values at ambient and elevated temperatures.
  • Testing and Inspection: Includes mandatory visual (VT), ultrasonic (UT) tests, dimensional and marking inspections, aligned with EN 2860-2 and EN 2043 for product qualification.
  • Heat Treatment References: Notes on solution treatment and precipitation heat treatment processes for potential material conditioning.
  • Standard Compliance: Structured in accordance with EN 4500-003 rules for drafting material standards and aerospace metallic material series (EN 4258).

Applications

The EN 4317:2025 standard applies primarily to the aerospace sector, where materials must withstand extreme temperatures and mechanical stresses without degradation. Typical applications include:

  • Turbine components in jet engines requiring exceptional heat resistance.
  • Structural aerospace forging parts exposed to thermal cycling.
  • High-performance fasteners and fittings where longevity and safety are critical.
  • Components in combustion chambers, exhaust systems, and related high-temperature environments.

This standard provides confidence in product quality, material traceability, and performance consistency, helping aerospace manufacturers deliver reliable, safe, and high-function aerospace parts.

Related Standards

  • EN 2860-2: Technical specifications for heat-resistant alloys forging stock and forgings, referenced extensively for manufacturing guidelines and mechanical testing.
  • EN 2043: General requirements for semi-finished product qualification in aerospace metallic materials, ensuring thorough qualification processes.
  • EN 4258: Outlines the general organization and links between European standards in aerospace metallic materials, providing foundational context for EN 4317:2025.
  • EN 4500-003: Specific rules for drafting and presenting material standards related to heat-resisting alloys, guiding the structure of this document.

Summary

EN 4317:2025 standardizes the technical requirements for heat-resisting alloy X6NiCrTiMoV26-15 (1.4980) used as non-heat-treated forging stock up to 200 mm in diameter for aerospace applications. It ensures high performance under thermal stress, backed by strict composition limits, manufacturing methods, and testing protocols. By complying with this standard, aerospace manufacturers can ensure their components meet rigorous safety and durability criteria essential for advanced aerospace technologies.


Keywords: EN 4317:2025, aerospace heat-resisting alloy, X6NiCrTiMoV26-15, forging stock standard, consumable electrode remelted, aerospace material standards, non heat treated alloy, aerospace forgings, heat resistant alloys, aerospace manufacturing standards, EN 2860-2, aerospace metal qualification

Frequently Asked Questions

EN 4317:2025 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980) - Consumable electrode remelted - Not heat treated - Forging stock - a or D ≤ 200 mm". This standard covers: This document specifies the requirements relating to: Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980) Consumable electrode remelted Not heat treated Forging stock a or D ≤ 200 mm for aerospace applications. W.nr: 1.4980. ASD-STAN designation: FE-PA2601.

This document specifies the requirements relating to: Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980) Consumable electrode remelted Not heat treated Forging stock a or D ≤ 200 mm for aerospace applications. W.nr: 1.4980. ASD-STAN designation: FE-PA2601.

EN 4317:2025 is classified under the following ICS (International Classification for Standards) categories: 49.025.05 - Ferrous alloys in general. The ICS classification helps identify the subject area and facilitates finding related standards.

EN 4317:2025 has the following relationships with other standards: It is inter standard links to EN 4317:2007. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

EN 4317:2025 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-februar-2026
Aeronavtika - Toplotno odporna zlitina X4NiCrTiMoV26-15 (1.4980) - Toplotno
neobdelana - Material za kovanje - a ali D ≤ 200 mm
Aerospace series - Heat-resisting alloy X4NiCrTiMoV26-15 (1.4980) - Non heat treated -
Forging stock - a or D ≤ 200 mm
Luft- und Raumfahrt - Hochwarmfeste Legierung X4NiCrTiMoV26-15 (1.4980) - Nicht
wärmebehandelt - Schmiedevormaterial - a oder D ≤ 200 mm
Série aérospatiale - Alliage résistant à chaud X4NiCrTiMoV26-15 (1.4980) - Non traité
thermiquement - Produits destinés à la forge - a ou D ≤ 200 mm
Ta slovenski standard je istoveten z: EN 4317:2025
ICS:
49.025.05 Železove zlitine na splošno Ferrous alloys in general
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EN 4317
EUROPEAN STANDARD
NORME EUROPÉENNE
December 2025
EUROPÄISCHE NORM
ICS 49.025.05 Supersedes EN 4317:2007
English Version
Aerospace series - Heat-resisting alloy X6NiCrTiMoV26-15
(1.4980) - Consumable electrode remelted - Not heat
treated - Forging stock - a or D  200 mm
Série aérospatiale - Alliage résistant à chaud Luft- und Raumfahrt - Hochwarmfeste Legierung
X6NiCrTiMoV26-15 (1.4980) - Refondu à l'électrode X6NiCrTiMoV26-15 (1.4980) - Mit selbstverzehrender
consommable - Non traité thermiquement - Produits Elektrode umgeschmolzen - Nicht wärmebehandelt -
destinés à la forge - a ou D  200 mm Schmiedevormaterial - a oder D  200 mm
This European Standard was approved by CEN on 26 October 2025.

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, Türkiye 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
© 2025 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4317:2025 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 4317:2025) 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 shall be given the status of a national standard, either by publication of an identical text
or by endorsement, at the latest by June 2026, and conflicting national standards shall be withdrawn at
the latest by June 2026.
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.
This document supersedes EN 4317:2007.
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