SIST EN 4800-002:2025
(Main)Aerospace series - Titanium and titanium alloys - Technical specification - Part 002: Bar and section
Aerospace series - Titanium and titanium alloys - Technical specification - Part 002: Bar and section
This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy bars and sections. It is applicable when referred to and in conjunction with the European material standard unless otherwise specified on the drawing, order or inspection schedule.
Luft- und Raumfahrt - Titan und Titanlegierungen - Technische Lieferbedingungen - Teil 002: Stangen und Profile
Série aérospatiale - Titane et alliages de titane - Spécification technique - Partie 002 : Barres et profilés
Le présent document spécifie les exigences relatives aux commandes, à la fabrication, aux essais, au contrôle et à la livraison des barres et profilés en titane et alliages de titane. Il doit être appliqué lorsqu'il est cité en référence et conjointement avec la norme de matériau EN, sauf spécification contraire figurant sur le dessin, la commande ou la fiche d'essais.
Aeronavtika - Titan in titanove zlitine - Tehnična specifikacija - 002. del: Palice in profili
General Information
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Standards Content (Sample)
SLOVENSKI STANDARD
01-april-2025
Aeronavtika - Titan in titanove zlitine - Tehnična specifikacija - 002. del: Palice in
profili
Aerospace series - Titanium and titanium alloys - Technical specification - Part 002: Bar
and section
Luft- und Raumfahrt - Titan und Titanlegierungen - Technische Lieferbedingungen - Teil
002: Stangen und Profile
Série aérospatiale - Titane et alliages de titane - Spécification technique - Partie 002 :
Barres et profilés
Ta slovenski standard je istoveten z: EN 4800-002:2025
ICS:
49.025.30 Titan Titanium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EN 4800-002
EUROPEAN STANDARD
NORME EUROPÉENNE
February 2025
EUROPÄISCHE NORM
ICS 49.025.30 Supersedes EN 4800-002:2010
English Version
Aerospace series - Titanium and titanium alloys - Part 002:
Bars and sections - Technical specification
Série aérospatiale - Titane et alliages de titane - Partie Luft- und Raumfahrt - Titan und Titanlegierungen -
002 : Barres et profilés - Spécification technique Teil 002: Stangen und Profile - Technische
Lieferbedingungen
This European Standard was approved by CEN on 25 November 2024.
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 4800-002:2025 E
worldwide for CEN national Members.
Contents Page
European foreword . 3
Introduction . 4
1 Scope . 5
2 Normative references . 5
3 Terms and definitions . 6
4 Wording of order . 7
5 Health and safety . 7
6 Technical requirements . 7
6.1 General. 7
6.2 Qualification requirements . 8
6.3 Release requirements . 8
6.3.1 Release tests . 8
6.3.2 Retests . 8
6.3.3 Rejection . 8
6.3.4 Special tests . 9
6.3.5 Capability clause . 9
6.3.6 Statistical process control. 9
6.3.7 Inspection and test report . 9
6.4 Traceability . 9
Bibliography . 35
European foreword
This document (EN 4800-002:2025) 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 August 2025, and conflicting national standards shall be withdrawn
at the latest by August 2025.
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 4800-002:2010.
The main changes with respect to the previous edition are as follows:
— EN 4800-002:2010-11:
o editorial improvements;
o update of Clause 2;
o update of the paragraph “Method of melting” in Table 1; and
o addition of a bibliography.
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 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 the
United Kingdom.
Introduction
This document is part of the series of EN metallic material standards for aerospace applications.
The general organization of this series is described in EN 4258.
1 Scope
This document specifies the requirements for the ordering, manufacture, testing, inspection and
delivery of titanium and titanium alloy bars and sections. It is applicable when referred to and in
conjunction with the European material standard unless otherwise specified on the drawing, order or
inspection schedule.
2 Normative references
The following documents are referred to in the text in such a way that some or all of their content
constitutes requirements of this document. For dated references, only the edition cited applies. For
undated references, the latest edition of the referenced document (including any amendments) applies.
EN 2002-001, Aerospace series — Metallic materials — Test methods — Part 001: Tensile testing at
ambient temperature
EN 2002-002, Aerospace series — Metallic materials — Test methods — Part 002: Tensile testing at
elevated temperature
EN 2002-005, Aerospace series — Test methods for metallic materials — Part 005: Uninterrupted creep
and stress-rupture testing
EN 2002-16, Aerospace series — Metallic materials — Test methods — Part 16: Non-destructive
testing — Penetrant testing
EN 2003-009, Aerospace series — Test methods — Titanium and titanium alloys — Part 009:
Determination of surface contamination
EN 2032-001, Aerospace series — Metallic materials — Part 001: Conventional designation
EN 2032-2, Aerospace series — Metallic materials — Part 2: Coding of metallurgical condition in delivery
condition
EN 2078, Aerospace series — Metallic materials — Manufacturing schedule, inspection schedule,
inspection and test report — Definition, general principles, preparation and approval
EN 2954-002, Aerospace series — Macrostructure of titanium and titanium alloy wrought products —
Part 002: Macrostructure of bar, section, forging stock and forgings
EN 2955, Aerospace series — Recycling of titanium and titanium alloy scrap
EN 3114-001, Aerospace series — Test method — Microstructure of (α + β) titanium alloy wrought
products — Part 001: General requirements
EN 3114-002, Aerospace series — Test method — Microstructure of (α + β) titanium alloy wrought
products — Part 002: Microstructure of bars, sections, forging stock and forgings
EN 3238, Aerospace series — Metallic materials — Test method — Shear test for wires and rivets
EN 3684, Aerospace series — Test methods — Titanium alloy wrought products — Determination of
β transus temperature — Metallographic method
Published as ASD-STAN prEN at the date of publication of this document, available at:
https://www.asd-stan.org/.
EN 3874, Aerospace series — Test methods for metallic materials — Constant amplitude force-controlled
low cycle fatigue testing
EN 3976, Aerospace series — Titanium and titanium alloys — Test method — Chemical analysis for the
determination of hydrogen content
EN 3987, Aerospace series — Test methods for metallic materials — Constant amplitude force-controlled
high cycle fatigue testing
EN 3988, Aerospace series — Test methods for metallic materials — Constant amplitude strain-
controlled low cycle fatigue testing
EN 4050-1, Aerospace series — Test method for metallic materials — Ultrasonic inspection of bars, plates,
forging stock and forgings — Part 1: General requirements
EN 4050-4, Aerospace series — Test method for metallic materials — Ultrasonic inspection of bars, plates,
forging stock and forgings — Part 4: Acceptance criteria
EN 4259, Aerospace series — Metallic materials — Definition of general terms
EN ISO 643, Steels — Micrographic determination of the apparent grain size (ISO 643)
EN ISO 21920-3, Geometrical product specifications (GPS) — Surface texture: Profile — Part 3:
Specification operators (ISO 21920-3)
Aerospace series — Metallic materials — Relationship between dimensional standards and
TR 2410,
material standards
AMS 2750, Pyrometry
3 Terms and definitions
For the purposes of this document, the terms and definitions given in EN 4259 apply.
ISO and IEC maintain terminological databases for use in standardization at the following addresses:
— ISO Online browsing platform: available at https://www.iso.org/obp
— IEC Electropedia: available at https://www.electropedia.org/
Published as ASD-STAN TR, available at: https://www.asd-stan.org/.
Published by Society of Automotive Engineers (SAE), available at: https://www.sae.org/.
4 Wording of order
The order shall clearly indicate:
a) quantities to be supplied;
b) dates of delivery;
c) material standard number;
d) delivery condition and metallurgical code of products;
e) dimensions and tolerances or reference to an appropriate dimensional standard;
f) product designation, when required;
g) forwarding address;
h) nature and type of packing, if required;
i) definition and frequency of any special tests and their retest procedures, if required.
5 Health and safety
a) The products in the delivery condition shall fulfil the current health and safety laws of the area of
the country when and where it is to be delivered.
b) A product safety data sheet shall be available.
6 Technical requirements
6.1 General
a) The product shall be manufactured in accordance with the requirements of the relevant material
standard and the applicable requirements of this document.
b) A manufacturing schedule shall be established and applied in accordance with EN 2078.
c) The product shall satisfy the requirements of the material standard and/or order and shall be free
from irregularities prejudicial to the subsequent manufacture or use of this product.
d) Notwithstanding previous acceptance complying with this material standard, any product that is
found, at a later stage, to contain such defects shall be rejected.
e) Unless otherwise specified, the requirements in Table 1 and Table 2 shall apply in conjunction with
those of the relevant material standard. Table 1 relates to lines 1 to 29 (inclusive) of the material
standard and Table 2 relates to lines 30 onwards in which the sub-line format is also used. Lines 2 to
98 may also be opened in line 100 if the material standard details specific qualification requirements.
f) If a specific line number is not shown in Table 1 and Table 2, the requirement is stated in the
material standard and/or order.
g) The requirements of the order and/or material standard shall override the requirements
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