EN 4800-001:2010

SLOVENSKI STANDARD
01-november-2011
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Aerospace series - Titanium and titanium alloys - Technical specification - Part 001:
Plate, sheet and strip
Luft- und Raumfahrt - Titan und Titanlegierungen Kneterzeugnisse - Technische
Lieferbedingungen - Teil 001: Platten, Bleche und Bänder
Série aérospatiale - Titane et alliages de titane - Spécification technique - Partie 001:
Plaques, tôles et bandes
Ta slovenski standard je istoveten z: EN 4800-001:2010
ICS:
49.025.30 Titan Titanium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD
EN 4800-001
NORME EUROPÉENNE
EUROPÄISCHE NORM
November 2010
ICS 49.025.30
English Version
Aerospace series - Titanium and titanium alloys - Technical
specification - Part 001: Plate, sheet and strip
Série aérospatiale - Titane et alliages de titane - Luft- und Raumfahrt - Titan und Titanlegierungen
Spécification technique - Partie 001: Plaques, tôles et Kneterzeugnisse - Technische Lieferbedingungen - Teil
bandes 001: Platten, Bleche und Bänder
This European Standard was approved by CEN on 20 February 2010.

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, Croatia, 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: Avenue Marnix 17, B-1000 Brussels
© 2010 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4800-001:2010: E
worldwide for CEN national Members.

Contents Page
Foreword .3
Introduction .4
1 Scope .5
2 Normative references .5
3 Terms and definitions .7
4 Wording of order .7
5 Health and safety .7
6 Technical requirements .7
Foreword
This document (EN 4800-001:2010) 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 May 2011, and conflicting national standards shall be withdrawn at the
latest by May 2011.
Attention is drawn to the possibility that some of the elements of this document may be the subject of patent
rights. CEN [and/or CENELEC] 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 European Standard: 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, Romania, Slovakia, Slovenia, Spain,
Sweden, Switzerland and the United Kingdom.
Introduction
This standard 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 standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of
titanium and titanium alloy plate, sheet and strip. It shall be applied when referred to and in conjunction with
the EN material standard unless otherwise specified on the drawing, order or inspection schedule.
2 Normative references
The following referenced documents are indispensable for the application 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
1)
EN 2002-6, Aerospace series — Test methods for metallic materials — Part 6: Bend testing
EN 2003-009, Aerospace series — Test methods — Titanium and titanium alloys — Part 009: Determination
of surface contamination
EN 2032-1, Aerospace series — Metallic materials — Part 1: 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 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 3114-003, Aerospace series — Test method — Microstructure of (α + β) titanium alloy wrought products —
Part 003: Microstructure of plate
EN 3114-004, Aerospace series — Test method — Microstructure of (α + β) titanium alloy wrought products —
Part 004: Microstructure of sheet for superplastic forming
EN 3683, Aerospace series — Test methods — Titanium alloy wrought products — Determination of primary
alpha content — Point count method and line intercept method
EN 3684, Aerospace series — Test methods — Titanium alloy wrought products — Determination of beta
transus temperature — Metallographic method
EN 3873, Aerospace series — Test methods for metallic materials — Determination of fatigue crack growth
rates using Corner-Cracked (CC) test pieces

1) Published as ASD-STAN Prestandard at the date of publication of this standard.
EN 3874, Aerospace series — Test method for metallic materials — Constant amplitude force-controlled low
2)
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 method for metallic materials — Constant amplitude strain-controlled low
2)
cycle fatigue testing
EN 4050-1, Aerospace series — Test method for metallic materials — Ultrasonic inspection of bars, plates,
2)
forging stock and forgings — Part 1: General requirement
EN 4050-4, Aerospace series — Test method for metallic materials — Ultrasonic inspection of bars, plates,
2)
forging stock and forgings — Part 4: Acceptance criteria
EN 4258, Aerospace series — Metallic materials — General organization of standardization — Links between
types of EN standards and their use
2)
EN 4259, Aerospace series — Metallic materials — Definition of general terms
EN 9100, Quality Management Systems — Requirements for Aviation, Space and Defense Organizations
EN ISO 643, Steels — Micrographic determination of the apparent grain size (ISO 643:2003)
EN ISO 6892-1, Metallic materials — Tensile testing — Part 1: Method of test at room temperature
(ISO 6892-1:2009)
prEN ISO 6892-2, Metallic materials — Tensile testing — Part 2: Method of test at elevated temperature
(ISO/DIS 6892-2:2009)
EN ISO 12737, Metallic materials — Determination of plane-strain fracture toughness (ISO 12737:2005)
EN ISO 4288, Geometrical product specifications (GPS) — Surface texture: Profile method — Rules and
procedures for the Assessment of surface texture (ISO 4288:1996)
TR 2410, Aerospace series — Metallic materials — Relationship between dimensional standards and material
3)
standards
4)
AMS 2750, Pyrometry
2) Published as ASD-STAN Prestandard at the date of publication of this standard.
3) Published as ASD-STAN Technical Report at the date of publication of this standard.
4) Published by: American Society for Testing and Materials (ASTM), 100 Barr Harbor Drive, PO Box C700, West
Conshohocken, PA, 19428-2959 USA.
3 Terms and definitions
For the purposes of this document, the terms and definitions given in EN 4259 apply.
4 Wording of order
The order shall clearly indicate:
 quantities to be supplied;
 dates of delivery;
 material standard number;
 delivery condition and metallurgical code of products;
 dimensions and tolerances or reference to an appropriate dimensional standard;
 product designation, when required;
 forwarding address;
 nature and type of packing, if required;
 definition and frequency of any special tests and their retest procedures, if required.
5 Health and safety
The product 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.
A product safety data sheet shall be available.
6 Technical requirements
6.1 General
The product shall be manufactured in accordance with the requirements of the relevant material standard and
the applicable requirements of this specification. A manufacturing schedule shall be established and applied in
accordance with EN 2078.
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.
Notwithstanding previous acceptance complying with this material standard, any product that is found, at a
later stage, to contain such defects shall be rejected.
Unless otherwise specified, the requirements in Tables 1 and 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. If a specific line number is not
shown in Tables 1 and 2, the requirement is stated in the material standard and/or order.
The requirements of the order and/or material standard shall over-ride the requirements of the technical
specification.
6.2 Qualification requirements
Qualification requirements when invoked by the material standard and/or order are detailed in Tables 1 and 2.
Unless otherwise agreed between the manufacturer and purchaser the qualification phase shall be run on the
first three batches coming from three ingots.
6.3 Release requirements
6.3.1 Release tests
Release testing shall be the responsibility of the manufacturer.
The purchaser reserves the right to perform any of the inspections and/or tests required by the material
standard and/or order.
The test samples shall be representative of the product.
When required the manufacturer shall inform the purchaser of the planned dates for extraction of samples and
release testing in order that these operations may be witnessed.
Tables 1 and 2 detail the requirements for each line of the material standard. Unless otherwise specifically
requested by the purchaser, a particular inspection and/or test for release shall be carried out if corresponding
acceptance criteria and/or values are stated in the applicable material standard, but see also in 6.3.5.
6.3.2 Retests
If the test procedure or test piece preparation is faulty, testing shall be re-applied at the original frequency
after rectification of the original cause of failure.
When failure cannot be attributed to faulty testing, or test piece preparation, further test samples shall be
selected at twice the original frequency from the product, one of which shall be that on which the original
results were obtained unl
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