Aerospace series - Titanium and titanium alloys - Technical specification - Part 002: Bar and section

This standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of
titanium and titanium alloy bar and section. 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.

Luft- und Raumfahrt - Titan und Titanlegierungen Kneterzeugnisse - Technische Lieferbedingungen - Teil 002: Stangen und Profile

Diese Norm legt die Anforderungen an die Bestellung, Herstellung, Prüfung, Inspektion und Lieferung von
Stangen und Profilen aus Titan und Titanlegierungen fest. Sie ist anzuwenden, wenn sie bei Verweisung auf
oder in Verbindung mit der EN-Werkstoffnorm erwähnt wird, sofern in der Zeichnung, Bestellung oder der
Prüfanweisung nichts anderes angegeben ist.

Série aérospatiale - Titane et alliages de titane - Spécification technique - Partie 002: Barres et profilés

Cette Norme européenne définit les exigences relatives aux commandes, fabrication, essais, contrôles et livraison des barres et profilés en titane et alliages de titane. La présente norme est applicable lorsqu'elle est citée dans la norme de matériaux EN et conjointement avec celle-ci, sauf instruction contraire figurant sur le plan, la commande ou la fiche d’essais.

Aeronavtika - Titan in titanove zlitine - Tehnična specifikacija - 002. del: Palice in profili

Ta standard določa zahteve za naročanje, proizvodnjo, preskušanje, pregledovanje in dobavo palic in profilov iz titana in titanovih zlitin, odpornih proti vročini. Uporablja se, kadar se nanaša na standard EN za materiale in skupaj z njim, razen če je drugače določeno na risbi, naročilu ali urniku pregleda.

General Information

Status
Published
Publication Date
24-Oct-2011
Technical Committee
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
14-Oct-2011
Due Date
19-Dec-2011
Completion Date
25-Oct-2011

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SLOVENSKI STANDARD
SIST EN 4800-002:2011
01-december-2011
$HURQDYWLND7LWDQLQWLWDQRYH]OLWLQH7HKQLþQDVSHFLILNDFLMDGHO3DOLFHLQ
SURILOL
Aerospace series - Titanium and titanium alloys - Technical specification - Part 002: Bar
and section
Luft- und Raumfahrt - Titan und Titanlegierungen Kneterzeugnisse - 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 4800-002:2010
ICS:
49.025.30 Titan Titanium
SIST EN 4800-002:2011 en
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

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SIST EN 4800-002:2011

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SIST EN 4800-002:2011


EUROPEAN STANDARD
EN 4800-002

NORME EUROPÉENNE

EUROPÄISCHE NORM
November 2010
ICS 49.025.30
English Version
Aerospace series - Titanium and titanium alloys - Technical
specification - Part 002: Bar and section
Série aérospatiale - Titane et alliages de titane - Luft- und Raumfahrt - Titan und Titanlegierungen
Spécification technique - Partie 002: Barres et profilés Kneterzeugnisse - Technische Lieferbedingungen - Teil
002: Stangen und Profile
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 4800-002:2010: E
worldwide for CEN national Members.

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
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
2

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
Foreword
This document (EN 4800-002:2010) 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.
3

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
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.
4

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
1 Scope
This standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of
titanium and titanium alloy bar and section. 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
EN 2002-16, Aerospace series — Metallic materials — Test methods — Part 16: Non-destructive testing —
1)
Penetrant testing
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 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 3683, Aerospace series — Test methods — Titanium alloy wrought products — Determination of primary
α content — Point count method and line intercept method
EN 3684, Aerospace series — Test methods — Titanium alloy wrought products — Determination of β transus
temperature — Metallographic method
EN 3874, Aerospace series — Test method for metallic materials — Constant amplitude force-controlled low
1)
cycle fatigue testing

1) In preparation at the date of publication of this standard.
5

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
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 9133, Aerospace series — Quality management systems — Qualification procedure for aerospace
standard parts
EN ISO 643, Steels — Micrographic determination of the apparent grain size (ISO 643:2003)
EN ISO 4288, Geometrical product specifications (GPS) — Surface texture: Profile method — Rules and
procedures for the assessment of surface texture (ISO 4288:1996)
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)
TR 2410, Aerospace series — Metallic materials — Relationship between dimensional standards and material
3)
standards
4)
AMS 2750, Pyrometry
4)
ASTM E 399, Standard test method for linear-elastic plane-strain fracture toughness k/c of metallic materials

2) In preparation 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.
6

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
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 products in the delivery condition shall fulfil the 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.
7

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
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 different 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 unless already withdrawn by the manufacturer after suitable identification of the cause
of failure. If all retest results are satisfactory, the batch shall be accepted. If one or more tests are
unsatisfactory, the batch shall be:
 rejected; or
 100 % retested and the conforming products accepted; or
 partially or fully re-heat treated if heat treatment can rectify the cause of the failure and tested as a
completely new batch except for chemical composition, for which redetermination of hydrogen content is
required. No product or test sample shall be re-heat treated more than twice.
6.3.3 Rejection
Any failure to meet the requirements of the material standard shall be cause for rejection.
6.3.4 Special tests
Special tests may be required by the purchaser. In such cases, the nature of the test, method, frequency and
technical requirements shall be specified on the order or inspection schedule and shall be mutually agreed by
the manufacturer and purchaser.
8

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
6.3.5 Capability clause
Where capability clause is invoked and where sufficient statistical evidence exists, the test shall not be carried
out (unless specifically requested by the purchaser). However, this in no way reduces the obligations of the
manufacturer to fulfil the requirements. If subsequent testing indicates that the product does not comply with
the requirements, the batch shall be rejected.
If sufficient statistical evidence does not exist, the test shall be carried out at a frequency agreed between the
manufacturer and the purchaser.
6.3.6 Statistical process control
Reduction in the extent of release testing, other than that defined in 6.3.5 above, may be negotiated with the
purchaser on the basis of appropriate statistical process control and/or statistical data.
6.3.7 Inspection and test report
The manufacturer shall furnish, with each delivery, a report conforming to the requirements of EN 2078 stating
the following:
 manufacturer's name and address and, if appropriate, identification of the plant;
 order number;
 material standard number;
 delivery condition and metallurgical code of the product;
 quantity and dimensions;
 manufacturing and inspection schedule reference;
 cast and batch number;
 batch and/or test samples heat treatment condition;
 results of the tests and retests if any.
6.4 Traceability
Each product shall be traceable to the cast, production batch and/or heat treatment batch at all stages of
manufacture, testing and delivery.

9

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
Table 1 — Technical requirements for lines 1 to 29, where appropriate
Frequency of testing
Material standard line
reference
Requirements
Qualification Release
No Title
1 Material designation See EN 2032-1. − −
2 Chemical composition The test samples used for chemical analysis shall be representative of the product and shall be taken from 2 per cast 2 per cast
location corresponding to top and bottom of each ingot produced after the final melting stage. The method
of chemical analysis shall be at the discretion of the manufacturer unless otherwise stated in the material
standard or order. In cases of dispute, the method of chemical analysis shall be agreed between the
manufacturer and purchaser preferably using existing chemical analysis standards. The measured
chemical composition shall be stated on the inspection certificate.
Specific requirements for hydrogen content: 1 per batch 1 per batch
The hydrogen content shall be determined on each batch in the delivery condition in accordance with
EN 3976.
3 Method of melting Method of melting consists of multiple melt using combination of non-consumable electrode, consumable − −
electrode and cold hearth (electron beam or plasma arc) melting practices. Some of the following
requirements are dependent on the actual melting route non-consumable electrode melting should be used
for consolidation purpose only.
1 Raw material:
Raw materials shall be purchased only from suppliers approved by the manufacturer and registered in
his list of approved suppliers.
Approval of suppliers shall be made in accordance with written procedures contained within the quality
assurance system of the manufacturer.
Titanium sponge and alloying elements:
The requirements shall be specified by the manufacturer who shall also establish the following
procedures for the evaluation and acceptance testing of each batch:
— titanium sponge: manufacturing method, level of impurities, particle size, freedom from surface
contamination;
— alloying elements: chemical composition including level of impurities, particle size, freedom from
foreign particles.
continued
10

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
Table 1 — Technical requirements for lines 1 to 29, where appropriate (continued)
Frequency of testing
Material standard line
reference
Requirements
Qualification Release
No Title
Recycling of scrap:
3 Method of melting – –
(continued) See EN 2955.
The categories and sub-categories of scrap which may be used by the manufacturer are given in the
following table.

Scrap categories and Melting method
VAR-only melt method
sub-categories (see EN 2955) which includes cold hearth
1 allowed allowed
2 allowed allowed
3 allowed allowed
a a
4.1
allowed  allowed
a b a
4.2.1
allowed  allowed
a b a
4.2.2
allowed  not allowed
a b a
4.3.1
allowed  allowed
a b a
4.3.2
allowed  not allowed
5.1 allowed allowed
5.2 not allowed not allowed
6 not allowed not allowed
a
 Only turnings produced by the melter shall be used, unless otherwise agreed by the purchaser.
b
X-ray inspection not required.

Foundry scrap, castings, bolts or used components shall not be used.

The manufacturer shall maintain a list of his approved scrap processors. The list shall indicate the
categories of scrap for which the processors are approved.
Each order for scrap shall refer to EN 2955, specify the category and, if necessary, the sub-category
of the scrap. In the case of turnings the limits for O , C and H shall also be specified.
2 2
continued
11

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
Table 1 — Technical requirements for lines 1 to 29, where appropriate (continued)
Frequency of testing
Material standard line
reference
Requirements
Qualification Release
No Title
3 Method of melting 2 Charge preparation: – –
(continued)
The melter shall establish procedures for the charge make up which shall include, if appropriate:
— scrap categories and sub-categories to be used;
— amount of recycled scrap;
— charge composition;
— requirements for recording the constitution of each charge;
— compaction.
The scrap shall be of the same alloy, or compatible with the final alloy composition.
 3 Electrode constitution (if appropriate):
Build up of electrodes and attachment of their stubs shall be carried out under a vacuum or inert gas
atmosphere in accordance with the procedure defined by the manufacturer.
 4 Welding:
The welding method to be used for fabricating electrodes, joining electrodes and joining stubs to the
electrode shall be Metal Inert Gas (MIG) or Plasma in an inert gas atmosphere or Electron Beam (EB)
under vacuum. In addition stubs may be attached to electrodes by electric arc in a VAR furnace.
 5 Melting:
Melting process consists of:
— a first melting using a consumable electrode or a cold hearth process, (non consumable electrode is
no longer in use as a first melt);
— at least one consumable electrode remelting, except where a cold hearth melting route is used for
commercially pure titanium.
Scrap may only be used during the first melt, except for striking the arc.
The stub weld interface shall not be melted during the second or subsequent melts. The stub weld
interface may be melted during the first melting operation if the stub is of the same alloy and the weld
has been made without filler metal, in a vacuum or inert gas atmosphere.
continued
12

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
Table 1 — Technical requirements for lines 1 to 29, where appropriate (continued)
Frequency of testing
Material standard line
reference
Requirements
Qualification Release
No Title
3 Method of melting Arc breaks during the final melting operation shall not exceed 60 s during steady state melting. − −
(concluded)
An appropriate system shall be provided for the control, checking and verification of the voltage,
pressure, and either current or melt rate.
The manufacturer shall establish written procedures which define (if appropriate):
— the cleaning of furnace and ingot-moulds;
— the purity of inert gas used;
— the current, the voltage and the maximum allowed pressure during melting;
— the maximum allowed leak rate in the furnace;
— the hot topping cycle at the end of the final melt;
— the inspection of the stub weld interface after melting.
4.1 Form Bar and section – –
4.2 Method of production Mechanical hot working:
The manufacturer shall establish a procedure for mechanical hot working.
This procedure shall define:
— the homogenisation thermal cycle;
— the thermo-mechanical working processes;
— the manufacturing schedule for each process: the temperatures and durations of pre-heating; the
maximum time of each working process; the dimensions of the products at each step and conditions
for heat treatment between operations.
 Mechanical cold working:
The manufacturer shall establish a procedure for the mechanical cold working.
This procedure shall define:
— the mechanical working processes;
— the manufacturing schedule for each process; the dimensions of the products at each step and heat
treatment conditions between operations.
Final conversion shall be done by hot or cold rolling according to material standard.
continued
13

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
Table 1 — Technical requirements for lines 1 to 29, where appropriate (continued)
Frequency of testing
Material standard line
reference
Requirements
Qualification Release
No Title
4.2 Method of production Straightening: – –
(concluded)
Straightening and stress relieving operations shall be indicated in the manufacturing schedule and shall
not cause any defects prejudicial to the intended use.
Surface finishing:
Products shall be supplied in the descaled condition. For products in the machined condition, all
additional requirements shall be defined on the order. The surface finish shall allow the satisfactory
performance of the inspection operation specified.
The method used for removal of defects such as cracks, burrs, etc. from the edges and ends of products
shall be agreed between manufacturer and purchaser.
4.3 Limit dimension(s) Minimum and/or maximum size of the product expressed as the nominal thickness a, or nominal − −
thicknesses for multi-legged/flanged sections, or as a nominal diameter, D, of round bar or as equivalent
diameter D of non circular or non rectangular section products.
e
5 Technical specification Reference to this technical specification EN 4800-002. In cases of conflict, the requirements of the material − −
standard shall take precedence over those of this technical specification.
6.1 Delivery condition Product shall be supplied in the delivery condition specified in this line in the material standard and/or as − −
stated on the order.
Marking:
The method of marking used shall not cause corrosion, crack initiation, contamination or unacceptable
deformation. The marking shall remain permanently visible after handling and contact with protective
products.
Unless otherwise specified, the nature and colour of marking ink and type of marking characters shall be
left to the discretion of the manufacturer. The marking inks shall be removable with cleaning products
which do not leave a residue which could affect further processing. The cleaning products shall not give
rise to corrosion.
continued
14

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
Table 1 — Technical requirements for lines 1 to 29, where appropriate (continued)
Frequency of testing
Material standard line
reference
Requirements
Qualification Release
No Title
6.1 Delivery condition All lengths shall be marked legibly as indicated in the following tables unless otherwise agreed between the − −
manufacturer and purchaser:
  Products of diameter or major sectional dimension, a or D ≥≥≥≥ 12,5 mm
a b
  Continuous marking  End marking

• Material standard
• Nominal dimensions in millimetres or
part/drawing no.

• Delivery condition code
• Manufacturer/plant identification
a
  Ink or similar product shall be used. All information shall be repeated at least every 500 mm.
b
Hard stamping on one end of the length.


  Products of diameter or major sectional dimension, a or D <<<< 12,5 mm
• The information stated in the above table shall be indelibly marked on a durable label

attached to each bundle or products.

Packing:

All necessary precautions shall be taken to prevent damage to the product, especially where the delivered
surface finish shall be maintained.
The packing shall be suitable for the type of transportation used.
The exterior of the packing shall bear the following information:
— name and address of recipient;
— mass;
— order number and sufficient information to enable the contents to be related to the relevant
documentation.
Shipment:
The responsibility for shipping shall be detailed in a transport contract.
continued
15

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SIST EN 4800-002:2011
EN 4800-002:2010 (E)
Table 1 — Technical requirements for lines 1 to 29, where appropriate (continued)
Frequency of testing
Material standard line
reference
Requirements
Qualification Release
No Title
6.1 Heat treatment Thermal and/or thermomechanical operations shall be applied to the product as specified in the material – –
standard and are listed in the same order as they are to be applied. No product shall be re-solution heat
treated more than once without the agreement of the purchaser. Abbreviations and symbols used in the
material standard are shown in the following table: all other terms are written in full.
  Term Abbreviation/Symbol Term Abbreviation/Symbol
temperature θ water quench WQ
time t oil quench OQ

hour h forced air quench AQ
air cool AC
minute min
  furnace cool FC
 AMS 2750 to be used unless otherwise agreed between customer
...

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