SIST EN 3335:2005
(Main)Aerospace series - Aluminium alloy AL-P7475-O2 - Sheet for superplastic forming (SPF) - 0,8 mm
- Abstract
This standard specifies the requirements relating to:
Aluminium alloy AL-P7475-
O2
Sheet for superplastic forming (SPF)
0,8 mm < or = a < or = 6 mm
for aerospace application.
- Status
- Published
- Publication Date
- 31-Oct-2005
- Technical Committee
- SS SPL - Technical Board for the general field
- Current Stage
- 6060 - National Implementation/Publication (Adopted Project)
- Start Date
- 01-Nov-2005
- Due Date
- 01-Nov-2005
- Completion Date
- 01-Nov-2005
SIST EN 3335:2005 is the Slovenian standard identical to EN 3335:2005 for aerospace aluminium sheet. It specifies the requirements for aluminium alloy AL-P7475-O2 sheet for superplastic forming (SPF) in the thickness range 0.8 mm to 6 mm, for aerospace application. Manufacturers, purchasers and test laboratories use it to agree the product form, heat treatment, testing and acceptance criteria.
What does SIST EN 3335:2005 specify?
SIST EN 3335:2005 is a product standard for a specific aluminium alloy sheet used in aerospace SPF applications. Clause 1 gives the scope, clause 2 lists the normative references, and the main body is a requirement table that covers the material, processing, tests and inspection.
The standard applies to sheet in the designated alloy and thickness range only. In practice, that means buyers and suppliers can use one document to define what material is being ordered and how it will be checked on delivery.
What are the key requirements of SIST EN 3335:2005?
Composition and product form
SIST EN 3335:2005 identifies the material as aluminium alloy AL-P7475-O2 in sheet form, produced by rolling and thermomechanical processing to improve SPF capability. The chemical composition table sets limits for the alloying elements and impurity elements, with aluminium as the base metal.
This matters because the chemistry and processing route control formability, strength and consistency from batch to batch. For procurement and incoming inspection, the document is the basis for verifying that the supplied sheet matches the specified alloy and condition.
Delivery condition, heat treatment and mechanical properties
SIST EN 3335:2005 requires delivery in condition O2 and gives a reference heat treatment for the release test condition T762. It also states that the heat treatment and minimum properties are for manufacturer release testing and may not necessarily be achieved in superplastically formed parts.
The requirement table sets minimum proof stress, tensile strength and elongation at ambient temperature in both the L and LT directions. In practice, this tells the manufacturer which test directions to use and which properties must be demonstrated before the batch is accepted.
Sampling, conductivity, grain size and defects
SIST EN 3335:2005 refers to EN 4400-2 for test samples, test pieces, grain size, external defects, marking inspection and dimensional inspection. It also gives a conductivity check after the T762 heat treatment, with acceptance linked to both conductivity and proof stress.
For the user, this means the batch is not judged only by chemistry and strength - it also has to meet microstructural and surface-condition requirements. That is important when sheet will later be formed into safety-critical aerospace components.
Superplastic forming capability and handling notes
SIST EN 3335:2005 includes a dedicated superplastic forming capability requirement. The capability is assessed by an elevated-temperature tensile test on samples taken per direction per batch, and the standard sets the acceptance criterion for elongation.
The notes also state that cold working or straightening is only acceptable within the stated strain limit. In practice, this protects the SPF behaviour of the sheet and helps preserve the properties needed for forming.
What terms does SIST EN 3335:2005 define?
- AL-P7475-O2 - the designated aluminium alloy and delivery condition covered by the standard.
- SPF - superplastic forming, the process the sheet is intended for.
- O2 - the delivery condition required for supplied sheet.
- T762 - the reference heat treatment used for release testing.
- WQ - water quench, part of the reference heat treatment route.
- Capability clause - the agreed provision that can reduce sampling when the manufacturer and purchaser accept it.
Who uses SIST EN 3335:2005?
SIST EN 3335:2005 is used by aerospace material suppliers, sheet manufacturers, purchasers, quality managers and test laboratories. They use it to specify the product, qualify batches, run acceptance tests, check dimensional and marking inspection, and decide whether the sheet is suitable for SPF parts.
It is also relevant for organizations that need to agree a common material basis before forming components. That makes ordering, release testing and incoming inspection easier to align across supply chains.
Which standards are used with SIST EN 3335:2005?
- EN 4258 - gives the general organization of aerospace metallic material standards and the links between EN standard types and their use.
- EN 4400-2 - gives the technical specification for aluminium and aluminium alloy wrought products, sheet and strip, and is used here for sampling, testing and several inspection items.
- EN 4500-2 - gives the rules for drafting and presentation of material standards for aluminium, aluminium alloys and magnesium alloys.
What does the SIST EN 3335:2005 document contain?
The document contains a specification table that covers material designation, chemical composition, method of melting, product form, production method, dimensional range, technical specification, delivery condition, test directions and temperature. It also sets out the required mechanical properties and additional checks such as conductivity, grain size, external defects and dimensional inspection.
Another part of the table describes the superplastic forming capability test, including the elevated-temperature tensile test setup used to assess elongation. The notes section adds guidance on sampling, acceptable handling after processing and how the properties relate to release testing.
Relations
- Effective Date
- 28-Jan-2026
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Frequently Asked Questions
SIST EN 3335:2005 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Aluminium alloy AL-P7475-O2 - Sheet for superplastic forming (SPF) - 0,8 mm <a <6 mm". This standard covers: This standard specifies the requirements relating to: Aluminium alloy AL-P7475- O2 Sheet for superplastic forming (SPF) 0,8 mm < or = a < or = 6 mm for aerospace application.
This standard specifies the requirements relating to: Aluminium alloy AL-P7475- O2 Sheet for superplastic forming (SPF) 0,8 mm < or = a < or = 6 mm for aerospace application.
SIST EN 3335:2005 is classified under the following ICS (International Classification for Standards) categories: 49.025.20 - Aluminium. The ICS classification helps identify the subject area and facilitates finding related standards.
SIST EN 3335:2005 has the following relationships with other standards: It is inter standard links to SIST EN 4258:2024. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
SIST EN 3335:2005 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-november-2005
Aerospace series - Aluminium alloy AL-P7475-O2 - Sheet for superplastic forming
(SPF) - 0,8 mm
Aerospace series - Aluminium alloy AL-P7475-O2 - Sheet for superplastic forming (SPF)
- 0,8 mm
Luft- und Raumfahrt - Aluminiumlegierung AL-P7475-O2 - Bleche für superplastische
Formgebung (SPF) - 0,8 mm
Série aérospatiale - Alliage d'aluminium AL-P7475-O2 - Tôles pour formage
superplastique (FSP) - 0,8 mm
Ta slovenski standard je istoveten z: EN 3335:2005
ICS:
49.025.20 Aluminij Aluminium
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EUROPEAN STANDARD EN 3335
NORME EUROPÉENNE
EUROPÄISCHE NORM
June 2005
ICS 49.025.20
English version
Aerospace series - Aluminium alloy AL-P7475-O2 - Sheet for
superplastic forming (SPF) - 0,8 mm ≤a ≤6 mm
Série aérospatiale - Alliage d'aluminium AL-P7475-O2 - Luft- und Raumfahrt - Aluminiumlegierung AL-P7475-O2 -
Tôles pour formage superplastique (FSP) - 0,8 mm ≤a ≤6 Bleche für superplastische Formgebung (SPF) - 0,8 mm ≤a
mm ≤6 mm
This European Standard was approved by CEN on 22 April 2005.
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 Central Secretariat 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 Central Secretariat has the same status as the official
versions.
CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France,
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Slovenia, Spain, Sweden, Switzerland and United Kingdom.
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EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre: rue de Stassart, 36 B-1050 Brussels
© 2005 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 3335:2005: E
worldwide for CEN national Members.
Foreword
This document (EN 3335:2005) has been prepared by the European Association of Aerospace
Manufacturers - Standardization (AECMA-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
AECMA, 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 December 2005, and conflicting national standards shall be withdrawn
at the latest by December 2005.
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, Cyprus, Czech Republic,
Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania,
Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, 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.
This standard has been prepared in accordance with EN 4500-2.
1 Scope
This standard specifies the requirements relating to:
Aluminium alloy AL-P7475-
O2
Sheet for superplastic forming (SPF)
0,8 mm ≤ a ≤ 6 mm
for aerospace application.
2 Normative references
The following referenced documents are indispensable for
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