1、AECMA STANDARD NORME AECMA AECMA NORM prEN 4400-3 Edition P 1 October 2001 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STANDARDIZATION (AECMA-STAN) Gulledelle 94 - B-1200 BRUXELLES - Tel. (+32) 2 775 81 10 - Fax. (+32) 2 775 81 11 Will supersede ICs: EN 2070-1 : 1989 + EN 2070-1/
2、Al : 1993 and EN 2070-3 : 1989 Descriptors: ENGLISH VERSION Aerospace series Aluminium and aluminium alloy wrought products Technical Specification Part 3: Bar and section Srie arospatiale Produits corroys en aluminium et alliages daluminium Spcification technique Partie 3: Barres et profils Luft- u
3、nd Raumfahrt Halbzeug aus Aluminium und Aluminium-Knetlegierungen Technische Lieferbedingungen Teil 3: Stangen und Pressprofile This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA-STAN (The European Association of Aerospace Industries - Standardization). It is pub
4、lished on green paper for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeabilit
5、y is affected, physically or functionally, without re-identification of the standard. After examination and review by users and formal agreement of AECMA-STAN it will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. Nota - Extra copies can be
6、 supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 92138 ISSY-LES-MOULINEAUX CEDEX I I Edition approved for publication I Comments should be sent within six months I Material Domain 2001-10-31 after the date of publication to Gulledelle 94 AECMA-STAN Mr Evetts 8-1200 BRUXELLES
7、 0 aecma 20C COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesPage 2 prEN 4400-3: 2001 Content Page O 1 2 3 4 5 6 Annex A Annex B Introduction . Normative references . Defin it ions . . Wording of order . Health and safety Technical requ
8、irements . (normative) Orientation and location of tensile test specimens in bar and sections . (normative) Orientation and location of bearing stress test specimens in bar and sections . 3 3 3 5 5 5 6 29 31 e * COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Infor
9、mation Handling ServicesPage 3 prEN 4400-3: 2001 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, manufactur
10、e, testing, inspection and delivery of aluminium and aluminium alloy, bar and section, produced by extrusion or drawing. 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 ref ere
11、n ces This European Standard incorporates by dated or undated reference provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of thes
12、e publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. IS0 3274 Geometrical Product Specifications (GPS) - Surface texture: Profile method - Nominal characteristics of con
13、tact (stylus) instruments Aluminium and aluminium alloys - Wrought products - Temper designations Aerospace series - Quality assurance - EN aerospace products - Approval of the quality system of manufacturers Aerospace series - Test methods for metallic materials - Part 1: Tensile testing at ambient
14、 temperature 1) Aerospace series - Metallic materials -Test methods - Part 6: Bend testing 1) EN 515 EN 2000 EN 2002-1 EN 2002-6 EN 2002-8 Aerospace series - Metallic materials - Test methods - Part 8: Micrographic determination of grain size 1) Aerospace series - Metallic materials - Test methods -
15、 Part 22: Plane strain fracture EN 2002-22 toughness test 4 EN 2004-1 EN 2004-10 Aerospace series - Test methods for aluminium and aluminium alloy products - Part 1: Determination of electrical conductivity of wrought aluminium alloy products Aerospace series - Test methods for aluminium and alumini
16、um alloy products - Part IO: Preparation of micrographic specimens for aluminium alloys 1) Aerospace series - Metallic materials -Test methods - Shear testing for thinflat product 1) Aerospace series - Metallic materials - Part 1 : Designation 1) Aerospace series - Metallic materials - Part 2: Codin
17、g of metallurgical condition in delivery condition Aerospace series - Metallic materials - Manufacturing schedule, inspection schedule, inspection and test report - Definition, general principles, preparation and approval EN 2021 EN 2032-1 EN 2032-2 EN 2078 COPYRIGHT Association Europeene Des Constr
18、ucteurs de Materiel AerospaceLicensed by Information Handling ServicesPage 4 prEN 4400-3: 2001 EN 2715 EN 2716 EN 2720 EN 3042 EN 3874 EN 3987 EN 3988 EN 4050-4 EN 4258 EN 4259 EN 4268 EN 4522 EN 4523 EN 4524 EN 4525 EN 4527 EN 6018 EN 6072 EN 10003-1 EN 12258-1 TR 241 O Aerospace series - Macrograp
19、hic examination of aluminium and aluminium alloy wrought products, forging stock and forgings Aerospace series - Test method - Determination of susceptibility to intergranular corrosion - Wrought aluminium alloy products - AL-P2XXX- series, AL-P7XXX- series and aluminium-lithium alloys 1) Aerospace
20、series - Test method for metallic materials - Testing of susceptibility to exfoliation corrosion in 2XXX and 7XXX series wrought aluminium alloy products for aerospace constructions 1) Aerospace series - Quality assurance - EN aerospace products - Qualification procedure Aerospace series - Test meth
21、ods for metallic materials - Constant amplitude force- controlled low cycle fatigue testing 1) Aerospace series - Test method for metallic materials - Constant amplitude force- controlled high cycle fatigue testing 2) Aerospace series - Test methods for metallic materials - Constant amplitude strain
22、- controlled low cycle fatigue testing 1) Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 4: Acceptance criteria 1) Aerospace series - Metallic materials - General organization of standardization - Links between types o
23、f EN standards and their use Aerospace series - Metallic materials - Definition of general terms 2) Aerospace series - Metallic materials - Heat treatment facilities - General requirements 2) Aerospace series - Metallic materials - Test methods - Pin-type bearing test of yield strength 1) Aerospace
24、series - Metallic materials - Test methods - Compression testing 1) Aerospace series - Metallic materials - Test methods - Measurement of fatigue crack growth rates 1) Aerospace series -Aluminium and aluminium alloys - Test methods - Shear testing 1) Aerospace series - Aluminium and aluminium alloy
25、products - Test methods - Determining susceptibility to stress-corrosion cracking 1) Aerospace series - Test methods for metallic materials - Determination of density according to displacement method 1) Aerospace series - Metallic materials - Test methods - Constant amplitude fatigue testing 1) Meta
26、llic materials - Brinell hardness test - Part 1 : Test method Aluminium and aluminium alloys - Terms and definitions - Part 1 : General terms Aerospace series - Relationship between dimensional standards and metallic material standard 3) I) Published as AECMA Prestandard at the date of publication o
27、f this standard 2) In preparation at the date of publication of this standard 3) Published as AECMA Technical Report at the date of publication of this standard COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesPage 5 prEN 4400-3: 2001 Ma
28、ss a or No. of final lengths a e3 Definit ions O, F, H TXXX I3 O00 kg I2 O00 kg 5 250 I200 General definitions, see EN 4259. For definitions of temper designation, see EN 51 5. For definitions specific to aluminium alloys, see EN 12258-1 and with the following additions for aluminium alloy bar and s
29、ection: 3.1 Batch As defined in EN 4259 with the following additions: I Temper 3.2 Controlled stretching Stretching performed after solution heat treatment and quenching for the purpose of reducing internal stresses andlor deviation from straightness/flatness or may be critical to the achievement of
30、 the specified mechanical properties. The stretching is defined by a minimum and maximum permanent elongation stated in the material standard. 4 Wording of order The order shall clearly indicate: - quantities to be supplied; - dates of delivery; - material standard number; - delivery condition; - di
31、mensions and tolerances or reference to an appropriate dimensional standard; - 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 fulf
32、il 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. COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesPage 6 prEN 4400-3: 2001 Starting Sample(s) f
33、rom the first 3 batches 6 Technical requirements Intermediate Samples from the 4th and 5th batches The product shall satisfy the requirements of the material standard and/or order. Instructions for the use of the material standard are contained in EN 4258. Unless otherwise specified, the requirement
34、s in tables 1 and 2 shall apply in conjunction with those of the relevant material standard. Table I 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 ma
35、terial standard details specific qualification requirements. If a specific line number is not shown in tables I and 2, the requirement is stated in the material standard and/or order. 6.1 Qualification requirements 6.2 Release requirements Release testing shall be the responsibility of the manufactu
36、rer. The purchaser reserves the right to perform any of the inspections andlor 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 r
37、elease 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 andlor test for release shall be carried out if corresponding acceptance cr
38、iteria andlor values are stated in the applicable material standard, but see also section 6.2.4 “Capability clause“. 6.2.1 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. Wh
39、en 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 id
40、entification 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 lengths accepted, or - partially or fully re-heat treated if heat treatment can r
41、ectify the cause of the failure and tested as a completely new batch except for chemical composition. No product or test sample shall be re-heat treated more than twice. COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesPage 7 prEN 4400-3
42、: 2001 6.2.2 Rejection Any failure to meet the requirements of the material standard shall be cause for rejection. 6.2.3 Special tests Special tests additional to those detailed in the material standard may be required by the purchaser. In such cases, the nature of the test, method, frequency and ac
43、ceptance criteria shall be specified on the order or inspection schedule and shall be mutually agreed by the manufacturer and the purchaser. 6.2.4 Capability clause Where this is invoked and where sufficient evidence exists, the test shall not normally be carried out unless specifically requested by
44、 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 ca
45、rried out at a frequency agreed between the manufacturer and purchaser. e 6.2.5 Statistical process control Reduction in the extent of release testing, other than that defined in 6.2.4 above may be negotiated with the purchaser on the basis of appropriate statistical process control andlor statistic
46、al data. 6.2.6 Inspection and test report The manufacturer shall furnish, with each delivery, a report conforming to the requirements of EN 2078 stating the following: - manufacturers name and address; - order number; - material standard number; - delivery condition and metallurgical code of the pro
47、duct; - quantity and dimensions; - cast and batch number; - batch and/or test samples heat treatment, if required by the purchaser; - results of the tests and chemical analysis. COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesPage 8 prE
48、N 4400-3: 2001 al lu CI .- k Q m al c L 3 m- hl O u) al S CI F .- - 8 + ci v) S E 2 .- 3 U al m o S .e o L - .- ii I n 7 al 2 c m 8 L a, a 7 c u) m U a, a L T- e cn o i a 7 cv - I - I - I e m U C m v) m I - .- i I E a, C U a, m v) a, v) a, O v) m a, C 3 5 .- c c 5 5 - 2 e Li S o 3 C - E a, O C O 5 c
49、 .- c1 u v) U a, .- 5 z - ul C .- c - E“ 2 Yi O U O 5 - o - - I - I - I C O o a, m U C m .- I m m - E u- - 7. d - I I I I - v m C O u) c .- E E I .- - I W 3 C e .- COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesPage 9 prEN 4400-3: 2001 Q, m a, U a, C .- - 5 .- i a, O a, O v) C E 5 c e E I L 5 3 P .- 3 U a, E C O o m c v) v) C O m C Is) v) a, U o 3 U - .- c .- c g U a, r v) C .- F .- E s U- L L % .- 3 U C a, c Y C a 9 - L 5 a, O U a, m e w - L a, Q O v) C a, K w e e o a, a, m C a, O C O m 5 E e .- I E e C C a, .-
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