Aerospace series - Nuts, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated - Classification: 1 550 MPa (at ambient temperature)/600 °C - Technical specification

This standard specifies the characteristics, qualification and acceptance requirements for self-locking nuts with MJ threads in NI-PH2601, silver plated.
Classification: 1 550 MPa  ) / 600 °C.
It is applicable whenever referenced.

Série aérospatiale - Ecrous, a freinage interne, a filetage MJ, en alliage résistant a chaud a base de nickel - NI-PH2601 (Inconel 718), argentés - Classification: 1 550 MPa (a température ambiante)/600°C - Spécification technique

Aerospace series - Nuts, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated - Classification: 1 550 MPa (at ambient temperature)/600 °C - Technical specification

General Information

Status
Withdrawn
Publication Date
30-Apr-2004
Withdrawal Date
31-May-2005
Technical Committee
Current Stage
9900 - Withdrawal (Adopted Project)
Start Date
01-Jun-2005
Due Date
01-Jun-2005
Completion Date
01-Jun-2005

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EN 4047:2004
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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Nuts, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated - Classification: 1 550 MPa (at ambient temperature)/600 °C - Technical specificationSérie aérospatiale - Ecrous, a freinage interne, a filetage MJ, en alliage résistant a chaud a base de nickel - NI-PH2601 (Inconel 718), argentés - Classification: 1 550 MPa (a température ambiante)/600°C - Spécification techniqueAerospace series - Nuts, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated - Classification: 1 550 MPa (at ambient temperature)/600 °C - Technical specification49.030.30MaticeNutsICS:Ta slovenski standard je istoveten z:EN 4047:2003SIST EN 4047:2004en01-maj-2004SIST EN 4047:2004SLOVENSKI
STANDARD



SIST EN 4047:2004



EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 4047February 2003ICS 49.030.30English versionAerospace series - Nuts, self-locking, MJ threads, in heatresisting nickel base alloy NI-PH2601 (Inconel 718), silver plated- Classification: 1 550 MPa (at ambient temperature)/600 °C -Technical specificationThis European Standard was approved by CEN on 1 November 2002.CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this EuropeanStandard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such nationalstandards may be obtained on application to the 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 translationunder the responsibility of a CEN member into its own language and notified to the Management Centre has the same status as the officialversions.CEN members are the national standards bodies of Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece,Hungary, Iceland, Ireland, Italy, Luxembourg, Malta, Netherlands, Norway, Portugal, Slovak Republic, Spain, Sweden, Switzerland andUnited Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMITÉ EUROPÉEN DE NORMALISATIONEUROPÄISCHES KOMITEE FÜR NORMUNGManagement Centre: rue de Stassart, 36
B-1050 Brussels© 2003 CENAll rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 4047:2003 ESIST EN 4047:2004



EN 4047:2003 (E)2ContentsForeword.31Scope.32Normative references.33Terms and definitions.44Quality assurance.64.1Qualification.64.2Acceptance.64.2.1Purpose.64.2.2Conditions.64.2.3Responsibility.64.2.4Inspection and test report.65Requirements.6SIST EN 4047:2004



EN 4047:2003 (E)3ForewordThis document EN 4047:2003 has been prepared by the European Association of Aerospace Manufacturers(AECMA).After enquiries and votes carried out in accordance with the rules of this Association, this Standard has receivedthe approval of the National Associations and the Official Services of the member countries of AECMA, prior to itspresentation to CEN.This European Standard shall be given the status of a national standard, either by publication of an identical text orby endorsement, at the latest by August 2003, and conflicting national standards shall be withdrawn at the latest byAugust 2003.According to the CEN/CENELEC Internal Regulations, the national standards organizations of the followingcountries are bound to implement this European Standard : Austria, Belgium, Czech Republic, Denmark, Finland,France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Luxembourg, Malta, Netherlands, Norway, Portugal,Slovakia, Spain, Sweden, Switzerland and United Kingdom.1 ScopeThis standard specifies the characteristics, qualification and acceptance requirements for self-locking nuts with MJthreads in NI-PH2601, silver plated.Classification: 1 550 MPa 1) / 600 °C 2).It is applicable whenever referenced.2 Normative referencesThis European Standard incorporates by dated or undated reference, provisions from other publications. Thesenormative references are cited at the appropriate places in the text, and the publications are listed hereafter. Fordated references, subsequent amendments to or revisions of any of these publications apply to this EuropeanStandard only when incorporated in it by amendment or revision. For undated references the latest edition of thepublication referred to applies (including amendments).ISO 2859-1Sampling procedures for inspection by attributes - Part 1: Sampling schemes indexed by acceptancequality limit (AQL) for lot-by-Iot inspection.ISO 3452Non-destructive testing - Penetrant inspection - General principles.ISO 3534Statistics -Vocabulary and symbols.ISO 4288Geometrical product specifications (GPS) - Surface texture: Profile method - Rules and proceduresfor the assessment of surface texture.
1)Corresponds to the minimum tensile stress which the nut is able to withstand at ambient temperature without breaking orcracking when tested with a bolt of a higher strength class.2)Maximum test temperature of the partsSIST EN 4047:2004



EN 4047:2003 (E)4ISO 8642:1986Aerospace - Self-locking nuts with maximum operating temperature greater than 425 °C - Testmethods.EN 2786Aerospace series - Electrolytic silver plating of fasteners 3).EN 3042Aerospace series - Quality assurance - EN aerospace products - Qualification procedure.ASTM E112-96Standard Test Methods for Determining Average Grain Size 4).3 Terms and definitionsFor the purposes of this European Standard, the following terms and definitions apply.3.1 batchquantity of finished nuts, of the same type and same diameter, produced from a material obtained from the samemelt, manufactured in the course of the same production cycle, following the same manufacturing route and havingundergone all the relevant heat treatments and surface treatments3.2 Surface discontinuities3.2.1 crackrupture in the material which may extend in any direction and which may be intercrystalline or transcrystalline incharacter3.2.2 seamopen surface defect3.2.3 lapsurface defect caused by folding over metal fins or sharp corners and then compressing them into the surface3.2.4 inclusionsnon-metallic particles originating from the material manufacturing process. These particles may be isolated orarranged in strings.3.3 test temperatureambient temperature, unless otherwise specified3.4 simple random samplingtaking of n items from a population of N items in such a way that all possible combinations of n items have thesame probability of being chosen 5)
3)Published as AECMA Prestandard at the date of publication of this standard4)Published by: American Society for Testing and Materials (ASTM), 100 Barr Harbor Dr, West Conshohocken, PA 19428-2959- USA5)Definition taken from ISO 3534SIST EN 4047:2004



EN 4047:2003 (E)53.5 critical defectdefect that, according to judgement and experience, is likely to result in hazardous or unsafe conditions forindividuals using, maintaining, or depending upon the considered product, or that is likely to prevent performance ofthe function of a major end item 5)3.6 major defectdefect other than critical, that is likely to result in a failure or to reduce materially the usability of the consideredproduct for its intended purpose 5)3.7 minor defectdefect that is not likely to reduce materially the usability of the considered product for its intended purpose, or thatis a departure from established specification having little bearing on the effective use or operation of this product 5)3.8 sampling planplan according to which one or more samples are taken in order to obtain information and possibly to reach adecision 5)3.9 limiting qualityin a sampling plan, the quality level which corresponds to the specified 10% probability of acceptance3.10 acceptable quality level (AQL)quality level which in a sampling plan corresponds to a specified but relatively high probability of acceptance.It is the maximum per cent defective (or the maximum number of defects per hundred units) that, for purposes ofsampling inspection can be considered satisfactory as a process average 5)3.11 finished nutnut ready for use, inclusive of any possible treatments and/or surface coatings, as specified in the product standardor definition document3.12 definition documentdocument specifying all the requirements for finished nuts3.13 self-locking torquetorque to be applied to the nut or bolt to maintain its movement of rotation in relation to the associated part, theassembly being under no axial load and the nut locking zone being completely engaged with the bolt (minimumprotrusion of two pitches, including the end chamfer)3.14 seating torquetightening torque to be applied to the nut or bolt to introduce or to increase the axial load in the assembly3.15 unseating torqueuntightening torque to be applied to the nut or bolt to reduce or remove the axial load in the assemblySIST EN 4047:2004



EN 4047:2003 (E)63.16 breakaway torquetorque required to start unscrewing the nut or bolt with respect to the associated part, with the nut locking zone stillfully engaged on the bolt, but after the axial load in the assembly has been removed by unscrewing half a turnfollowed by a halt in rotational movement3.17 torque for testing the wrench featuretorque to be applied to the wrenching feature of the nut4 Quality assurance4.1 QualificationEN 3042Qualification inspections and tests (requirements, methods, numbers of nuts) are specified in Table 1. They shallbe carried out on:- each type and diameter of nut;- 46 nuts selected from a single batch by simple random sampling.The test programme may possibly be reduced, or the qualification be granted without inspection or testing : anysuch decision shall be based on the results obtained on similar types and diameters of nuts provided that thedesign and manufacturing conditions are identical.Table 2 indicates the allocation of nut samples for the inspections and tests.4.2 Acceptance4.2.1 PurposeThe purpose of acceptance inspections and tests is to check, as simply as possible, by a method representative ofactual use conditions, with the uncertainty inherent to statistical sampling, that the nuts constituting the batchsatisfy the requirements of this standard.4.2.2 ConditionsAcceptance inspections and tests (requirements, methods, numbers of nuts) are specified in Table 1. They shall becarried out on each batch. Nuts from the batch to be tested shall be selected by simple random sampling.Each nut may be submitted to several inspections or tests.If a more stringent inspection is deemed necessary, all or part of the qualification inspections and tests may beperformed during the acceptance inspection and testing. In this case, the number of nuts submitted to theseinspections and tests is the same as that submitted for qualification inspection and tests.4.2.3 ResponsibilityAcceptance inspections and tests shall be carried out by the manufacturer, or under his responsibility4.2.4 Inspection and test reportA test report showing actual numerical values shall be provided if specified in the purchase order.5 RequirementsSee Table 1.SIST EN 4047:2004



EN 4047:2003 (E)7Table 1 – Technical requirements and test methodsClauseCharacteristicRequirementInspection and test methodQ/A aSample sizeQ5.1MaterialIn accordance with the productstandard or definition documentChemical analysis orcertificate of compliance issuedby the manufacturer of the semi-finished productAQ435.2Dimensions,tolerancesandtolerances ofform andpositionIn accordance with the productstandard or definition documentStandard gauging.ATables 3 and 45.3ManufacturingQ5.3.1FormingNuts shall be formed by a hot orcold forming process.If hot formed, the formingtemperature shall not exceed1150 °C and they shall be aircooled or faster.The equipment shall ensure auniform temperature throughoutthe batch.The method of forming shall beindicated5.3.2continuedHeattreatmentThe heat treatment medium oratmosphere shall not cause anysurface contamination exceptas permitted by 5.5.4.Any scale which will not beremoved by subsequentmachining shall be removed byabrasive blasting with anappropriate equipment.Solution treat (if applicable) at atemperature of 950 °C to 980°C, held at the selectedtemperature within ± 15 °C forbetween 1 h min. and 2 h max.,quench in oil, or alternativemedium or faster.Precipitation treat at (720 ± 5)°C holding at heat for 8 h ± 15min furnace cooling at (55 ± 5)°C per h to (620 ± 5) °C holdingat 620 °C for 8 h ± 5 minfollowed by air cooling or faster.Instead of the55 °C per h cooling rate to 620°C, parts may be furnacecooled atany rate provided the time at620 °C is adjusted to give atotal precipitation time of 18 hmin.Calibration of the heat treatmentequipment shall be confirmed.Visual examinationExamination of the heattreatment specificationQSIST EN 4047:2004



EN 4047:2003 (E)8Table 1 (continued)ClauseCharacteristicRequirementInspection and test methodQ/A aSample sizeQ435.3.3Bearing surfaceperpendicularityIn accordance with the productstandard or definition document.For non-floating plate nuts having abearing surface exceeding1,5 times the thread nominaldiameter, the perpendicularityrequirement shall, unless otherwisespecified by the product standardor definition document, apply onlyto that portion of the bearingsurface of the part contained withina diameter equal to 1,5 times thethread nominal diameter.ISO 8642ATables 3 and 4Q435.3.4Thread andthreaddeformation(form out-of-round)Threads in the locking zone maybe deformed in any mannerprovi
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