NASM 22978-2000 Fastener, Rotary, Quick-operating,

0338743050830493bW-2978ADOPTIONNOTICENASM22978,nFASTENER,ROTARY,QUICK-OPERATING,HIGH-STRENG='I,wasadoptedon29JUNE2000forusebytheDepartrentofDefense(DoD).ProposedchangesbyDoDActivitiesæu8tbesubmittedtotheDoDAdoptingActivity:DefenseSupplyCenterPhiladelphia,ATTN:DSCP-ILEA,700RobbinsAvenue,Philadelphia,PA19111-5096.DoDActivitiesmayobtaincopiesofthisstandardfromtheStandardizationDocumentOrderDesk,700RobbinsAvenue,BuildingQD,Philadelphia,PA19111-5094.TheprivatesectorandotherGovernmentagenciesmaypurchasecopiesfromtheAEROSPACEINDUSTRIESASSOCIATIONOFAMERICA,INC.,1250EYESTREET,N.W.,WASHINGTON,DC20005-3924.custodians:Navy-ASAirForce-99DIA-ISAdoptingactivity:DIA-IS(Project5325-1033-002)COPYRIGHTAerospaceIndustriesAssociationofAmerica,Inc.(AIA[NAS])LicensedbyInformationHandlingServicesCOPYRIGHTAerospaceIndustriesAssociationofAmerica,Inc.(AIA[NAS])LicensedbyInformationHandlingServicesNATIONALAEROSPACESTANDARDOCOPYRIGHT2000AEROSPACEINDUSTRIESASSOCIATIONOFAMERICA,INC.ALLRIGHTSRESERVEDNASM22978SPECIFICATIONFASTENER,ROTARY,QUICK-OPERATING,HIGH-STRENGTH1.SCOPE1.IScope.Thisspecificationcoversthegeneralrequirementsforahigh-strength,quick-operating,rotaryfastener.1.2Classification.Fastenersfurnishedunderthisspecificationshallbeofthefollowingtypes,asspecified(see6.2):TypeI-FlushheadTypeII-Protrudinghead2.APPLICABLEDOCUMENTS2.1Thefollowingdocuments,oftheissueineffectonthedateofinvitationforbidsorrequestforproposal,formapartofthisspecificationtotheextentspecifiedherein:SPECIFICATIONSFederalQQ-A-287AluminumAlloyPlateandSheet,Alclad7075QQ-A-362AluminumAlloyPlateandSheet,Alclad2024QQ-Pd16Plating,Cadmium(Electrodeposited)MilitaryMIL-H-3982Hardware(FastenersandRelatedItems)PackagingandPackingforShipmentandStorageofMIL-S-5000Steel,Chrome-Nickel-Molybdenum(4340orE-4340)MIL-C-5541ChemicalFilmsforAluminumandAluminumAlloysMIL-S-6050Steel,Chrome-Nickel-Molybdenum(8630)Bars,MIL-H-6875HeatTreatmentofSteels,(AircraftPractice)MIL-A-8625AnodicCoatings,forAluminumandAluminumAlloysMIL-S-18728SteelPlate,Sheet,andStrip,Alloy,8630,AircraftQualityMIL-S-18729SteelPlate,Sheet,andStrip,Alloy,4130,AircraftQualityBarsandReforgingStockRods,andReforgingStock(forAircraftApplications)ProcessforTHEINITIALRELEASEOFTHISDOCUMENTSUPERSEDESMIL-F-22978,REVISIONA,AMENDMENT1.LISTOFCURRENTSHEETSNOREVNEW12NEW9NEW6NEW3NEW11NEW8NEW5NEW2NEW13NEW10NEW7NEW4NEW1REVNOREVNOREVNOREVNOLISTOFCURRENTSHEETS..~~~,NONFW17NEW9NEW6NEW3NEW11NEW8NEW5NEW2NEW13NEW10NEW7NEW4NEW1REVSHEET1OF13FSC5325APPROVALDATEMAY2000USEOFORRELIANCEUPONTHISDOCUMENTORANYNATIONALAEROSPACESTANDARDISENTIRELYVOLUNTARY.AIADOESNOTREVISIONQUALIFYSUPPLIERSORCERTIFYCONFORMANCEOFITEMSPRODUCEDUNDERNATIONALAEROSPACESTANDARDS.AIAMAKESNOREPRESENTATIONORCLAIMRESPECTING(1)THESUITABILITYOFITEMSFORANYPARTICULARAPPLICATION,OR(2)THEEXISTENCEOFORAPPLICABILITYTHERETOPFPATENTORTRADEMARKRIGHTS.COPYRIGHTAerospaceIndustriesAssociationofAmerica,Inc.(AIA[NAS])LicensedbyInformationHandlingServicesCOPYRIGHTAerospaceIndustriesAssociationofAmerica,Inc.(AIA[NAS])LicensedbyInformationHandlingServicesSTD.AIA/NASNASfl22976-ENGL2000I03387430507043800INATIONALAEROSPACESTANDARDOCOPYRIGHT2000AEROSPACEINDUSTRIESASSOCIATIONOFAMERICA,INC.ALLRIGHTSRESERVEDNASM22978STANDARDSFederalFED.STD.NO.66Steel:ChemicalCompositionandHardenabilityFED.STD.TESTMETHODNO.151Metals;TestMethodsMilitaryMIL-STD-129MarkingforShipmentandStorageMIL-STD-130IdentificationMarkingofUSMilitaryPropertyMS9006RecessesCross,LowTorqueDrive,DimensionsandGageMS17731Fasteners,Rotary,Quick-Operating,FlushHead,FloatingType,MS17732Fastener,Rotary,Quick-Operating,ProtrudingHead,FloatingDimensionsFor2210Lbs.MinTensileStrengthType,221OLbs.MinTensileStrength(Copiesofspecifications,standards,drawings,andpublicationsrequiredbysuppliersinconnectionwithspecificprocurementfunctionsshouldbeobtainedfromtheprocuringactivityorasdirectedbythecontractingofficer.)3.REQUIREMENTS3.1Qualification.Themanufacturershallberesponsibleforconductingqualificationtestsandfurnishingpartdrawings,certifiedqualificationtestreports(ifrequiredbythepurchaser)andtestsamples.Thefastenersfurnishedunderthisspecificationshallbeproducedusingthesamemanufacturingmethodsasusedtoproducefastenersthathavepassedqualificationtests.Thepurchasermayapplyanyoralltestsspecifiedhereintoanyproductrepresentedasmeetingthisspecification,atanytime,toverifyconformance.3.2Materials.Materialsshallbecarbonoralloysteelselectedfromoneofthefollowingtablestitled:“StandardNonresulphurizedCarbonSteels:CompositionsandFormsAvailable”“Standard(SAE)NonresulphurizedCarbonSteelsforPlates,Sheet,Strip,StructuralShapes,andWeldedTubing”or“StandardandTentativeStandardAlloySteels”ofFederalStandardNo.66.Thematerialshallbesound,ofuniformqualityandcondition,freefrompipes,andshallnotcontaindecarburization,carburization,lap,cracks,twists,seams,orotherdefectsdetrimentaltothefabricationorperformanceofparts.3.2.1Heattreatment.HeattreatmentofsteelshallbeinaccordancewithSpecificationMIL-H-6875.SHEET2REVISIONAPPROVALDATEMAY2000USEOFORRELIANCEUPONTHISDOCUMENTORANYNATIONALAEROSPACESTANDARD