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1、9/8/98AC43.13-1BSECTION8.TAPTESTINGPar5-105Page5-539/8/98AC43.13-1B5-105.GENERAL.Taptestingiswidelyusedforaquickevaluationofanyaccessibleaircraftsurfacetodetectthepresenceofdelaminationordebonding.a.Thetaptestingprocedureconsistsoflightlytappingthesurfaceofthepartwithacoin,lightspecialhammerwitham
2、aximumof2?ounces(seefigure?522),oranyothersuitableobject.Theacousticresponseiscomparedwiththatofaknowngoodarea.b.A“flat”or“dead”responseisconsideredunacceptable.Theacousticresponseofagoodpartcanvarydramaticallywithchangesingeometry,inwhichcaseastandardofsomesortisrequired.Theentireareaofinterest
3、mustbetapped.Thesurfaceshouldbedryandfreeofoil,grease,anddirt.Taptestingislimitedtofindingrelativelyshallowdefectsinskinswithathicknesslessthan.080?inch.Inahoneycombstructure,forexample,thefarsidebondlinecannotbeevaluated,requiringtwosideaccessforacompleteinspection.Thismethodisportable,butnoreco
4、rdsareproduced.Theaccuracyofthistestdependsontheinspector’ssubjectiveinterpretationofthetestresponse;therefore,onlyqualifiedpersonnelshouldperformthistest.Par5-105Page5-539/8/98AC43.13-1BFigure5-22.Sampleofspecialtaphammer.5-106.?5-111.[RESERVED.]SECTION9.ACOUSTICEMISSIONPar5-Page5-559/8/98AC43.1
5、3-1B5-112.GENERAL.AcousticEmissionisanNDItechniquethatinvolvestheplacingofacousticalemissionsensorsatvariouslocationsontheaircraftstructureandthenapplyingaloadorstress.Thelevelofstressappliedneednotreachgeneralyielding,nordoesthestressgenerallyneedtobeofaspecifictype.Bendingstresscanbeappliedtob
6、eamedstructures,torsionalstresscanbeappliedtorotaryshafts,thermalstressescanbeappliedwithheatlampsorblankets,andpressureinducedstresscanbeappliedtopressurecontainmentsystemssuchastheaircraftfuselage.Thematerialsemitsoundandstresswavesthattaketheformofultrasonicpulsesthatcanbepickedupbysensors.C
7、racksandareasofcorrosioninthestressedairframestructureemitsoundwaves(differentfrequenciesfordifferentsizedefects)whichareregisteredbythesensors.Theseacousticemissionburstscanbeusedbothtolocateflawsandtoevaluatet