T.O. 33B-1-14-664.5.8.3 MetalSmearing.Flowing of surface metal may result from machining operations, abrasion during service, or by deformation duringassembly or disassembly of an aircraft or component. The depth of smearing in nonmagnetic materials and itsmetallurgical effects will rarely exceed 0.002 to 0.003 inch. At normal crack detection frequencies, the metallurgicalchanges created by smeared metal may not affect eddy current response. However, metal build-up and depressionsassociated with the smearing create changes in lift-off. With meter type instruments this change may exceed lift-offcompensation and cause irrelevant indications. With impedance plane analysis instruments detection of flaws will notbe affected, if sufficiently separated inphase angle from the lift-off angle. In ferromagnetic steel, eddy currentpenetration is very shallow, and any blemish of the surface increases the difficulty of inspection.4.5.8.4 Scratches,Gouges,AndPitting.Scratches, gouges, and pits may result in eddy current signals similar in magnitude to those from cracks. As testfrequencies increase, the sensitivity to scratches tends to increase, because the eddy current field is more concentrated atthe surface.4.5.8.5 CompensationOfMetersForSurfaceConditions.Because eddy current inspection is sensitive to a number of material and inspection conditions, many indicationsrequire additional investigation to separate cracks from other variables. In some cases when testing with meter typeinstruments, separation of cracks from increases in lift-off may be obtained by changing the amount of lift-offadjustment. Increasing the amount of lift-off adjustment or intermediate layer reduces the signal from lift-off orreverses its direction. Reduction of the amount of lift-off adjustment increases the magnitude of the response from lift-off.4.5.8.6 RateOfDeflection.Rapidity of response with a meter or impedance plane display instrument is also a means of evaluating indications.When traversing a crack, a quick rapid deflection is obtained. Variations in conductivity, gradual thickness changes,out-of-round holes, and variations in edge-to-probe spacing provide a slow, gradual change in measured response. Theinspector should be aware of the rate of change in response from cracks, as contrasted to the rate of signal change fromslow changing material properties or test conditions.4.5.8.7 EstimationOfCrackSize.Cracks have the three dimensions of length, width, and depth. All three of these dimensions have an effect on the eddycurrent response from the flaw. In general, the length of the flaw can be related to the distance over which a signalabove a specified level is obtained. When the crack is perpendicular to the surface, the approximate depth of the crackcan be determined from the eddy current indication. With meter type instruments this will usually be related to thesignal amplitude. With impedance plane analysis instruments the depth can be determined by the phase angle andamplitude of the indication. When using a meter type instrument to measure small cracks, amplitude correlates betterwith crack area rather than crack depth. The width of the crack also influences the magnitude of the indication. Withimpedance plane analysis instruments, the signal shape, phase, and amplitude can be used to estimate the depth andarea of the crack. Generally, the crack dimension of greatest interest is the depth. With meter type instruments this isthe most difficult dimension to measure, and estimation of crack size should only be applied to those situations wherecrack geometry is similar and considerable data has been developed relating crack size to meter response. Withimpedance plane analysis instruments, crack depth measurements in nonferromagnetic materials can be performedwhen based upon the phase response.4.5.9 EffectOfScanRateAndPattern.4.5.9.1 MeterInstruments.When manualscanning is performed using meter type instruments without a recorder, the amplitudeof responsedecreases with increasing scanning speed because of the damping effect of the meter. In the same manner, the ends of acrack can be established by the point at which the amplitude of deflection falls below a predetermined level.Mechanized scanning rates with meter instruments and recorder output are limited to the response rate of the recorder.Scan speeds must always be maintained below the maximum response of the detection system in order for the systemsensitivity to remain linear and within calibration.
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