T.O. 33B-1-14-73gap, paint and primer thickness. Standards for pitting may also be used for exfoliation and intergranular attack.Standards should also have approximately the same curvature as the part.4.6.5.11 InspectionProcedure-CorrosionDectection.Detection of corrosion with eddy current techniques is applied to aircraft skins when corrosion may occur oninaccessible interior surfaces. Corrosion usually results in areas where moisture is entrapped. If relatively uniformthinning is expected, corrosion detection may be simply a matter of thickness measurement. In most instances,corrosion is confined to smaller localized areas of relatively small diameter. As skin thickness increases, sensitivity tosmall areas and shallow depths of corrosion is reduced.4.6.5.12 PartPreparation.Prior to inspection, all foreign material should be removed from the area to be inspected. Any roughness, sharp edges,or protrusions that could damage the probe or cause errors in readings should be removed by light sanding within thelimits of the applicable T.O.'s. The locations of all fasteners, edges and changes in structure on the far side of theinspection surface should be established and marked with an approved removable marker to aid in the interpretation ofinspection results. Paint removal is not required if it is relatively uniform and not loose or flaking.4.6.5.13 InspectionProcedures.Because of the wide variety of corrosion attack, inspection shall be performed in accordance with the applicable T.O.SECTION VIICONDUCTIVITY MEASUREMENT4.7 SPECIFICAPPLICATION—CONDUCTIVITYMEASUREMENT.4.7.1 RelationshipOfMechanicalPropertiesAndConductivity.4.7.1.1 StructureOfMetals.The atoms of a chemical element have a nucleus or center with a positive charge. Around each nucleus are orbitingelectrons. Each element has a different size nucleus surrounded by a characteristic number and arrangement oforbiting electrons. The distribution and number of the outermost electrons determine the properties of theelement,including its metallic or nonmetallic nature. In a crystalline solid the atoms are stacked in orderly arrangement calledlattices.4.7.1.2 MehcanicalProperties.The physical properties of a metal are related to the binding energy between the atoms. Yield strength, tensile strengthand fatigue strength are determined by resistance to plastic deformation. Plastic deformation is permanent distortion ofthe metal and results from shearing along layers of atom. Plastic deformation is made easier by the presence oflocalized imperfections in the lattice. These lattice imperfections are called dislocations and are present in greatnumbers in all commercial metals and alloys. If the resistance to movement of the dislocations can be increased, thestrength of the metal can be increased.4.7.1.3 ConductivityOfMetals.Metals are good conductors of electricity. Conductivity is dependent on the arrangement of atoms in each metal latticeand the distribution and energy of the electrons surrounding each atom. Any variation in the structure of metals thataffects the electronic structure and energy of the atoms changes the conductivity of the metal. For simplicity, adecrease in conductivity may be associated with obstacles in the path of electron flow through a metal. The obstacles toelectron flow may be caused by lattice distortions resulting from dislocations, missing atoms (lattice vacancies), foreignatoms, or grain boundaries. The presence of particles of different composition also restricts the flow of electrons, agreater number of smaller particles offering more resistance than fewer larger particles.
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