T.O. 33B-1-1Figure 1-6.Illustration of Crack Depth in Chrome-Plated Panel1.5.4.2Procedure for Testing Material Performance.NOTEPanels are cracked on one face only. When the penetrant materials areapplied to the cracked face, surplus penetrant materials often get on the backof the panel. Penetrant materials on the back must be removed to keep fromcontaminating the cracked panel face.a.Observe the following precautions when processing the cracked chrome plate panels:(1)Do not expose the test panels to temperatures above 212oF (100oC).(2)Use extreme care in handling and storing the panels. Do not drop, hit, or place undue mechanicalstress on the test panels. Do not attempt to bend or straighten the test panels.(3)Prior to and after each use, clean the test panels by immersion and agitation in a solvent.Cleaning with an ultrasonic solvent cleaning system can also be used. Some handling or touchingof the plated surfaces is necessary, but should be kept to a minimum to reduce fingerprintcontamination. After cleaning, examine the plated surfaces under a black light for evidence ofentrapped residues from previous inspections. Time must be allowed after cleaning to ensure allof the solvent has evaporated from the panels before using them.(4)The mirror surface finish and f law shape on the test panels are not representative of normalaircraft parts. This requires special procedures when using the test panels. The main differenceis the extreme care that must be taken during the surface penetrant removal step. It is very easyto remove entrapped penetrant from the test panel cracks.b.Place a small quantity of in-process or working bath materials and reference materials in separatecontainers for each material. DO NOT apply the reference materials from their storage containers toavoid contaminating the entire reference sample. DO NOT apply the working bath and referencematerial with the same brush or swab. Any mixing of the two materials will invalidate the testresults.1-32Change 2
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