Ensuring Structural Integrity
in Aircraft Engine Components
Figure 4 - A complementary inspection system ensures the detection of all critical cracks at a high probability of detection.
Figure 5 - KET indications correlate with metallurgy but not with florescent penetrant inspection.
Figure 6 - Leaking gage assembly caused by microshrinkage. (Photo © 1995 Radian Corporation. Used by permission.)
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