The width of an outer aircraft panel is uniformly distributed between 1.00 to 1.10 millimeters. Determine the following: a. Proportion of panels that exceed 1.05 millimeters b. Thickness exceeded by...


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The width of an outer aircraft panel is uniformly distributed between 1.00 to 1.10 millimeters. Determine<br>the following:<br>a. Proportion of panels that exceed 1.05 millimeters<br>b. Thickness exceeded by 90% of the flanges<br>O a. 0.30, 0.06<br>b.0.50, 0.96<br>Oc. NONE<br>O d.0.50, 1.01<br>

Extracted text: The width of an outer aircraft panel is uniformly distributed between 1.00 to 1.10 millimeters. Determine the following: a. Proportion of panels that exceed 1.05 millimeters b. Thickness exceeded by 90% of the flanges O a. 0.30, 0.06 b.0.50, 0.96 Oc. NONE O d.0.50, 1.01

Jun 08, 2022
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