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The thickness of a flange on an aircraft component s uniformly distributed between 1.95 and 2.05 millimeters. Determine the following. a) Cumulative distribution function of

The thickness of a flange on an aircraft component s uniformly distributed between 1.95 and 2.05 millimeters. Determine the following.

a) Cumulative distribution function of flange thickness

b) Proportion of flanges that exceeds 2.03 millimeters.

c) thickness exceeded by 95% of the flanges.

d) Mean and variance of flange thickness.

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