Hello can you please help me solving this question using MINITAB only can you please show me the steps also of how you did it on minitab please

6.1.8) Preventing fatigue crack propagation in aircraft structures is an important element of aircraft safety. An engineering study to investigate crack in n = 10 cyclically loaded wing boxes reported the following crack lengths (in mm): 2.20, 2.98, 3.04, 1.78, 1.10, 1.29, 2.10, 2.50, 2.60, 2.55. Calculate the sample mean, sample standard deviation, prepare a dot diagram of the data and interpret the diagram and calculated sample statistics