Show transcribed image text The propagation of fatigue cracks in various aircraft parts has been the subject of extensive study in recent years. The accompanying data consists of propagation lives to reach crack size in fastener holes intended for use in military aircraft. 736 .863865 .913.915 937 .9831.007 1.011 1.064 1.109 1.132 1.140 1.153 1.253 1.394 Construct a normal probability plot for the data. Does it appear plausible that propagation life has a normal distribution? Explain. (Please make sure you upload any graphs or tables to support your explanation.)
The propagation of fatigue cracks in various aircraft parts has been the subject of extensive study in recent years. The accompanying data consists of propagation lives to reach crack size in fastener holes intended for use in military aircraft. 736 .863865 .913.915 937 .9831.007 1.011 1.064 1.109 1.132 1.140 1.153 1.253 1.394 Construct a normal probability plot for the data. Does it appear plausible that propagation life has a normal distribution? Explain. (Please make sure you upload any graphs or tables to support your explanation.)
