Reconsider the model for the aircraft fastener data from Problem 13.3, part a. Construct plots of the deviance residuals from the model and comment  on these plots. Does the model appear satisfactory from a residual analysis viewpoint?

Problem 13.3

The compressive strength of an alloy fastener used in aircraft construction is being studied. Ten loads were selected over the range 2500−4300$2500-4300$ psi and a number of fasteners were tested at those loads. The numbers of fasteners failing at each load were recorded. The complete test data are shown below.

Load, x (psi) Sample Size, n Number Failing, r 2500 2700 50 10 70 17 2900 100 30 3100 60 21 3300 40 18 3500 85 43 3700 90 54 3900 50 33 4100 80 60 4300 65 51