ESDU 85010 discusses the application to the complete aeroplane of the prediction methods given in the Series for the contributions to the derivatives from wing planform and dihedral@ and empennage. Illustrations show for diverse configurations at cruise the relative magnitudes of the contributions for each derivative@ and comparisons with experimental data also show the effect of Mach number@ incidence@ wing sweep@ and high lift devices. A detailed comparison of predictions with experimental data drawn from a wide range of sources including tunnel and flight results shows that the sideforce derivative is predicted to within 0.06@ the yawing moment derivative to within 0.016@ and the rolling moment derivative to within 10 per cent. A comprehensive worked example shows the application of the methods. A computer program of the method is provided as ESDUpac A8510.