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4-5 <br />Although a fixed single value for each material was selected for the <br />stability assessment, sensitivity of the results was reviewed to <br />determine if reduced conservatism in the selection of a parameter for a <br />particular material would greatly affect the resultant factor of <br />safety. Conclusions drawn concerning this subjective parametric <br />analysis are discussed below. <br />4.1.2 Piezometric Conditions <br />1 The effects of ground water levels and seepage are critical factors in <br />the stability evaluation of the tailings dam. The piezometric levels <br />used for the stability analysis were based on the hydrologic model <br />conditions as discussed in Section 3.3 and shown in Figure 8. <br />The observed piezometric conditions were incorporated into the analyti— <br />cal model for Case A (existing conditions) as shown in Figure 9. For <br />the two future cases, maximum operating pool and raised embankment, it <br />was necessary to extrapolate the existing data. Phreatic surfaces <br />through the embankment associated with the higher pond levels were <br />estimated using approximate theoretical methods. The assumption was <br />made that flow through the core would be consistent with standard flow <br />through a homogeneous dam core. The piezometric levels in the bedrock <br />were assumed to increase in direct proportion to the increased differen— <br />tial head between the pond and the ground surface downstream from the <br />dam toe. The extrapolated piezometric surfaces for each case are shown <br />on Figure 9. <br />4.1.3 Analysis Results <br />The minimum factor of safety against slope failure was calculated for <br />each case for two modes of failure <br />(circular and black), and for static <br />and earthquake conditions. The pseudostatic earthquake analysis was <br />performed with a ground acceleration of 0.025 based on the seismic risk <br />for the project location (Corps of Engineers, 1977). The results of the <br />stability analysis are presented in Figure 9. <br />1" !!! ;0e �� <br />