A control system for controlling compressor extraction air flows from extraction points along a compressor of a turbine system during engine turn down comprising: a plurality of sensors located in a turbine system; a control unit comprising a control unit processor in communication with the plurality of sensors, wherein the control unit processor is configured to execute computer-implemented instructions to: monitor by the control unit, a combustor exit temperature of a turbine system; detect, by the control unit, the combustor exit temperature is below a threshold, wherein the threshold is associated with a decrease in the exit temperature of the combustor; in response to detecting the combustor exit temperature is below the threshold, increasing the combustor exit temperature by transmitting a control signal to at least one variable compressor extraction orifice located in the turbine system the at least one variable compressor extraction orifice being in connection with an extraction conduit disposed in flow communication with an extraction point of the compressor, the control signal causing the at least one variable compressor extraction orifice to alter at least one extraction air flow from the compressor, wherein prior to transmitting a control signal to at least one variable compressor extraction orifice located in the turbine system transmitting to a user interface an indicator that the combustor exit temperature is below the threshold and receiving from the user interface, instructions to adjust at least one variable compressor extraction orifice located in the turbine system; detect that at least one additional operating parameter is operating in a predetermined operating range; and based on the detection causing at least one additional variable compressor extraction orifice to increase the extraction air flow from the compressor, wherein the control unit processor is further configured to execute computer-implemented instructions to redirect the at least one compressor extraction air flow into a portion of the turbine system. a plurality of sensors located in a turbine system; a control unit comprising a control unit processor in communication with the plurality of sensors, wherein the control unit processor is configured to execute computer-implemented instructions to: monitor by the control unit, a combustor exit temperature of a turbine system; detect, by the control unit, the combustor exit temperature is below a threshold, wherein the threshold is associated with a decrease in the exit temperature of the combustor; in response to detecting the combustor exit temperature is below the threshold, increasing the combustor exit temperature by transmitting a control signal to at least one variable compressor extraction orifice located in the turbine system the at least one variable compressor extraction orifice being in connection with an extraction conduit disposed in flow communication with an extraction point of the compressor, the control signal causing the at least one variable compressor extraction orifice to alter at least one extraction air flow from the compressor, wherein prior to transmitting a control signal to at least one variable compressor extraction orifice located in the turbine system transmitting to a user interface an indicator that the combustor exit temperature is below the threshold and receiving from the user interface, instructions to adjust at least one variable compressor extraction orifice located in the turbine system; detect that at least one additional operating parameter is operating in a predetermined operating range; and based on the detection causing at least one additional variable compressor extraction orifice to increase the extraction air flow from the compressor, wherein the control unit processor is further configured to execute computer-implemented instructions to redirect the at least one compressor extraction air flow into a portion of the turbine system. monitor by the control unit, a combustor exit temperature of a turbine system; detect, by the control unit, the combustor exit temperature is below a threshold, wherein the threshold is associated with a decrease in the exit temperature of the combustor; in response to detecting the combustor exit temperature is below the threshold, increasing the combustor exit temperature by transmitting a control signal to at least one variable compressor extraction orifice located in the turbine system the at least one variable compressor extraction orifice being in connection with an extraction conduit disposed in flow communication with an extraction point of the compressor, the control signal causing the at least one variable compressor extraction orifice to alter at least one extraction air flow from the compressor, wherein prior to transmitting a control signal to at least one variable compressor extraction orifice located in the turbine system transmitting to a user interface an indicator that the combustor exit temperature is below the threshold and receiving from the user interface, instructions to adjust at least one variable compressor extraction orifice located in the turbine system; detect that at least one additional operating parameter is operating in a predetermined operating range; and based on the detection causing at least one additional variable compressor extraction orifice to increase the extraction air flow from the compressor, wherein the control unit processor is further configured to execute computer-implemented instructions to redirect the at least one compressor extraction air flow into a portion of the turbine system.