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A series of calibration and flow survey tests were conducted in the 11-By 11-Foot Transonic Wind Tunnel following the modernization of the Unitary Plan Wind Tunnel at the NASA Ames Research Center. These tests included measurements of the static and total pressure which are required to develop the calibration tables used to compute the facility tunnel conditions and to correct the model airplane data for longitudinal buoyancy effects. Measurements of the total temperature, flow angle, and boundary layer characteristics were also made to provide an indication of the flow quality in the test section. Calibration parameters were determined for both test section wall configurations; slots normal for fullspan model testing and floor slots sealed for semi-span model testing.