An aeroacoustic analysis of a turbulent boundary layer numerical database is conducted, aiming at the identification of acoustically efficient flow structures. The free-stream Mach number is 0.5 while the initial Reynolds number based on the local momentum thickness of the laminar boundary layer is 480. The flow and its acoustic radiation was obtained in a previous study by direct numerical solution of the unsteady Navier-Stokes equations for a compressible, viscous flow. The post-treatment starts with data reduction, keeping only the first mode of a spanwise Fourier series expansion, selecting relevant parallel planes: one near the wall and one in the acoustic region, and focusing on the pressure field. The data thus reduces to two scalar fields of the streamwise coordinate and time. Space-time correlations then allows to quantify global properties of both fields, such as time and length scales and convection velocity of the hydrodynamic pressure, and main acoustic propagation angle, which are found in agreement with the qualitative and quantitative previous observations. Collection of flow and acoustic events is then conducted using amplitude criteria, and causality relationship is investigated assuming convected spherical radiation.