An experimental research program was performed in a pressurized hot component test rig to evaluate surface temperatures, cooling effectiveness and heat transfer coefficients on a convective cooled turbine vane at near engine conditions. The results were obtained in a 40° five-vane sector cascade at exit Reynolds numbers of 0.98*106 and 2.28*106 at a turbulence level of 4 %. The tests were performed both in steady state and in transient modes. The temperature solving part of a cooling design system was used to evaluate the heat transfer coefficients. A two-dimensional boundary layer program and the commercial Navier-Stokes code Rampant were used for obtaining the numerical results. This paper describes the experimental procedure, the evaluation model and method and the comparison of the first experimental results with numerical calculations.