Recent aircraft noise calculation methods separate engine and airframe noise components to provide accurate single-flight noise predictions. General noise mapping, such as legal compliance calculations, usually relies on position data as the only available input. Therefore, more advanced input variables of engine and airframe noise models require estimation based on position data. We present a methodology to estimate aircraft's configuration and engine rotational speed for jet airliners from position data. The problem is split into a statistical evaluation of the aircraft's configuration, and a flight phase specific modelling of engine rotational speed. The modelling is validated using flight data recorder data, both as relative deviations of the estimation with respect to the reference and in terms of its acoustic impact on noise contours. The latter gave receiver level deviations of less than 0.2 dB for 85% and of less than 0.6 dB for 95% of the areas affected by departures, as well as of less than 1 dB for 95% of the areas affected by approaches. Major differences (above 0.6 dB) mostly occur in areas with low relevance for noise contours for scenarios. With a few modifications based on local procedures, the models are applicable to other airports.