For effective development of jet noise reduction concepts, it is necessary to understand the physics underlying noise generation process. One of experimental methodsAzimuthal Decomposition Technique (ADT) -which allows extracting subtle features of noise sources of different types, was elaborated in TsAGI. ADT was successfully applied to the analysis of jet noise sources at small-scales. In laboratory tests, ADT is realized by a circular 6-microphone array with uniformly distributed microphones located in the acoustic far field of the jet. In the present paper, we present a generalization of this method for the case of azimuthally nonuniform microphones distribution with the view of its application to the analysis of large-scale jet noise. It is shown that jet noise measurements by only 3 microphones in each cross-section allow reconstruction of 3 azimuthal modes directivities (axisymmetric, 1 st and 2 nd ) for low and moderate frequency bands, while 2-microphone measurements make it possible to reconstruct axisymmetric mode directivity and sum directivity of 1 st and 2 nd modes, the microphones being properly located. The latter method is shown to be suitable for utilizing on an outdoor test bench. At first stage, the modified methodology is validated on the small-scale laboratory database, and then it is applied to the jet issuing from the real engine in the ground tests. The information about the azimuthal modes properties is used to investigate physical aspects of the large-scale jet noise sources.