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This paper describes a ground facility for an APU, TG-16M-type.This kind of APU assisted some Russian (soviet) passenger aircraft during their ground engines’ startup and also when the deicing electrical system was switched on. TG-16M turboshaft and generator embedded system together with its control panel and electrical sources are parts of the Aerospace Engineering Laboratories in University of Craiova facilities. One has realized a fuel supplying installation, an electrical supplying and control system, as well as an engine operating parameters’ board apparatus panel. Tests results were used for some scientific contributions and papers, but the embedded system is also useful for aerospace students education (both for license and master studies); some specific results may be useful also for PhD studies.

GROUND TEST FACILITY FOR A TURBOSHAFT-TYPE APU TG-16M FOR PASSENGER AIRCRAFT