The article includes the description of the measurements of the military aircraft’s fuselage resistance, conducted for the purpose of identifying corroded spots in the fuselage’s mechanical connections’ structure. Considerations regarding the errors in measuring the single connections of the airframe’s mechanical element pairs and the entire structure of such connections in an actual aircraft are also presented. The paper includes the proposal of the superposition method for locating the mechanical connection pairs with improved electrical resistance. Simultaneously, for the purpose of forecasting the time of exploitation of the selected (most endangered) fuselage mechanical connections pairs, the article proposes conducting (in laboratory conditions) of the accelerated ageing process and converting the results to real-time using the Arrhenius method.
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