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This paper deals with selected methods of approximate determination of a strain-controlled fatigue life curve for aluminium alloy sheets used in aircraft structures first of all. Authors based their analysis of those methods on the results of own research of 2024-T3 alloy and its Russian equivalent D16CzATW. The approximate strain-fatigue life curves were compared with the experimental curves. The influence of inconsistencies between those curves on the calculation results was analyzed onfatcat:7onfqq7vz5et3d2kpj45mgghle