In this paper, fatigue performance of an aluminide layer coated, coarse-grained MAR 247 nickel superalloy was monitored by using the full-field Electronic Speckle Pattern Interferometry (ESPI) method in the range of stress amplitude from 350 MPa to 650 MPa. It was found, that the ESPI method enables precise monitoring of the fatigue behaviour of coated MAR 247 specimens since the area of potential failure was accurately indicated within the initial stage of fatigue damage development.