In this paper, experimental tests have been performed in order to examine the behavior of double lap adhesive joints under constant amplitude fatigue loading and then, a fatigue damage model was proposed based on ratchetting strain as a damage parameter. This parameter was employed in this study since it is feasible to be measured during the operational life of structures without interruptions and in a non-destructive manner. The predictions produced by proposed model revealed acceptable agreements with the experimental data. Afterward, an alternative form of the F-N curve was obtained which can be used to establish the design allowables.