A B S T R A C T A model describing corrosion fatigue crack growth rate da/dN has been proposed. The crack growth rate is assumed to be proportional to current flowing through the electrolyte within the crack during a loading cycle. The Shoji formula for the crack tip strain rateε has been assumed in the model. The obtained formula for the corrosion fatigue crack growth rate is formally similar to the author's empirical formulae established previously. The different effects of K and the fatigue loading frequency f on da/dN, in region I as compared to region II of the corrosion fatigue crack growth rate characteristics can be described by a change of one parameter only: the crack tip repassivation rate exponent.Keywords a model; corrosion fatigue; ship and offshore steels. N O M E N C L A T U R E a = crack nominal-length (i.e. including the notch length) a n = crack net-length (i.e. measured from the notch root) a * f = a constant in the Shoji relation forε A' = a constant in the Gangloff's model B = specimen thickness C = the Paris Law constant C 1 ; C 2 ; C 3 ; C V = constants C II = constant in Eq. (2) da d N air = fatigue crack growth rate in air da d N CF = crack length increment per cycle due to interaction of cyclic deformation and chemical reactions da d N e = corrosion fatigue crack growth rate da d N m = pure mechanical fatigue crack growth rate E tip = the crack tip electrochemical potential E x = electrochemical potential within the crack at the point of coordinate x f = loading frequency i A = anodic current density i(t) = the transient current after the crack tip surface film rupture K max ; K = respectively: the maximum and the range of stress intensity factor m = the Paris Law exponent n = exponent in Eq.(2) n i = the crack tip repassivation exponent P; P = respectively: load and the load range Q = electric charge passed through the crack per load cycle Q r = electric charge passed through the crack per rupture event of the crack tip filmCorrespondence: M. Jakubowski.