This paper describes an investigation into the effects of a single-peak tensile overload on fatigue crack propagation in a 9%Cr 1 %Mo steel. Overloads were applied during cycling at a constant stress intensity range (AK), and any consequent transients in growth rate were recorded. The severity of retardation rises as the magnitude of the applied overload is increased. The effect of temperature is complex, but a 525°C retardation is significantly less marked than at 25 or 225°C. Signs of crack face contact are seen on post-overload fracture surfaces, but there is little crack branching. The dominant cause of overload retardation in this steel appears to be plasticity-induced closure. At 525"C, post-overload dwell periods significantly reduce the severity of retardations. This is not observed at lower temperatures, indicating that the residual clamping stresses that lead to closure are gradually relieved at 525°C. NOMENCLATURE aR = length of subsequent crack growth over which growth rates are affected by an overload do, = size of monotonic plastic zone resulting from an overload da/dN = crack growth increment per cycle AK = stress intensity range AKef = effective stress intensity range experienced at the crack tip when a closure mechanism is operating AK,,, = threshold stress intensity range, below which there is negligible crack growth K,,, = maximum stress intensity during the baseline fatigue cycle KO, = peak stress intensity applied during an overload Nd = number of cycles by which an overload delays crack growth N: = Nd normalised with respect to the number of cycles a crack would normally take to grow the distance aR during constant amplitude loading if no overload were imposed cry = uniaxial yield stress