Recently, the application of fracture mechanics to metal fatigue has proven to be quite successful, that is, the fatigue crack propagation rate da/dn has been known to be expressed well by a power function of the range of stress intensity factor AK [I]. This expression, however, is not applicable to the case of very low crack propagation rate, and there is the stress intensity threshold level AK.. below which fatigue crack propagation becomes insignificant [2]. tn On the other hand, the stress ratio R(=o . /a =K . /K ) has been _. I mln _max mln max _ . found to influence the Xa~lgue crack propagation rate and the stress intensity threshold level [2-4]. Furthermore, observations of the tip of crack have revealed that the fatigue cracks are partially closed, even though loading is tension-tension. By considering the effective stress intensity range AK ~. which is calculated from the el crack opening stress, the effect of stress ratlo on the crack propagation rate has been explained [5]. The authors have suggested by a result of measurement on very low propagation rates for various stress ratios that the fatigue crack closure at the stress intensity threshold level shows a particular behavior [4]. To clarify this phenomenon further, the behavior of fatigue crack closure at AK _ was investigated for R of -i, -0.5, 0, 0.4, 0.6, and 0.8 in HTS0 stee~