Research related to fatigue life assessment of turbine attachment was introduced. The progress， shortcomings， and development trends of existing research were discussed in terms of multi-field load analysis， crack initiation life assessment， crack propagation analysis， and test techniques， respectively， focusing on the methods for assessing the service life and damage tolerance of turbine attachment. The results show that the existing analysis and test methods can basically achieve the fatigue life assessment of turbine attachment， but due to various limitations， the engineering applicability needs to be improved. It is necessary to conduct research on robust reduction order methods for load analysis， life assessment methods based on physical mechanisms and data-driven， crack growth simulation under variant loading amplitude， and test techniques in complex thermomechanical environments， and to develop a system to support the fatigue life assessment and validation of turbine attachment in advanced aero-engine.