The invention discloses an integrated 
avionics equipment fault intelligent diagnosis 
system, and aims to provide a diagnosis 
system which is accurate in fault positioning, high in fault identificationcapability and strong in robustness. The 
system is realized through the following technical scheme: a data preprocessing module converts acquired equipment data into a difference value of equipment fault timestamps, and the two columns of data are stored into a first 
database as a fault 
event sequence; a Hawkes 
process module periodically sends a detection 
signal, judges whether the system has afault and the type of the system fault, diagnoses the fault type, the fault part and the reason, and sends the detected fault 
signal to a 
survival analysis and prediction module to identify the faultsize and the time-varying characteristic, a time dependent variable is introduced, a proportional risk regression model COX regression model is constructed by taking survival outcome and survival timeas dependent variables, a survival function is obtained from the Hawkes 
process module, and 
fault analysis is performed according to units of different fault timestamps to complete a fault diagnosistask.